If all goes well, Venus Express will be a major topic for discussion in this forum a year from now. Does anyone know how good the surface coverage will be from VIRTIS and VMC? My understanding is that VIRTIS will obtain low resolution multispectral maps, and that VMC will, in addition to cloud monitoring, have one channel that can see the surface, but I don't know at what resolution or at what quality. It will be nice to have some non-radar images of Venus' surface besides the Venera snapshots and the shadowy images from Earth and Galileo's NIMS.
Ted
See my new note on the "Radar on Venus Express?" thread, Ted. I may be able to get you some more precise resolutional data later on if I can find the time. (However, VMC -- unlike VIRTIS -- cannot see the surface; it's entirely for UV cloud top patterns.)
Actually, VMC will have some limited capabliity to detect the surface. My source on this is the ESA mission documentation. See below:
3.7 VMC (Venus Monitoring Camera)
Precursors. Imaging of the Venus disc at different wavelength was carried out by the Pioneer Venus orbiter, during the fly-bys of Mariner-10 and Galileo, and from the ground. These data was used to study the atmospheric dynamics at the cloud tops (UV), to investigate the thermospheric dynamics (UV, visible, and near-IR airglow), to map the surface brightness and to study cloud opacity variations (near-IR). However, these observations lacked global spatial and temporal coverage as well as spatial resolution. At the same time they demonstrated the power of the global imaging in the study of dynamical processes in the Venus atmosphere.
VMC/Mars Express. The Video Monitoring Camera (VMC) onboard the Mars Express is a monochrome wide-angle CCD camera that was designed to take the video sequence of Beagle-2 lander leaving the Mars Express spacecraft at Mars.
VMC/Venus Express. The Study Team has recommended to modify the Mars Express camera into a wide-angle multi-channel Venus Monitoring Camera. The modification will consist of adding several narrow band filters in the UV, visible, and near-IR spectral ranges that would allow the camera to provide support imaging for the whole mission, achieve additional science goals, and contribute to the public outreach programme. Preliminary study showed that the modification of VMC will not specify additional requirements to the Mars Express bus and will be fully compatible with spacecraft interfaces. More detailed elaboration of the technical, programmatic, and financial issues related to the VMC modification and accommodation on the spacecraft will be done by the VMC team, Astrium, and ESA during the pre-Phase B study in the beginning of 2002 if the mission is approved. The modified VMC will be prepared in parallel with available VMC/Mars Express in order not to jeopardize the schedule of the mission. In case of failure to modify VMC in time VIRTIS will be able to cover significant part of the VMC goals so that the achieving of the mission objectives would be secured.
The VMC camera will be capable of achieving scientific goals in atmospheric dynamics and surface studies by means of global multi-channel imaging. An example of UV image expected from VMC at Venus is shown in Figure 2.2. Sequence of such images would allow one to visualize the motions of the cloud tops and to study the general circulation and wave phenomena at the altitude of ~70 km. Images of the Venus disc taken every 30 min will be used to create movies of the cloud motions and propagating waves that would be extremely valuable for investigation of the atmospheric dynamics. Figure 2.6 shows an example of image that VMC will take in the visible at night. The monitoring of airglow patterns that originate at 90-110 km is an efficient tool to study the dynamics of the Venus upper atmosphere. The VMC observations in the 1 m transparency window will give the images similar to those shown in Figures 2.5 and 2.9. These images have two types of features. Some of them belong to the surface and result from the temperature and emissivity variations. Second type of markings originates in the main cloud deck and indicates cloud opacity variations. The movies based on such imaging will be used to study global atmospheric dynamics at ~50km.
To summarize, VMC will fulfill the following scientific goals:
Support imaging, i.e. global imaging context for the whole mission;
Observations of the global cloud motions in the UV and near-IR spectral ranges;
Study of distribution of the unknown UV absorber at the cloud tops;
Monitoring the UV and visible airglow and its variability as dynamical tracer;
Mapping the surface brightness temperature distribution and search for volcanic activity.
Besides important scientific goals the VMC imaging and movies will significantly contribute to the public outreach programme.
You've caught me -- I was completely unaware of VMC's near-IR sensitivity. Very embarrassing.
To the powers that be, thank you for creating this forum. It is the first I heard of this mission.
I am fascinated by Venus and looking forward to it now. It sounds like they are interested in studying the atmosphere extensively. Some of the questions they want to answer:
"What are the global characteristics of the atmosphere?"
"How does it circulate?"
"How does the composition of the atmosphere change with depth?"
"How does the atmosphere interact with the surface?"
"How does the upper atmosphere interact with the solar wind?"
The understanding and possible control/conversion of greenhouse gasses on Venus could directly benefit us on Earth. Terraform Mars? Too easy; I say we go for Venus!
Here are some excellent Magellan images of the surface.
http://www2.jpl.nasa.gov/magellan/images.html
Ted - do you have a link for the ESA mission doc(s)?
http://megasn.obspm.fr/VEX_MDR51.doc
It is a bit dated in terms of VENSIS still being listed, but I don't think anything lese has changed.
I wonder if the effects of looking thru narrow spectral bands will result in the sort of quality we get at Titan - or something a bit better than that
Doug
Hard to tell. It is sort of like Pre-Cassini Titan, in that the limiting factor in all images we have is the resolution of the detector, so we don't know just how well we will be able to see. I will research this a bit more and see if I can dig up any speculation. Still, if Venus Express can take images at Cassini/ISS Titan resolution, they will look even more spectacular, because Venus is so much larger. And at last we will have some global multispectral data (although some data to this effect has been assembled from different Radar systems (PVO, Magellen, Venera, and the earthbased collection).
Anyhow, it seems the VMC, while it is a clone of the "Beaglecam" on Mars Express, seems to be hav converted in to quite a good little science instrument. Here is the info from the regular Venus Express website:
http://sci.esa.int/science-e/www/object/index.cfm?fobjectid=33964&fbodylongid=1448
I can dig up some stuff on this for you, given a little more time (sorry it took me so long to even notice the question). As I recall, they're hoping for a resolution of roughly 30-50 km in VIRTIS' near-IR surface maps at Venus' poles, where it will be best -- but that may be just for its possible mineral maps, with the resolution of its actual albedo maps being a lot better.
I believe the spectral 'windows' are much less clear than for Titan, but for Galileo NIMS, some people have made temperature maps of the surface, clearly showing topography. quite cool
My understanding is that the topographically related infrared brightness variations seen by Galileo at Venus were diffused through the lower atmosphere and then the dense middle cloud deck.
VIMS' middle infrared visibility of Titan's surface is quite good, compared with poor visibility and high amounts of diffuse scattering of reflected light in the 1 micrometer 'window" as seen by the Cassini imaging system.
My understanding is that at Venus, the atmosphere has no non-scattering transmission till you reach microwave wavelengths. Basically, imagine holding a sheet of blotchy waxed paper 50 km above the planet's surface and examining the diffuse patterns on the waxed paper from variable amounts and colors <spectral emissivity variations> of the surface below. The blotches will be constantly varying with time and location, but the color and brightnesses of the glow from beneath will be constant, and the color especially, can be separated from the blotchy cloud patterns <which themselves are interesting>
On Cassin, the VIMS is the best instrument we could design with early 90's mid-infrared imaging technology.
We now have real mid-infrared imaging detectors. Not 10 megapixel, but still real camera chips, that can take quality images with really good resolution in the mid-IR (1 to 5 micrometers, more or less). We just @#$@# didn't back then.
An update....though not much new information.
http://www.spacedaily.com/news/venus-05a.html
I suppose it's possible, if not easy, to subtract images taken at night from daytime images. "Not easy" might be too much of an understatement.
http://www.esa.int/esaCP/SEMNBT808BE_index_0.html
She's got it ..... (Am I allowed to quote Bananarama in a space forum ? )
Here's my long-promised entry on whatever I've got regarding VIRTIS' possible ability to map Venusian surface composition.
Unfortunately, the two most important documents on this aren't available for free on the Web: the Nov. 2000 Icarus article by Langevin et al ("Detection of Sub-Micron Radiation from the Surface of Venus by Cassini/VIMS"), and the March 2002 article by V.I. Moroz in "Planetary and Space Science" ("Estimates of Visibility of the Surface of Venus from Descent Probes and Balloons"). I have a photocopy of the former, but can't find the copy I thought I had of the latter. Anyway, the former is optimistic about the possibility: "The 5 spectral windows between 0.85 and 1.18 microns now proven to be sensitive to surface spectral sensitivity provide a potentially effective means for remotely mapping the mineralogical composition of the surface of Venus" [something co-author Kevin Baines was saying for previously]... [They] can be effectively used to distinguish ferric (hematite) and ferrous minerals (e.g., the pyroxenes augite and hypersthene, and olivine). The hydrous mineral tremolite -- thought to be stable on geologic timescales on Venus -- also displays a detectable absorption feature...Both wollastonite -- a CO2 buffer mineral thought to be relating the CO2 surface pressure -- and pyrite are spectrally flat, but have distinctly different ablbedos." There's an accompanying graph of these various minerals' near-IR reflectivities, with the Venusian surface spectral windows overlaying it.
The Moroz article is much more pessimistic: "Constraints on the mineral surface composition would be difficult to derive from orbital observations due to multiple reflections between the surface and the atmosphere." The VIRTIS group itself, the Japanese VCO group and the Vernadsky-Brown Venus group are all intermediate in optimism: they think that it will almost certainly be possible to map FeO, thus distinguishing between felsic and mafic minerals and thus between granites and basalts, and also looking for magnetite on the highly radar-reflective mountaintops -- but aren't sure they can go any farther. (The two longest-wavelength windows seem to be the most useful.) Moreover, it seems much more possible to do this in the north polar regions than elsewhere (which, by an agreeable coincidence, is where Ishtar Terra -- Venus' most likely continent -- is located).
As for spatial resolution (including for temperature and near-surface volcanic gases), estimates are all over the place. Moroz sets it at 50-100 km, the VCO group at 100 km, and David Crisp at no better than 250 km (based on Galileo's flyby results). The VIRTIS group itself initially set it as high as 30 km, but now seems to have it pegged at 90-150 km ( http://irsps.sci.unich.it/~luciam/VEX/DOC/SurfaceScience_VIRTIS.pdf and the May 2005 report at the VIRTIS site: http://irsps.sci.unich.it/~luciam/VEX/ ).
As for quake detection through sensing pressure waves in Venus' dense CO2 air, they are still very interested in that -- although it will require special observational techniques (see the Dec. 2003 and May 2005 reports at the VIRTIS site).
Two more notes:
(1) The VIRTIS team is fully ready to filter out altitude effects from their maps, using Magellan's altimetry maps (see their May 2005 report).
(2) There's another good paper on the possible detection of Venusquakes through atmospheric pressure waves at http://www.lpi.usra.edu/meetings/lpsc2005/pdf/2274.pdf .
http://messenger.jhuapl.edu/the_mission/images/timeline_full_sm.jpg
You gotta love the ESA press people.
"Venus Express will be making the first global examination of the atmosphere of Venus."
Pioneer Venus Orbiter? And to some degree the Venera orbiters?
"The scientific teams of the seven very precise instruments and multi-wavelength cameras on board expect to collect infinitely more science data than all previous missions combined - with the exception of Magellan more than 500 megabits of data received every day."
Yes, it is a lot more than missions besides Magellan, but infinite? I think there is a bit of grandstanding here.
America will just have to make a new probe that returns infinitely more data than the infinite amount ESA is getting.
Well, I doubt there would be time-lapse images. The cloud photopolarimeter built scans slowly like Pioneers 10 and 11, so there wouldn't be many sequences close enough together, and changes in position throughout the scan would be a problem.
New update. Now it is less than 14 days from launching on October 26 from Baikonour Cosmodrome.
http://www.esa.int/SPECIALS/Venus_Express/SEMTXB5Y3EE_0.html
* Propellant loading already completed. Two tanks with more than 260 liters capacity.
* Venus already has its wings. Provides 1,100 watts of power. It is made of Gallium Arsenide Triple Junction
* Electrical test completed. Automatic sequence of maneuvers works.
Almost ready for a trip of 153 days toward to Venus for a mission of 500 days in Venus orbit.
Launch mass is 1,270 kg.
Rodolfo
Preparations for ESA's Venus Express mission passed a new milestone when the
spacecraft was attached to its Fregat upper-stage rocket. The mission is now
only two weeks away from launch on 26 October.
More at:
http://www.esa.int/SPECIALS/Venus_Express/SEMTYW5Y3EE_0.html
The spacecraft Technical details
Spacecraft facts
Spacecraft bus dimensions 1.5 x 1.8 x 1.4 m
Spacecraft mass 1270 kg (including 93 kg of payload and 570 kg fuel)
Thrust of main engine 400 N
Attitude thrusters Two sets of four, each delivering 10 Newtons each
Solar arrays Two triple-junction Ga As;
5.7 square metres; generating 800 Watts
near Earth and 1100 Watts at Venus
Power storage Three lithium-ion batteries
Antennas Two high-gain dishes, HGA1 = 1.3 m diameter,
HGA2 = 0.3 m in diameter, 2 low-gain antennas
http://www.esa.int/SPECIALS/Venus_Express/SEMEE3808BE_1.html#subhead1
The proportion of total weight versus fuel is 44.8% of weight is fuel comparing to the MRO (1,187 kg of fuel hydrazine of 2,180 kg = 54.4% to reduce 1.4 KM/sec during the orbit insertion.) I have not found how the Venus Express will insert into the Venus. At what speed and the what orbit will be traveling VE (Polar, some inclination Equatorial).
The panel solar is very small : 5.7 M^2 versus 10 M^2 of MRO. VE will have about 1,100 Watts and MRO around 1,000 Watts of power when these spacecraft are in their orbits. VE uses Lithium-ion batteries and MRO uses Nickel-hydrogen batteries. What is the difference?
Rodolfo
The problem was already solved by changing the proxy IP Address.
Thanks,
Rodolfo
According to the VE's pdf document, VE has greater challenge to orbit around Venus than Mars Express since it has two great concern that must be adjusted continuously:
1) The thrusters has to adjust to correct the altitude of orbit's pericentre approximately once every day. In fact, due to the gravitational pull of the Sun while the spacecraft is further away from the planet, the pericentre naturally drifts upwards at a rate of about 1.5 kilometres per day.
2) For a spacecraft in orbit around Venus, it is not always possible to point a single
antenna dish at Earth while always keeping the cold face of the spacecraft, hosting
delicate instruments, away from the Sun.To overcome this pointing constraint,Venus
Express has two high-gain antennas mounted on different spacecraft faces.The
main high-gain antenna, used for most of the communications with Earth, is a 1.3
metre-diameter dish.The second, smaller high-gain antenna (30 centimetres
diameter) is used when the spacecraft is in the part of its orbit closest to Earth (less
than 0.78 AU* away).
On the other hand:
I have a doubt about the VE's trajectory to Venus. Will the Soyus-Fraget travel in the opposite way to the Earth's rotation before going to Venus?
I tought it since the Earth position is on the apehelion comparing to the Venus position as perihelion. Hence, the trajectory from Earth to Venus is of inward bound. To launch a spacecraft from Earth to an inner planet such as Venus using least propellant, its existing solar orbit (as it sits on the launch pad) must be adjusted so that it will take it to Venus. In other words, the spacecraft's aphelion is already the distance of Earth's orbit, and the perihelion will be on the orbit of Venus.
This time, the task is to decrease the periapsis (perihelion) of the spacecraft's present solar orbit. A spacecraft's periapsis altitude can be lowered by decreasing the spacecraft's energy at apoapsis. To achieve this, the spacecraft lifts off of the launch pad, rises above Earth's atmosphere, and uses its rocket to accelerate opposite the direction of Earth's revolution around the sun, thereby decreasing its orbital energy while here at apoapsis (aphelion) to the extent that its new orbit will have a perihelion equal to the distance of Venus's orbit. Of course the spacecraft will continue going in the same direction as Earth orbits the sun, but a little slower now. To get to Venus, rather than just to its orbit, again requires that the spacecraft be inserted into its interplanetary trajectory at the correct time so it will arrive at the Venusian orbit when Venus is there. Venus launch opportunities occur about every 19 months.
Will do VE follow the trajectory of least energy orbit as mentioned above?
Rodolfo
Your diagram shows the most common Hohmann transfer orbit, achieved by reducing the aphelion to coincide with the orbit of Venus (preferably when Venus itself is occupying that point along its own orbit).
There is another type of Hohmann trajectory for this type of mission. Instead of braking against the Earth's solar orbital velocity, the spacecraft thrusts at right angles to Earth's near-circular orbit (likely directly towards the Sun), creating a lopsided orbit with a perihelion at Venus and an aphelion well outside of Earth's orbit. The good thing is that the average orbital velocity of such an orbit is very nearly the same as the Earth's velocity, so you don't need to brake so much. The bad thing is that it takes even more energy to enter this transfer orbit, and your approach speed at Venus is somewhat higher, requiring more energy to brake you into orbit.
It gets you there a little faster than the brake-against-solar-orbit method, but it takes more energy.
-the other Doug
Fairing Installation
Today, Monday 17 October 2005, the payload fairing has been successfully installed on the nose block (composite of Fregat Upper Stage and Venus Express spacecraft). The first part of the activity was the tilting of the nose block from vertical to horizontal position. With both the spacecraft and the Upper Stage being fully fuelled the activity is classified as hazardous, and was hence conducted with the minimum number of personnel present in the clean room.
8 days...
The update including some images of the operation :
http://sci.esa.int/science-e/www/object/index.cfm?fobjectid=38153
New updates about Venus Express. More details about the magnetometer instrument.
http://www.spacedaily.com/news/venus-05g.html
Rodolfo
New ESA update : summary of the launch, cruise and arrival phases.
http://www.esa.int/esaCP/SEM0U7R01FE_index_0.html
Rakhir
Delayed:
http://www.esa.int/esaCP/SEM0CV3J2FE_index_0.html
Venus Express preliminary investigations bring encouraging news.
"On Monday 24 October the fairing was removed and engineers started the inspection to assess the status of the spacecraft.
The scenario is so far very encouraging, as only fairly large particles, pieces of the insulating material initially covering the launchers Fregat upper stage, have been found on the body of the spacecraft.
The ESA Project team is confident that Venus Express will be launched well within the launch window, which closes on 24 November this year."
http://www.esa.int/esaCP/SEM2714J2FE_index_0.html
Rakhir
Spaceflightnow Mission Status Center: Venus Express
http://spaceflightnow.com/venusexpress/status.html
--- Although a new launch date has not been set, liftoff is expected to be targeted for sometime between November 6 and 9. ---
Russian space officials Monday set a Nov. 9 blastoff.
http://www.space.com/missionlaunches/ap_051031_venusexp_updt.html
Rakhir
Strange news.
The postpone of the launch was due to contamination problem in the faring. Now, according to the news from space.com :
Russian space officials Monday set a Nov. 9 blastoff for a European probe to explore Venus after its earlier launch was postponed because of a booster rocket problem.
Is it of another story?
Rodolfo
Roll Out to Launch Pad
http://sci.esa.int/science-e/www/object/index.cfm?fobjectid=38214
Rakhir
Pre-launch sequence was executed.
2 days...
http://sci.esa.int/science-e/www/object/index.cfm?fobjectid=38218
Rakhir
Interesting article:
'Venus Mission May Hold Surprises For Scientists And Public, Says CU Prof'
http://www.colorado.edu/news/releases/2005/421.html
If Venus is almost exactly like Earth, but much hotter, and Mars is quite a lot like Earth, but much cooler, and Venus is closer to the sun than Earth, and Mars is further away from the sun than Earth, then hmm, what could it be I wonder...
I'm looking forward to this mission myself..
Besides, the other intrigating thing is that Venus sluggishly rotates on its axis once every 243 Earth days, while it orbits the Sun every 225 days - its day is longer than its year!
On the other hand, Venus rotates retrograde, or "backwards," spinning in the opposite direction of its orbit around the Sun. From its surface, the Sun would seem to rise in the west and set in the east.
The other odd thing is that its Equatorial Inclination to Orbit is 177.3 degrees. By comparison, it is: 7.56 x Earth. That is its north pole is almost pointing to the south pole.
These are at least one of the oddies things that I would like to understand:
Why does the day is longer than a year?
Why the planet rotates on backwards?
Rodolfo
Moons tend to orbit their parent planet in the same direction as the planets rotation - so were a moon to colide with its parent planet, the likely impact would be an increase in rotation I'd have thought.
Perhaps it's a symptom of planet formation closer to the centre of the protoplanetary disk - further out from the sun, the local gravity from chunks of whatever is the major force, but closer in, the suns gravity is dominant.
It's a complex process, that's for sure.
Doug
Well, as Chesterton said, the most remarkable thing about coincidences is that occasionally they DO occur. The classic one in the Solar System is the disks of the Moon and Sun being virtually the same size as seen from Earth, which is the only thing that makes solar eclipses as we know them possible.
The trouble comes when the fact that the human (and presumably animal) mind is designed to specifically look for patterns leads us to jump to the conclusion that a genuine coincidence is more than that. Arthur Koestler once wrote an infamous crank philosophical book based on precisely that logical fallacy.
Anyway, at the beginning of the planetary formation, all planets is formed orbiting around the sun in the counter-clockwise, all have the same plane inclination with respect to the sun, all planets has their axis in perpendicular position to the planetary plane and all rotate the same way as it is orbiting around the sun, it is counter-clockwise.
are those all above suppositions affirmative or not?
Rodolfo
Less than one hour from launch!
Live webcast should be here:
http://www.starsem.com
Alternative link for the live webcast of the launch: http://www.esa.int/SPECIALS/Venus_Express/SEMHZY538FE_0.html
The live feed won't start until 03:28 GMT, at least on the ESA site. I assume it is the same on the Starsem site.
Both webcasts are working now although you get better resolution from the Starsem site.
0327 GMT (10:27 p.m. EDT Tues.)
The Venus Express flight director in mission control has given the final "go" for launch.
0336 GMT (10:36 p.m. EDT Tues.)
T+plus 3 minutes. The first stage strap-on boosters have been jettisoned. The second stage core is still running as planned. All system parameters are reported normal.
Cutoff of 3rd stage and separation of nose module.
There goes the feed. Oh well..guess I'll have to rely on the Spaceflightnow updates.
0348 GMT (10:48 p.m. EDT Tues.)
T+plus 15 minutes. ESA says the first Fregat burn has been successful. The vehicle is now coasting in Earth orbit for more than an hour before the upper stage is re-started to propel the spacecraft to Venus.
Argh! Is that second Fregat burn happening or not?
Fregat burn should be underway by now.
No word on Spaceflightnow yet...
EDIT: cross posting with you Emily. I feel your pain, I don't know how much more page reloads my computer (and me) can take!
From Spaceflightnow.com
0514 GMT (12:14 a.m. EST)
T+plus 1 hour, 41 minutes. By this point in the flight the Fregat should have completed its burn and then released Venus Express. We're awaiting confirmation from ESA that these events have occurred successfully.
From http://sci.esa.int/science-e/www/object/index.cfm?fobjectid=38243
Fregat second stage has successfully fired and place Venus Express to an escape trajectory
From http://sci.esa.int/science-e/www/object/index.cfm?fobjectid=38243
MET: +01h 40m
Fregat second stage has successfully fired and place Venus Express to an escape trajectory
Rakhir
EDIT : You were 1 min quicker than me Bricktop.
Hurrrah!
Venus here we come
This from Daniel Fischer: "Just to report that Venus Express has phoned home exactly on time at 5:30 UTC through ESA's ground station in New Norcia, Western Australia! Everything seems to be going exactly to plan since 2 hours. Now it's about 3 weeks of spacecraft and instrument checkout; perhaps some nice pictures of Earth will be taken during that period (as ESA's Gerhard Schwehm just told me). Then it's quiet cruising (no science on the way), until Venus Orbit Insertion on April 11, 2006."
MET: +02h 40m
Sun acquisiton and successfully deployment of solar arrays confirmed
http://sci.esa.int/science-e/www/object/index.cfm?fobjectid=38243
Rakhir
"Sun acquisiton and successfully deployment of solar arrays confirmed "
------------------ YEEEEHAAWWWWWW! ------------------------------------
Chances of "Loss-of-Mission" have dropped by some 85%
well...there's still orbit insertion.
but hopefully that will all go well. in the meantime: hooray!
"....well...there's still orbit insertion...."
Mars Observer, lost during orbit insertion preparation.
Mars Climate Orbiter, lost in atmosphere during unsurvivable accidental areo-CAPTURE attempt.
Mars-4 and Nozomi both could not attempt orbit insertion burn.
85% is probably a fair arm-waving assessment of the risk fraction for an orbiter mission.
- First star tracker switched on.
- Reaction wheels switched on.
- Venus Express achieved Normal Mode indicating full 3 axis stabilised conditions and full control through ground operations.
http://sci.esa.int/science-e/www/object/index.cfm?fobjectid=38250
Rakhir
Venus' upper atmosphere is MUCH more stable, density-wise, than Mars' -- simply because Mars' total atmosphere is so thin that the heating from dust storms can cause the atmosphere as a whole to dramatically warm, and thus balloon upwards in Mars' weak gravity. In fact, it was stated by a speaker at the COMPLEX meeting that this is the one piece of new environmental engineering measurements we absolutely MUST have for near-future Mars missions even of the unmanned variety: a satellite to monitor Martian weather and its correlation with upper-atmospheric density fluctuations in much more detail than has yet been done. We came within a hair of losing the Spirit rover even BEFORE it also ran into those high-speed near-surface winds (which, by the way, are less important for a throttled-rocket soft lander), because Mars' upper air density was 10% less than even the worst-case prediction based on obsevations the week before the landing, and so the vehicle was braked much less during entry than expected.
I am looking forward to the great discovery of the fact that the visible imaging channels can't see through to the surface.
The EDL data is on the PDS - but it's a bit awkward to use - the derived stuff is in there, I'll see if I can put Pathfinder, Spirit and Oppy pressure profiles together.
Doug
Well MEX stuff is already in the PDS, and ESA opperate their own pseudo-PDS-tool at http://www.rssd.esa.int/index.php?project=PSA - problem being, due to the nature of HRSC data, it's basically impossible to use
Doug
While I agree that the ESA press releases can be exaggerated (infinitely more data?), I can't blame them for wanting to hold onto the data for a while. Nobody has landed anything on Titan before, and as Europe hasn't had much of a space program compared to the US I'm sure they want to impress as much as possible.
Personally, I'm happy with the images they've released thus far. I think that once the ESA has something definitive to say regarding the data they'll say it. I can't think of any benefit for them to holding onto the data forever, unless maybe they're just scouting for rare minerals (and they'd lose all credibility in that case).
It seems to me a difference between releasing data because you want people to be able to access it versus releasing it to the public simply because you are being made to.
Any Earth departure images planned?
Anyway, I think that there is science on the one hand and marketing on the other...
The critical Launch and Early Orbit Phase (LEOP) for Venus Express was completed today.
The spacecraft is performing flawlessly.
Trajectory Correction Manoeuvre (TCM-1) was successfully completed.
The craft is now on the exact trajectory required for Venus Orbit Insertion in five months' time.
With LEOP running so smoothly, controllers were able to bring forward some platform commissioning activities, which were originally planned for the weekend.
With the start of the Near Earth Commissioning Phase, payload activities are due to start on 18 November; these initial switch-on and test activities are scheduled to be complete by 14 December.
http://www.esa.int/SPECIALS/Venus_Express/SEMK9UJBWFE_0.html
Rakhir
Platform Completes near Earth Commissioning.
The remaining testing activities on the platform side will take place in January (thermal characterization) and in February (main engine calibration).
Payload Commissioning Underway : MAG, VIRTIS, and VMC.
During this period the Earth-Moon observation is planned
http://sci.esa.int/science-e/www/object/index.cfm?fobjectid=38323
the earth data cubes from VIRTIS look very promising! Imagine seeing all the cloud layers of venus with this! and even the surface! (sorry just being a bit excited )
http://www.esa.int/esaCP/SEMOIGULWFE_index_0.html
Venus Express - End of Near Earth Commissioning Phase
During the reporting period the last activities of the Near Earth Commissioning
have been completed according to the plan. Two slots with the New Norcia ground
station have been dedicated to test the performance of the TTC subsystem and of
the Ultra Stable Oscillator (USO) for the radio science experiment (VeRA). In
both occasions problems in operating the ground station equipment have affected
the test.
http://sci.esa.int/science-e/www/object/index.cfm?fobjectid=38473
VENUS EXPRESS STATUS REPORT
Report for Period 16 December 2005 - 05 January 2006
During the reporting period the spacecraft has been configured for a passive cruise phase and the only activities conducted on top of the routine ones are the DDOR tests with ESA (NNOCEB) and DSN (GDS-CAN) stations.
http://sci.esa.int/jump.cfm?oid=38559
At the end of the last NNO pass in the reporting period (DOY 006, 06:00) Venus Express was 15.5 million km from the Earth, 131.7 million km from the Sun, and 25.5 million km from Venus. The one-way signal travel time was 52 seconds.
VE is already above than 38% of distance from Earth.
Future Milestones
The coming week will mark a "close to inferior conjunction" condition, therefore, no major operations are planned. The actual conjunction condition will be reached on DoY 011 at around 18:00 when the angular distance between the Sun and the spacecraft as seen from the Earth will be approximately 1.6 degrees. No significant impact is foreseen on the RF link.
http://www.spacedaily.com/news/Venus_Express_Passive_Cruise_Phase_Begins.html
Rodolfo
An interesting milestone today : We are at the halfway point of the 153 days cruise phase.
And it's already a couple of days that VE is closer from Venus than from Earth.
On January 19th, Venus Express was 21.9 million km from the Earth and 19.2 million km from Venus.
http://sci.esa.int/science-e/www/object/index.cfm?fobjectid=38648
Rakhir
Venus Express articles in ESA Bulletin Number 124 online here:
http://www.esa.int/SPECIALS/ESA_Publications/SEMW3IMZCIE_0.html
Contents
Venus Express: The Mission Begins
The Venus Express Mission
Donald McCoy, Thorsten Siwitza & Roy Gouka
Venus Express: The Spacecraft
Alistair J. Winton et al.
The Science Return from Venus Express
Hεkan Svedhem, Olivier Witasse & Dmitri V. Titov
Venus Express Ground Segment and Mission Operations
Manfred Warhaut & Andrea Accomazzo
ESAs New Cebreros Station Ready to Support Venus Express
Manfred Warhaut, Rolf Martin & Valeriano Claros
The Roadmap for a GMES Operational Oceanography Mission
Mark Drinkwater et al.
A Tsunami Early-Warning System
The Paris Concept
Manuel Martin-Neira & Christopher Buck
EGNOS Operations and Their Planned Evolution
Laurent Gauthier et. al.
The BGAN Extension Programme
Juan J. Rivera, Eyal Trachtman & Madhavendra Richharia
Subscribe to the printed version of the ESA Bulletin free of charge. Visit our Bookshop for ordering information.
Thanks, this is really interesting background.
But the pedant in me cant help but quibble at the following quote from the Venus Express Mission section:
surface temperatures reach 470C (about ten times higher than the hottest temperature on Earth),
I know its outreach and all, but thats simply wrong, conceptually wrong. 470C (~740K) is about 2.5 times Earth surface temperature.
It's about 10 times higher above FREEZING than the highest temperatures on Earth, which presumably is what they meant to say.
Continued Spacecraft Testing
http://sci.esa.int/science-e/www/object/index.cfm?fobjectid=38746
During next week the Main Engine pressurisation and calibration will take place.
After the Main Engine burn, an eventual correction will be done one week later.
Successful Venus Express main engine test
http://www.esa.int/esaCP/SEMVX5MVGJE_index_0.html
One hundred days after beginning its cruise to Venus, ESAs Venus Express spacecraft successfully tested its main engine for the first time in space.
Venus Express Ground Observing Project
The Venus Express Ground Observing Project (VEXGOP) is an opportunity to
contribute scientifically useful images and data to compliment the Venus Express
(VEX) spacecraft observations of Venus. The project will focus on utilising the
capabilities of advanced amateurs to obtain images of the atmosphere of Venus;
specifically filtered monochrome images obtained with CCD based cameras in the
350nm to 1000nm (near ultraviolet, visible and near infrared range).
The Venus Express (VEX) spacecraft will observe the planet Venus using seven
instruments for at least two Venusian years (1000 days) beginning in May 2006.
The instrument package includes the Venus Imaging Camera (VMC), which will image
the planet in the near-UV, visible and near-IR range. Although VMC will provide
much higher resolution images of the planet than visible from Earth, continuous
monitoring of the planet will not be possible.
There may be periods, therefore, when parts of the planet are visible from Earth
that are not visible from the spacecraft (due to the spacecraft position in
orbit). Additionally it is important to compare Earth-based observations with
simultaneous spacecraft observations. In particular this will allow us to extend
our understanding of the dynamics of Venusβs atmosphere based on the VEX data
to observations made prior to the VEX mission, as well as after completion of
VEX operations.
Objectives
The objectives of VEXGOP is to obtain high quality images of Venus before, after
and during VEX operations. Amateur astronomers, using CCD based cameras with
filters for specific band passes in the near ultra-violet, visible and near
infrared wavelengths (350nm to 1000nm), are encouraged to participate in the
gathering of images. Observation campaigns will include:
* Routine images of Venus during each apparition
* Coordinated observations during specific periods of the VEX mission to
provide either simultaneous or complimentary ground based images to VEX
spacecraft observations
For more details go to:
http://sci.esa.int/science-e/www/object/index.cfm?fobjectid=38833
Successful Trajectory Correction Manoeuvre
http://sci.esa.int/science-e/www/object/index.cfm?fobjectid=38887
On 24 February a Trajectory Correction Manoeuvre was executed in order to trim the spacecraft trajectory after the Main Engine calibration manoeuvre. The manoeuvre executed flawlessly but the current knowledge of the orbit indicates that it is very likely that another fine tuning will be required once the orbital knowledge has increased.
Preparation for Venus Approach
http://sci.esa.int/science-e/www/object/index.cfm?fobjectid=38933
All calibration, science and maintenance activities of the instruments have been completed and focus is now on the Venus approach phase.
VOI Events Timeline (11 April) :
- Spacecraft reorientation starting at 08:03 (CEST)
- 51 min engine burn starting at 09:19
- Reacquisition of radio contact after a 10 min occultation at 09:56
http://www.esa.int/esaCP/SEMJITM65LE_index_0.html
New VOI timeline (slight modifications compared to previous release) :
- 09:17 --> VEX main engine burn starts
- 09:45 --> Occultation starts (loss of S-band signal)
- 09:55 --> Occultation ends
- 10:07 --> VEX main engine burn ends
- 10:10 --> Announcement by Flight Operations Director
- 11.07 --> X-band transmitter on
- 11:12 --> Telemetry received
- 11:30-12:15 --> Press Conference
All times above are 'Earth Received' time (CEST)
http://www.esa.int/SPECIALS/Venus_Express/SEMMM0NFGLE_0.html
No.12-2006 Paris, 31 March 2006
Venus within ESA probe reach
After its five-month, 400 million kilometre journey inside our solar system
following its lift-off on 9 November 2005, ESAs probe Venus Express will
finally arrive on 11 April at its destination: planet Venus.
Venus Express mission controllers at the ESA Space Operations Centre (ESOC) in
Darmstadt, Germany are making intensive preparations for orbit insertion. This
comprises a series of telecommands, engine burns and manoeuvres designed to slow
the spacecraft down from a velocity of 29000 km per hour relative to Venus, just
before the first burn, to an entry velocity some 15% slower, allowing the probe
to be captured into orbit around the planet.
The spacecraft will have to ignite its main engine for 50 minutes in order to
achieve deceleration and place itself into a highly elliptical orbit around the
planet. Most of its 570 kg of onboard propellant will be used for this
manoeuvre. The spacecrafts solar arrays will be positioned so as to reduce the
possibility of excessive mechanical load during engine ignition.
Over the subsequent days, a series of additional burns will be done to lower the
orbit apocentre and to control the pericentre. The aim is to end up in a 24-hour
orbit around Venus early in May.
The Venus orbit injection operations can be followed live at ESA establishments,
with ESOC acting as focal point of interest (see attached programme). In all
establishments, ESA specialists will be on hand for interviews.
ESA TV will cover this event live from ESOC in Darmstadt. The live transmission
will be carried free-to-air. For broadcasters, complete details of the various
satellite feeds are listed at http://television.esa.int.
The event will be covered on the web at venus.esa.int. The website will feature
regular updates, including video coverage of the press conference and podcast
from the control room at ESAs Operations Centre.
Media representatives wishing to follow the event at one of the ESA
establishments listed below are requested to fill in the attached registration
form and fax it back to the place of their choice.
For further information, please contact:
ESA Media Relations Division
Tel : +33(0)1.53.69.7155
Fax: +33(0)1.53.69.7690
Venus Express Orbit Insertion Tuesday 11 April 2006
ESA/ESOC, Robert Bosch Strasse, 5 Darmstadt (Germany)
PROGRAMME
07:30 Doors open
08:45 Start of local event, welcome addresses
09:10 ESA TV live from Mission Control Room (MCR) starts
09:17 Engine burn sequence starts
09:45 Occultation of spacecraft by Venus starts
09:55 Occultation ends
10:07 Main engine burn ends
10:20 Address by Jean-Jacques Dordain, ESAs Director General, and other
officials
Break and buffet
Interview opportunities
11:30-12:15 Press Conference
Jean-Jacques Dordain, Director General, ESA
Prof. David Southwood, Director of Science, ESA
Gaele Winters, Director of Operations and Infrastructure, ESA
Manfred Warhaut, Flight Operations Director, ESA
Hεkan Svedhem, Venus Express Project Scientist, ESA
Don McCoy, Venus Express Project Manager, ESA
13:15 End of event at ESOC
Venus Express Orbit Insertion ESA/ESOC Darmstadt 11 April 2006
First name: _________________________ Surname: __________________________
Media: ________________________________________________________________
Address: _______________________________________________________________
Tel: _______________________________ Fax: ________________________________
Mobile : ____________________________ E-mail: ______________________________
I will be attending the Venus Express Orbit Insertion event at the following
site:
( ) Germany
Location: ESA/ESOC
Address: Robert Bosch Strasse 5, Darmstadt, Germany
Opening hours: 07:30 13:00
Contact: Jocelyne Landeau-Constantin, Tel: +49.6151.902.696 Fax:
+49.6151.902.961
( ) France
Location: ESA HQ
Address: 8/10, rue Mario Nikis Paris 15, France
Opening hours: 08:00 13:00
Contact: Anne-Marie Remondin Tel: +33(0)1.53.69.7155 fax: +33(0)1.53.69.7690
( ) The Netherlands
Location: Newton Room, ESA/ESTEC
Address: Keplerlaan 1, Noordwijk, The Netherlands
Opening hours: 08:30 12:30
Contact: Michel van Baal, tel. + 31 71 565 3006, fax + 31 71 565 5728
( ) Italy
Location: ESA/ESRIN
Address: Via Galileo Galilei, Frascati (Rome), Italy
Opening hours: 07:00 14:00
Contact: Franca Morgia Tel: +39.06.9418.0951 Fax: +39.06.9418.0952
( ) Spain
Location: ESA/ESAC
Address: Urbanizaciσn Villafranca del Castillo, Villanueva de la Caρada,
Madrid, Spain
Opening hours: 8:30 - 13:30
Contact: Monica Oerke, Tel + 34 91 813 13 27/59 Fax: + 34 91 813 12 19
It looks like the ESA is making a very real effort to allow the public to witness the orbital insertion - complete with a mission scientist news conference. Does anyone know if NASA will patch the broadcast through on the NASA channel?
Venus Express is going as cool toward the hot Venus:
The Venus approach phase is proceeding according to plan with all activities conducted successfully.
A Trajectory Correction Manoeuvre of about 13 cm s-1 has been executed in the evening of 29 March to reduce the pericenter altitude at Venus arrival by a bit more than 100 kilometres. The latest calibration of the nominal TCM gives the following results (uncertainties are 1-sigma):
* magnitude error = -1.2 mm/s (-0.9% +/- 2.1%)
* direction error = 0.8 deg +/- 0.3 deg
The final calibration will be made on 3 April. The current orbit determination does not show the need for any further trajectory correction.
http://sci.esa.int/science-e/www/object/index.cfm?fobjectid=39030
Rodolfo
Two new articles for the preparation of the VOI.
ESAs Venus Express to reach final destination
http://www.esa.int/esaCP/SEM0UGNFGLE_index_0.html
Some information on observations to be performed in capture orbit.
Final Preparations for Orbit Insertion
http://sci.esa.int/science-e/www/object/index.cfm?fobjectid=39059
The fuel and oxidizer tanks have been pressurised and the helium tank is being warmed-up to properly sustain the main engine burn.
On 7 April, the essential commands for the VOI burn will be uplinked to the spacecraft.
Drama in mission control
ESAPod goes to the heart of Venus Express and meets with a veteran ESA
operations engineer in the mission control centre. The large, well-equipped Main
Control Room enables flight controllers to work as a focussed team during
critical events and gives them the central facilities they need to communicate
with support teams worldwide.
Listen to this ESAPodcast at:
http://www.esa.int/SPECIALS/ESApod/SEMCVLNFGLE_0.html
ESAs Venus Express to reach final destination
It was on 9 November last year that ESA's Venus Express spacecraft lifted off
from the desert of Kazakhstan onboard a Soyuz-Fregat rocket. Now, after having
travelled 400 million kilometres in only about five months, the spacecraft is
about to reach its final destination. The rendezvous is due to take place on 11
April.
Full story :
http://www.esa.int/esaCP/SEM0UGNFGLE_index_0.html
Monday, 10-Apr-2006
On 11 April, Venus Express will arrive at Venus and enter orbit around the
planet. The spacecraft's main engine will perform a 50 minute burn, starting
around 07:10 UT, to slow the spacecraft and allow it to be captured by Venus's
gravity.
Updates on the Venus Orbit Insertion (VOI) activities will be posted on the page
http://sci.esa.int/jump.cfm?oid=39060
and on the ESA Portal Venus Express website
http://www.esa.int/SPECIALS/Venus_Express/index.html
ESA TV will broadcast live coverage of the event. For details see
http://television.esa.int
===================================================
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http://sci.esa.int/jump.cfm?oid=34651
The start time of VOI : 7:07:59 UTC. That zone time corresponds to Greenwich line?
Rodolfo
Good Luck VEX!
Don't know how much can be read into it, but at least the webcam at ESOC shows a green board on the screen:
http://www.esa.int/SPECIALS/Venus_Express/SEMN3Y274OD_0.html
We seem to have re-acquisition of the s-band signal. No confirmation yet on success but events are following the plan.
Emily: The main engine has shut down exactly on time!
Also from Emily's report :
Also, another useful tidbit this morning, is that Venus Express Project Scientist Hεkan Svedhem reported on when the first images are expected: about 48 hours after VOI. They will be released to the public, the program moderator said, on April 13 after 4:00 p.m., I presume she meant Central Euroupean Summer Time, or 14:00 UTC
http://planetary.org/blog/article/00000534/
Weird , nothing at spaceflightnow.com They only seem interested in NASA missions now.
I think they are waiting for the press comference and HGA data in a few minutes from now to see if the spacecraft is healthy.
hurray! telemetry recieved!
http://www.planetary.org/blog/article/00000536/
edit: and..
http://www.esa.int/SPECIALS/Venus_Express/SEMZ7QNFGLE_0.html
Is anyone getting the streaming video of the press conference> I;m getting zip..
Im using BBC Online...The briefing doesnt seem to have started yet.
Now says its staring 10am GMT/11 BST
My sound is cutting out.......have they actually said anything about its condition yet? lol
That was like some terrible oscar acceptance speech !!
Emily has been busy. Almost the whole PC is already transcribed on the blog:
http://www.planetary.org/blog/article/00000537/
The PC ran only a few minutes late on the ESA stream, but otherwise the PR of this event was pretty bad. The quickest source of information was still Emily, even though she was runnin back and forth to the mission control and the press room! ESA should employ her for live event reporting :-P
spaceflightnow caught up...
http://www.spaceflightnow.com/venusexpress/060411voi.html
This is great news - congratulations to ESA (and thanks to Emily for detailed news from VOI and the PC).
Now we can look forward to seeing the first images two days from now. It's rather strange that with the exception of 50-100 Galileo images and a few from Cassini these will be the first spacecraft images from this closest neighbor obtained using a modern camera system.
Damn smart is VEX! congratulations to the team! Also to Emily for the updated posting.
Rodolfo
N° 13-2006 Paris, 11 April 2006
Europe Scores New Planetary Success:
http://www.esa.int/SPECIALS/Venus_Express/SEM2GQNFGLE_0.html
Changed to a link - seriously, hundreds of lines ot text in a forum post doesnt make a lot of sense when you can just link to it with the pictures in situ etc. - Doug
I don't think so - IIRC they were going to try the PFS cover again some time after VOI. That text just looks like a copy/paste job into the press release...
...and my congrats to ESA on the successes of VEX & MEX too! Now I think I'll go get some TEX-MEX for lunch
Let me add my kudos to ESA and their fantastic job. Time to dust off the old Venus books!
Podcast ESA.
http://esamultimedia.esa.int/multimedia/esc/venus_express_powers_into_orbit.mp4
There's a bit more from two abstracts from the Fall 2005 AGU meeting on just what they hope to do with VIRTIS where surface observations are concerned:
http://www.agu.org/cgi-bin/SFgate/SFgate?&listenv=table&multiple=1&range=1&directget=1&application=fm05&database=%2Fdata%2Fepubs%2Fwais%2Findexes%2Ffm05%2Ffm05&maxhits=200&="P33A-0227"
http://www.agu.org/cgi-bin/SFgate/SFgate?&listenv=table&multiple=1&range=1&directget=1&application=fm05&database=%2Fdata%2Fepubs%2Fwais%2Findexes%2Ffm05%2Ffm05&maxhits=200&="P33A-0225"
Also, Noam Izenberg's presentation to last November's VEXAG meeting on the observations MESSENGER will make during its second Venus flyby ( http://www.lpi.usra.edu/vexag/Nov2005/MESSENGER_VEXAG.pdf ) includes, on page 8, a description of a possible attempt to mkake similar observations of surface composition
And don't forget VMC....
http://www.agu.org/cgi-bin/SFgate/SFgate?language=English&verbose=0&listenv=table&application=fm05&convert=&converthl=&refinequery=&formintern=&formextern=&transquery=sc%3dplanetary&_lines=&multiple=0&descriptor=%2fdata%2fepubs%2fwais%2findexes%2ffm05%2ffm05%7c1000%7c3633%7cVenus%20Monitoring%20Camera%20for%20Venus%20Express%7cHTML%7clocalhost:0%7c%2fdata%2fepubs%2fwais%2findexes%2ffm05%2ffm05%7c22266835%2022270468%20%2fdata2%2fepubs%2fwais%2fdata%2ffm05%2ffm05.txt
That very nice (and pictorial) document on the DISR photos from last year's Titan Conference which I mentioned down in one of the Titan threads yesterday says that we did manage to get three "almost complete" mosaics, as opposed to the 10 hoped for.
Venus Express has reached final orbit:
http://www.esa.int/esaCP/SEM33O8ATME_index_0.html
Wait until June 4, 2006 when Venus Express start to collect observations from Venus. Now it is undergoing the switching on every 7 scientific instruments.
Until beginning of June, Venus Express will continue its orbit commissioning phase, started on 22 April this year. "The spacecraft instruments are now being switched on one by one for detailed checking, which we will continue until mid May. Then we will operate them all together or in groups" said Don McCoy, Venus Express Project Manager. "This allows simultaneous observations of phenomena to be tested, to be ready when Venus Express nominal science phase begins on 4 June 2006," he concluded.
Venus Express will live for only 2 days !
While Venus Express is expected to spend about 15 months studying its cloud-covered target, the mission will span only two of the worlds exceedingly long days.
Rodolfo
I hear the ESA has a scientific probe in orbit around Venus. Anyone else heard that? I wonder what it's doing? Do you think it might send back pictures? Maybe we will get to see them!
Yes, I hear they plan daily releases of pics, a la MER. (Venusian days.)
Maybe, the most-well informed is of Emily with her blog at http://www.planetary.org/explore/topics/venus_express/
However, the news is still cold dated May 9, 2006 as the most recent ones. I am afraid that the time will be cronometred as venusian day as Lyford is smelling!
Rodolfo
'Until beginning of June, Venus Express will continue its orbit commissioning phase, started on 22 April this year. "The spacecraft instruments are now being switched on one by one for detailed checking, which we will continue until mid May. Then we will operate them all together or in groups" said Don McCoy, Venus Express Project Manager. "This allows simultaneous observations of phenomena to be tested, to be ready when Venus Express nominal science phase begins on 4 June 2006," he concluded.'
http://www.esa.int/esaCP/SEM33O8ATME_index_0.html
What did you want ESA to do before? Draws?...
Let's be patient and hope for some news on the following days...They'll appear...
I hope...
B)-->
B)-->
There is a more recent update from the 6th of June:
http://sci.esa.int/science-e/www/object/index.cfm?fobjectid=39343
And there are, since April, images available:
http://sci.esa.int/science-e/www/object/index.cfm?fobjectid=30913&fareaid=63
OK, it is not a flood of information but there is some...
EDITED: I've contacted the Project Manager Don McCoy but he will be out untill the 12th (maybe he will be at the world cup...who knows?... )
Let's see if there is an answer by then...
Yes, June marks the "Routine Science Operations" becoming, well, routine. (I, despite the highest respect I have for our Quebecois UMSF members, am grateful there are no http://www.montrealpoutine.com/ scheduled.)
I know I can rely on the grace and good humor of this board to get me through the longs dry spells between "daily" releases of information.
Though, as Ustrax pointed out, the VE website does appear to have weekly updates, which is a great thing if they can keep it going. And yes as far as images go like MRO they are few until the operational orbit begins which is now I understand. We should see more soon.
Looking at past missions, there is clearly a problem. People in the EU should apply some healthy critcism of this policy of closed data and image access. It is not appropriate to such an expensive publically-funded program.
Well, yes, but where would the Europeans find someone that dotty? (By the way, a recent E-mail exchange with Keith -- of which I will spare you the sordid details, except that it started out with me trying to compliment him on something -- has confirmed again that his website should feature one of those warning labels that says, "Caution: Contains Nuts".)
This seems that ESA is facing against the powerful democratic way which is the WEB where everybody is the witness of his taxpayer.
Rodolfo
Pillinger, duh!
I mean, a Beagle-2 RINGTONE?!?
Venus Express Commissioning Phase Completed
Paris, France (SPX) Jun 12, 2006
After 207 days of flight, 43 orbits around Venus and many test activities, Venus Express formally completed its commissioning phase June 3 and entered the routine science phase, ESA announced last week.
http://www.spacedaily.com/reports/Venus_Express_Commissioning_Phase_Completed.html
B)-->
This is encourgaging, but the time lag can be disheartening. It would be helpful to have access to all of the Huygens data by now...who knows - something in the data might have pushed a Titan/Enceladus mission ahead of Europa on the wish list...
Ad astra per bureaucracia.
Cannot avoid to firmly agree with you, Don.
I think we european tax payers should be hungry about this stupid policy!
There are two interesting articles in the http://www.blackwell-synergy.com/toc/aag/47/3: "http://www.blackwell-synergy.com/doi/abs/10.1111/j.1468-4004.2006.47313.x" by Andrew Coates and "http://www.blackwell-synergy.com/doi/abs/10.1111/j.1468-4004.2006.47316.x" by Peter M Grindrod and Trudi Hoogenboom.
Note for those who don't subscribe to A&G: The full Grindrod and Hoogenboom article can be downloaded http://www.homepages.ucl.ac.uk/~ucfbpmg/docs/paper_5.pdf.
'Report for Period 11 June to 17 June 2006
During the reporting period, Venus Express experienced its first Safe Mode since launch. This occured on 12 June, DoY 163, at the end of a data recovery action due to a ground station problem on DoY 162.'
http://sci.esa.int/science-e/www/object/index.cfm?fobjectid=39400
New press release today.
Double vortex at Venus South Pole unveiled
http://www.esa.int/esaCP/SEMYGQEFWOE_index_0.html
In case there were any other morons like me who couldn't "get" the double vortex, you're only "seeing" the night-side half of the vortex in the pictures on ESA's webpage. The dayside half of the vortex is washed out!
EDIT: *sigh*, nevermind. I'm a moron (see above)
I sorted out the images at different wavelengths by date and put them on to a page here:
http://www.planetary.org/explore/topics/venus/venus_southpole.html
One strange thing: According to Hakan Svedhem there were six "slots" in which they could perform imaging, and most of the releases show six views of Venus' south pole. But in the "movie" that they released of the 5-micron image data, there is a 7th image (I think the second-to-last image in the sequence might be the extra one?).
Thanks for gathering the images up on your blog. VIRTIS looks like it could reveal a lot more about the circulation of the atmosphere.
It looks like there has been progress in numerical modeling of the atmosphere too: http://www-atm.physics.ox.ac.uk/main/research/posters2005/2005cl.pdf
From http://sci.esa.int/science-e/www/object/index.cfm?fobjectid=39464:
'Activities of Medium Term Planning 003 will start now with great focus on the Earth occultations season that starts on 11 July and will continue till the end of August.'
Monica Talevi just e-mailed me...There are news from Venus, stay alert:
"Have a look to website this afternoon: we are about to post a new science
release on Venus Express!"
Here it is...lots of nifty new animations!
http://www.esa.int/esaSC/SEM9A3XAIPE_index_0.html
Thanks for the heads up, ustrax! I'll be digging into these pictures thoroughly today...
--Emily
I realize now that these are the pictures that they said they'd release in association with their presentations to the 36th COSPAR, to take place in Beijing on 16-23 July. There's a http://www.cosis.net/members/meetings/sessions/accepted_contributions.php?p_id=170&s_id=2743. Wish I could be there but travel to China is a bit out of the question at the moment
--Emily
Does anyone have a feel for the mean polarity of the Venus atmosphere is, with respect to the Earths? O2 and N2 are nonpolar, but I'm not sure about CO2, and H2O is highly polar - so are many sulfur compounds and all acids...
Polarity could come into play in interactions with the solar magnetosphere and the solar wind...magnitoshear?
Venus Express is the first time a decent camera has been placed in orbit around Venus, which is very exciting. Exploiting the narrow near-infrared windows, VIRTIS should show new details about the atmospheric circulation, cloud formation, and perhaps surface vulcanism.
I believe it was the Australian astronomer, David Allen, who first realized that these infrared windows existed into the deep Venusian atmosphere (Nature, 1984). Images were taken by the Galileo spacecraft during a flyby, and Mark Bullock has done some intersting work using Earth-based astronomy to peer through these windows: http://www.boulder.swri.edu/recent/VenusSwRI_PR.html
I am also disapointed by the PFS failure. This provides added incentive now for JAXA to send Planet-C and hopefully answer some of the questions about the chemical makeup of the Venusian clouds.
OK, so now I have a question about the images and movies.
Looking at the http://www.esa.int/esaSC/SEM9A3XAIPE_index_1.html, the caption states: "The spacecraft was flying over the northern hemisphere approaching the planet, over distances ranging between about 39 100 and 22 600 kilometres from the surface. The images were taken at 365 nanometres, starting respectively 03:30 and 01:45 hours before reaching the pericentre." But if you watch the movie it looks like we are actually moving from one hemisphere toward the equator on approach. The shape of Venus Express' orbit is such that you approach over the southern hemisphere, fly close over the equator and northern hemisphere, and then retreat back out over the southern hemisphere. And if you look at the orbit diagram (here's one I pulled from Hεkan Svedhem's VEXAG presentation), the times and distances do imply that we're looking primarily at the southern hemisphere, moving toward the equator, I think. Am I seeing this right?
--Emily
Emily, I believe you are correct. The "flying over the northern hemisphere" phrase in their press release is confusing. I believe the movie we are seeing is "upside down" and we are coming up from the south. BY the way, the orginal gray version of the movie is much clearer than the blue-colored one.
Bob is right too. In the original Bullock image, the bright regions are thin spots in the clouds, where heat from the surface is shining through. That goes for the VIRTIS images too, I believe.
I think ESA is following the standard NASA algorithm for how to ruin a beautiful space image:
step 1. Expand the contrast until light and dark areas pop.
step 2. Apply a Laplacian sharpening filter until noise artifacts are prominant.
step 3. Enlarge the image with a nearest-neighbor filter, so pixels are big and square.
step 4. Pick an ugly primary color, like orange or purple, and colorize the image.
Just to illustrate, here is the original Hubble image of Venus, and the one released to the press:
[attachment=6650:attachment] [attachment=6649:attachment]
A meaty new http://www.esa.int/esaCP/SEM9A3XAIPE_index_1.html is now online at the ESA site. It includes several animations and a wealth of science findings.
In one of the early Venera-13 papers, the Russian authors discussed the need to apply the inverse method (solving an integral equation) to correctly create RGB color from sensor inputs. They knew their math and radiometry, but didn't have easy access to computers to do it. In the West, you have the opposite -- big computers and relatively ad hoc image processing. I don't believe the colors in any of NASA's images, even when they are not "false".
I'm not sure these guys even know about the sRGB standard. If you know the spectrum of a color, there is a clear algorithm for creating a 24-bit color value. That's fine for some of the latest cameras that record huge spectral image cubes. But if you have signal levels from several sensors, with various spectral responses, then the problem of deriving the maximum-likelihood color value is nontrivial.
Malmer, I was impressed by how you processed the Mariner-10 images, calibrating the sensor weights with Mariner's Earth images.
i actually ended up relatively close to the responsecurve that where in that paper you sent me...
VMC is kind of a primitive camera (http://www.mps.mpg.de/projects/venus-express/vmc/), but that doesn't mean it won't spot something interesting. I think VIRTIS is a more sophisticated experiment, but probably won't take as large a volume of images as VMC. As for learning what the UV absorber is, I'm afraid that rested with the PFS. Its failure cost them the chance to learn a major new thing at Venus.
I think there is one other major new things that VEX could discover -- IR images of active volcanism on the surface. That would be incredibly exciting.
Assuming <I hope otherwise> that the PFS stays disabled, there could be a real opportunity to fly a backup/flight-spare/engineering-model of the instrument on the Japanese Venus atmosphere orbiter mission. It's moderately well along the design development cycle, but I suspect that it's not too late to refly the PFS on that mission.
What guarantee do we have that the backup wouldn't fail the same way this one failed? Wouldn't it be wise to reevaluate the weak points in the design and improve it if necessary. Meaning additional costs?
Let me give a brief update about what I know regarding the publication of VEX science images and information, based on what I've heard over the last few days.
A major issue of Nature has been in planning for some time. It seems like it may come out in May, which would be nice since it would coincide with the one year anniversary of when VEX began routine science operations. Since most efforts now are focused on that paper, any other publications are unlikely until that issue comes out.
Getting more PR images out is getting pushed internally. I can't say that comments on this site have been taken into account, necessarily, but they are one factor that has been brought up in discussions. What I'm hearing now is that another PR person has been brought in at ESTEC to help Monica Televaes, and they are hoping to do the following:
- upcoming web stories in the end of March, 11 April and end of April.
- More information on the Ground based observations campaign will be coming up. There is a process in place to coordinate ground coverage of Venus during VEX observations, with the amatuer community.
-Try to do one web story per month, with one team each month.
-Try to put out more images in general.
It is possible they may fall short of this, but they are at least going to try it.
Cheers-
Don Merritt
They are rapidly approaching the first scheduled PSA release of VEX data - but we've seen it all before with Smart 1 so I'm not holding my breath.
Doug
Don, I could not appreciate your reports more. Thanks so much.
And we'll likely see that amateur data before we ever see any VEX results... *sigh*...
Unless the VEX Science Operations Team is putting all this together to try and keep the *amateur* data secret, too??? (OK, I'm not really serious about that. I don't think...)
-the other Doug
The problem is that the amateurs almost certainly will only have acess to their own data so these coordinated ground based observations are unlikely to reveal much that is new without the corresponding VEX data.
However this is a really interesting effort and I'm very happy to see that ESA is also doing this - it seems to be similar to the collaboration with the amateur Jupiter observing community that NH benefited from during it's recent flyby.
And I'd like to thank Don for his updates - they very much appreciated.
For those of you interested in the Venus data that amatuers are submitting to ESA,
the Venus Amateur Observing Project page is at:
http://sci.esa.int/science-e/www/object/index.cfm?fobjectid=38833&fbodylongid=1856
You can click on "Results and Observations" in the right sidebar if you'd like to see some of the results so far.
Cheers-
Don Merritt
VEX Mission Ops Reporting, 11 - 17 March
At the end of the last CEB pass in the reporting period (DOY 076, 18:00z) Venus Express was
orbiting Venus at 195 million km from the Earth. The one-way signal travel time was 652 sec.
The Attitude and Orbit Control System (AOCS), power, thermal, mechanisms and fuel system continue to operate extremely well. Continued kudos to Astrium, and the flight control team at ESOC.
We did not receive a small amount of science data last week, because high winds at the Cebreros ground station required the antenna to be safed. That data was stored on board, and has now been downlinked. The data is transferred from Cebreros to a server at ESOC, in Darmstadt, Germany. Our science teams pull their data off of that, knowing that the data is not final for at least a week or two after the actual downlink, just for such occurences. This recent data delay will not cause any problems. The Cebreros station is new, the schedule being driven primarily by VEX support requirements; it still has that new ground station smell. There are occasional problems with equipment or procedures, but just the usual small stuff one would expect.
VIRTIS movie passes are scheduled for the second week of April (DOY 98-101). This includes five orbits, where the mission constraints allow us to take extended mosaic images of the south pole from apocenter. Planning of science operations during this event is now finished. A proficiency pass is scheduled on DOY 078
with DSS-63 (Madrid 70-m DSN antenna) to test system readiness for this activity. Being able to use the DSN 70-meter antenna means that it greatlly increases our data rate. Using the DSN station in Madrid, located in the 'same' spot as the Cebreros antenna, means that we do not need to make any changes in our usual orbit timing; we'll be downlinking at the same time as we would have if we had used the Cebreros station. We have made regular but limited use of the DSN stations; in the past, it was only for radio science observations. NASA has been very helpful in this regard; ESA isn't charged for the time, but on the other hand we get whatever time is left over. We put in requests; if no one else needs that antenna at that time, they give it to us. We are always in a position to get bumped, but it hasn't happened yet. So it is great that we get the time, as ESA doesn't yet have any 70-meter dishes.
The science planning for the 14th month of operations (MTP014) has been completed, and final checks are to be done shortly at ESOC in Darmstadt. The science planning for MTP015 has also been completed. Spacecraft pointing requests have been approved by Flight Dynamics, and the flight control team received the instrument commanding files last Thursday for their final checks. I sure hope they work. This set covers the second half of our quadrature period, and the special and special Messenger Fly-By support observations.
We've been so busy, time has flown by. But 11 April 2006 was the day we got to Venus, so our first anniversary of Venus operations is almost here.
Cheers-
Don
Venus Express: One Year In Orbit
On 11 April 2006, VEX went into orbit around Venus. The ESA Science web page contains an article about it, which focuses on the oxygen airglow which is being investigated. The page is at:
http://www.esa.int/esaSC/SEM26GLJC0F_index_0.html
Nice, finally some new images and a cool movie!
It seems like this glow would be invisible to the eye. My mind leaps for an explanation for the ashen light, but it will probably end up being an optical illusion, not a real phenomenon.
VEX Mission Status
As of 14 April, Venus Express was orbiting Venus at 169 million km from the Earth. The one-way signal travel time was 564 sec.
From 08 April through 12 April, a series of special mosaic images of the south pole were taken with higher than normal resolution. The amount of data would exceed the capability of the nominal ESA ground station at Cebreros, Spain. The data was instead downlinked via the DSN 70-meter Madrid station, under a cross-support agreement between ESA and NASA. This South Pole 'movie' should show excellent coverage and detail of the south polar vortex.
was interesting to note that the brand-new Cebreros 35-meter antenna was 'shadowing' the DSN 70-meter, with no margin built in, and had as good a data rate capture as the much bigger DSN antenna. Which seems to indicate that the DSN 70-meter dish needs a little maintenance.
Some data was lost on DOY 101 due to bad weather in Spain. The data was recovered due to the shadowing with the Cebreros antenna. And all of us in Holland were glad to hear about bad weather in Spain.
Quadrature period begins in May. During this period, the spacecraft will switch to our smaller high-gain antenna, sharply reducing our data rate. The VEX bus is designed so that only two of the eight faces can be exposed indefinitely to the Sun. In the quadrature phase, we would get Sun exposure on the prohibited faces during Earth communications, which lasts at least eight hours per day. The spacecraft is then flipped, and Earth communications is done via the smaller high-gain antenna to keep the Sun exposure only on the allowed faces. The spacecraft is designed for this situation, but this is the first time in the mission we have been in this quadrature situation, so a lot of details on the ground have needed to be worked out and verified. The Flight Control Team at ESOC, in Darmstadt Germany, have been working on it for a while now, and final testing of the changes are underway now. The science planning for this period was wrapped up some time ago.
All spacecraft systems continue to operate nominally, with the occasionaly hiccup just to make sure that people are paying attention.
Much appreciated update Don.
New VEX Science Information Released
On the ESA Science page at: http://www.esa.int/SPECIALS/Venus_Express/
there are two new releases that you might find interesting.
The first shows some great 'movie' images taken by the VIRTIS imaging spectrometer of Venus' south pole. Combining the IR images with a UV image of the dayside, you can see the full rotation of the south polar vortex. Over a period of five orbits, VIRTIS took images centered around apocenter. The page strings them all together, so that you see the five or so shots from one orbit, and the sudden jump is when the data jumps to the images from the next orbit. You can really see the change in the cloud structure over time in the vortex.
Just released is an article about ground-based observations that will be taking place in coordination with VEX. This will extend up to the Messenger Fly-By in early June, when we will be (sort of) simultaneously taking data from Messenger, VEX and the ground.
Over the next few months, Venus will be around its closest distance to Earth (inferior conjunction). Planning began this week for late August through late September, slightly past conjunction, and during that period we'll also be coordinating VEX observations with some ground observations:
- Infrared observations will be made by the Infrared Telescope Facility (IRTF) facility in Hawaii, USA.
- Sub-millimetre observations will be made for two days with the James Clerk Maxwell Telescope (JCMT), located in Hawaii, USA.
Venus Express Status
At the end of the last Cebreros pass in DOY 132, 18:00z, Venus Express
was orbiting Venus at 139 million km from the Earth. The one-way
signal travel time was 463 seconds. We are approaching inferior
conjunction, when Venus will be between Earth and the Sun.
The Venus Express spacecraft has been operating nominally, with only
relatively minor exceptions. One of these was a problem related to an
anomaly where a thruster failed to close. The thinking on that is
its "probably due to a missed pulse in the commanding
circuitry". I'd feel better if I knew what that meant, but even then
it would still mean that we don't know. We haven't seen a repeat, and
the best spacecraft problems are the ones that fix themselves.
With the installation of a flight software patch and the update of the
on-board ephemeris, Venus Express was configured for the quadrature
phase. This phase is defined as the period during which the
Sun-Spacecraft-Earth angle is between 75° and 95°.
During the quadrature phase, revised operating constraints on the
VMC camera lead to the necessity for changing the spacecraft attitude to
prevent unacceptable illumination of the VMC camera. To this end, fake
ephemerides on the positions of the spacecraft and the Earth were
uploaded to Venus Express.
On 11 May 2007, for the first time, Earth pointing was achieved
using fake ephemerides with a Sun illumination of ~10 degrees on
the +Y spacecraft face. The first pass with a tilted attitude was
closely monitored by the Flight Control Team (FCT). No anomalies
related to quadrature operations were detected and the performances
of the system was nominal. The flight control team and flight
dynamics teams at ESOC, in Darmstadt Germany, spent a large amount
of time and effort in planning this 'quadrature' exclusion period,
but it all looks good now. We're in Quadrature, in the
exclusion period, and it is all working perfectly. The ESOC flight
control and flight dynamics teams are very good.
Later in the quadrature phase, a swap to the smaller High Gain Antenna 2
is required for Earth communications, as the spacecraft attitude for
continued use of HGA 1 would result in illumination of spacecraft
faces not designed to cope with such exposure. This is scheduled for
01 June, and will immediately drop our downlink data rate from 228 Kbps
to 28 Kbps. Its unfortunate that during inferiour conjunction, our data
rate has to drop so much. Re-using the Mars Express design allowed
the VEX mission to get funded, but one consequence is that the thermal
constraints force things like this.
It looks like we've had our first non-recoverable failure. It appears that
the S-Band downlink path has a problem which significantly reduces our
downlink power on S-Band. That's the bad news. The current indications
suggest that the problem lies in the path between the entry to the RF
switch immediately prior to the HGA 1 antenna, and the antenna itself.
The good news is that radio science, which used to rely on having both
the X-band and S-band downlink, can now use only the X-band downlink
along with models of the Earth ionosphere (which replaces the need for
the S-band signal). There is still a lot of work being done, to try and
figure out exactly what happened, and more importantly, why.
Some delays have been encountered in the data deliveries for ingestion
to the archive, but a first release of (a subset of) Venus Express
data in the Planetary Science Archive (PSA) is still expected for
this summer.
The preparations for a special section on Venus Express results
(some 9 papers), to be published in Nature, are ongoing.
Planning for our sixteenth monthly medium-term plan of operations (MTP016)
are completed. We are just now finishing MTP017, and MTP018 planning started
this week.
http://www.esa.int/esaCP/SEMLYY8RR1F_index_0.html
European Space Agency
23 May 2007
You're right. The PFS instrument
(http://sci.esa.int/science-e/www/object/index.cfm?fobjectid=33964&fbodylongid=1444)
never worked. The mechanical scanner is stuck.
I guess I don't count that because technically, they are still trying to free it. The flight control team is working with PFS to do a test shortly where they try to move it while we are doing a burn. Which is trying to kick it and turn it at the same time.
We don't hold out much hope. But one never knows.
There was some discussion about getting data down from spacecraft, and frustration with the amount of time it takes. I think I finally figured out how to post images, so I'll put up a couple examples from VEX to show how this stuff gets downloaded.
When we do our planning, our ESA proprietary simulation tool will create a prediction of how much data the instruments accumulate each orbit, as well as how much we are able to downlink during each comm pass with the Cebreros Station in Spain.
The resulting up-and-down graph looks like this, for our 18th monthly plan which I just finished:
hi cndwrld
thanks for providing a window into the dataflow workings
"There was some discussion about getting data down from spacecraft, and frustration with the amount of time it takes. I think I finally figured out how to post images, so I'll put up a couple examples from VEX to show how this stuff gets downloaded.
When we do our planning, our ESA proprietary simulation tool will create a prediction of how much data the instruments accumulate each orbit, as well as how much we are able to downlink during each comm pass with the Cebreros Station in Spain."
Is the storage capacity on V.E. heavily-burdened?
As to transmission back to earth, I wonder if there could be a software on the spacecraft similar to the program that updates a web page, looking for numbers that change. For example, once a normal temperature range in a given area over a given time period has been established, the craft prioritizes data that appears outside the norm for sending back to earth.
Similarly, I've wondered how "smart" the Mars orbiters can get as they "pushbroom" their way around the planet. Perhaps they can automatically notice small changes like new gullies.
>>Is the storage capacity on V.E. heavily-burdened?
Well, yes and no. The instruments (particularly the imaging spectrometer VIRTIS and the VMC camera) could take much more data than they do. We are usually limited by our data rate, and our ground contact periods, not the SSMM volume.
>>I wonder if there could be a software on the spacecraft similar to the program that updates a web page, looking for numbers that change.
I'd see two problems with this. First, it only would work with housekeeping telemetry, not with science data. And the housekeeping is much less in volume than the science data. We dump a fixed 216 Mbits per orbit for housekeeping data; we dump about 4200 Mbits per orbit of science data. It might be a useful idea in some circumstances, though. Say, on spacecraft on long duration missions in cruise phase, where all you have housekeeping telemetry and no science, or commercial spacecraft.
Two, you'd only get data when it changed. But in that case, if you are looking at telemetry to find a problem, you would have to trust the numbers you don't have. You'd have to believe that if no data came down, that everything was working and the number you got last week is still the number you have now. I would have real trouble doing that. In my experience, data that doesn't exist has an unknown value, and the item generating the data doesn't work unless it proves it works by putting out data. Things 'fail silent' all the time.
Again, though, in certain circumstances, it might be useful.
VEX Status, 22 June 2007
At the end of the last Cebreros ground station pass on DOY 167, 18:00z,
Venus Express was orbiting Venus at 97 million km from the Earth. The
one-way signal travel time was 323 sec. We are executing our 15th monthly
plan, MTP015, and beginning the first week of MTP016 next week. We are still
operating on the small high-gain antenna, HGA2, due to Sun angle on the
spacecraft during Earth Pointing.
We are currently in the Quadrature Period, meaning that the angle
Sun-Venus-Earth is less than 90 degrees. Only two faces of the spacecraft
can take long-term solar exposure, +X and +Z. During parts of this
Quadrature Phase, these two faces can only face the Sun if we point with
the smaller antenna. So our data rate, when we are closest to Earth, is
pretty low. Kind of counter-intuitive, one could say.
During short periods of Quadrature, near the beginning and end, when in
normal Earth pointing the +Z face of the spacecraft (the one with all the
instrument fields-of-view) was too close to the Sun. We want to prevent light
falling in the VMC camera field-of-view, as they don't have a shutter and found
out after launch that direct sunlight on their camera CCD causes degradation
to the plastic lenses. So for the past few weeks, we were operating with a
10 degree roll whenever we were in Earth pointing, to keep the Sun out of
the VMC field-of-view. For a spacecraft with tight pointing requirements and
precise pointing systems, it was not easy to find a way to make it continually
position itself 10 degrees off what it knew to be correct. But the team in ESOC
in Darmstadt figured out how to do it. Last week, we finished our need for this
offpointing, so we are back to normal pointing modes now. Still on the darn
small antenna, though.
No new problems have developed lately. Flight control systems and power are
fine; still have plenty of gas. Some instrument glitches occur now and then,
but nothing too worrisome. VIRTIS did a big upload to their instrument to
update their operating system and take care of some small errors they were
getting. The PFS instrument, stuck since launch, is going to be operated
during some momentum wheel off-loadings, when the thrusters are fired, in
the hope that moving it and kicking it at the same time might jar it loose.
The other earlier problems have not gone away: S-band downlink is way too
weak due to expected thermal damage on large antenna or cabling; thruster
abnormal firing which occurred but has not re-appeared; SPICAV shutter
gives odd readings now and then. But nothing new lately.
The radio science experiment team was able to do a Bi-Static Radar test last
week. This is where we turn on a special, ultra-stable transmitter, point the
big antenna at a feature on the surface, and blast away at full power at such
an angle that the reflected signal goes towards Earth, where it is usually
captured at Europe's antenna at New Norcia, Australia. The geometry between
Venus Express, a surface feature of interest and the ground station have to
be just right in order to do it, so we've only done five or six of these so
far in the mission. With low staffing, data analysis has not been what you
would call timely. Upcoming BSR observations have been cancelled because
they have discovered that the latest BSR data are significantly different
from what was expected and won't give them the information they need. It
will take a bit of time for them to figure out what to do next.
All the data from the Messenger fly-by support is on the ground, and being
looked at. We hope to see some press releases soon. The ground-based
observing campaign will be ending soon, as Venus moves further away from
Earth. We had a bit of a panic last week with the Moon's occultation of
Venus. One of our team realized that our downlink files didn't take the
occultation into account, and there was much rushing about. Turns out that
the occulation occurred in The Netherlands and Germany, but the Cebreros
station in Madrid was just outside of the occulation area. Which is why the
files didn't take it into account.
Planning began this week for two monthly plans in parallel, meaning double
the work for us and the instrument teams for the next four weeks. But we
are doing this because most of the teams take a month off for the summer
holidays. We'll work harder for a month so they can take a month off. I
think most of our team will not take a lot of time off during the summer.
Since none of us have kids, we can take our holidays outside of the rush
period in the summer.
In this planning period, we are introducing a new type of pointing that our
software will now support, called 'track pointing'. We should be able to
give a start time, and end time, and the lat/lon/elevation of a point, and
the spacecraft will track the point. Or we can give it
the name of a astronomical object in our database, and it will track the
object. I say that we should be able to do these things. The software has
a few 'issues' that were discovered recently, so we are going to just
allow a couple of them in each of the MTPs we are starting to plan now.
We'll see how it goes. If it works, though, it will probably get heavily
used.
In summary, things have not gotten calm and boring yet, we're doing a lot
of science that people can whine about not seeing but which should be more
published soon, and the spacecraft is doing well. Our next Science Working
Team meeting is near Rome in July, and I'm going to stay over an extra
day to finally go see the Pantheon, and the remains of the Venus temple
in the Forum. I'll pay my respects to Venus while I'm there.
Yes, that answers a lot of my questions -- thanks! I guess one thing I was wondering was whether a dozen, or a hundred, little (like half- to one-meter) dishes on the ground could be used in a sort of an "antenna farm" mode to simulate a 70m or larger receiving antenna.
You see, there are literally hundreds of thousands of people here in the U.S. who have at one time or another used a satellite cable system (like Dish Network) but who no longer use that service. That's a lot of parabolic dish receiving antennas that are just going to waste.
If all of those unused dishes were mounted with decent views of the ecliptic (where most of the unmanned probes spend their lives) and tracking mounts, and set to communicate to a central data collection center, we could have a "distributed" DSN network made up of thousands of dishes. And heck -- some of them could be tracking Venus, some Mars, some Mercury, and some Saturn. And some tracking points in between.
I know it's probably a foolish pipe dream, but it would seem that you could vastly expand the DSN (within North America, at least) at relatively little overall cost (certainly at relatively little cost per dish) by making use of these unused dishes.
Your response tells me that such a network of dishes could be useful for getting additional science out of the assets we have in place around the Solar System. That's the information I was looking for. Now all we have to do is find the seed money for outfitting these unused little dishes, and we can get started...
-the other Doug
An upgrade for the DSN based on arrays of modest ( <30m but >1m ) sized dishes is under serious study - with a test dish being used at JPL - (I think it's 12m).
Doug
VEX Mission Status
Quadrature is the period when the Earth-Venus-Sun angle is less than 90 degrees, which includes inferior conjunction. At the start and end of quadrature, we have to undertake special operations in order to avoid Sun exposure into the VMC instrument which has no shutter. On 16 June, the spacecraft's 10° +Y tilt was removed at the end of the first quadrature transition period.
Removal of the 10° +Y tilt was removed by execution of previously
uploaded commands, just prior to start of the Earth communications pass.
It was done this way so that the spacecraft orientation could be checked
immediately upon the start of communications with Earth, and time for the
science downlink would not be used to observe the orientation change.
Routine observations took place during this reporting period, and
occurred as planned. A full VIRTIS software upload was carried out
including the related testing on DOY 165 and 166.
On DOY 167, the telemetry bitrate changed to 45 kbps.
At the end of DOY 167, Venus Express was orbiting Venus at 97 million km
from the Earth. The one-way signal travel time was 323 seconds.
Payload Activities have been routine. Two VeRA radio science occultation
observations were performed using the ESA New Norcia antenna in Australia
on DOY 164, 166, 168, 170 and 173. For these observations, a highly stable
local oscillator is used to generate the downlink signal to Earth, a ground
antenna locks on the signal, and the signal is measured as the spacecraft
is occulted behind the planet. This is repeated when the spacecraft leaves
occultation and emerges from behind the planet. The spacecraft is re-oriented
during the occulation to account for the diffraction of the atmosphere, to
maintain the link withe the ground station. The changes in the signal are
used to determine properties of a deep slice of the atmosphere. Since this
was in the quadrature period, the smaller high gain antenna was used, greatly
limiting the signal strength.
A VeRA Bistatic Radar observation was also performed, using the 70m Canberra
DSN station on DOY 163. In these experiments, the stable oscillator is used
for the downlink to the big high gain antenna, and the antenna is pointed at
a ground feature and tracks it. The reflected signal is detected by the Earth-
based antenna, which is why the large 70 meter DSN antennas must be used.
For the VIRTIS imaging spectrometer, a full instrument operating software
upload and related testing were carried out on DOY 165 and 166.
On DOY 170, a new on-board control procedure (OBCP) was uploaded for
SPICAV shutter operation. The OBCP is expected to automate the operations of
the SPICAV shutter. The shutter is closed when the instrument is not in use,
because exposure to direct sunlight would damage the instrument optics.
The commands have been inserted into the normal command uploads to the
spacecraft for shutter operations, but in the case of a spacecraft safe
mode the shutters would not have gotten closed and might have exposed the
instrument to hours of exposure in the worst case.
PFS spectrometer tests are being prepared to try to move the instrument's scanner during
a wheel off-loading (WOL). The instrument is non-functional due to a stuck
scanner. It is hoped that operating the scanner motor while the thrusters
kick the spacecraft might free the scanner. Hoped, but not expected.
Today I plotted out the fuel, oxidizer and helium pressurant since the start of the mission.
The state of the consumables is just fine, and VEX life will be limited by money much more than
by fuel. The plot below shows how much was used to get into orbit; since then, we've been using
very little. We've got room for some big orbit changes if it is decided to try something new.
Thanks for the update! I always enjoy reading them even if I don't always comment.
When will we know about the PFS?
PFS has delivered their inputs for the Scanner test during a wheel off-loading. The tests are to be run over 6 days, during the last three weeks of July.
They'll want to look pretty closely at the data for any signs of movement, and no one is in a hurry to announce bad news. So I wouldn't expect us to get any official word on the result until about mid-August. But that's just my guess.
Of course, if the thing actually moves, we'll hear about it in no time. This test is a Hail Mary pass, so I'm not holding my breath. Still, would be nice if it worked.
...so no news is bad news...
The ESA gets kudos for a brave, daring, and resourceful use of a 'hammer'
We have a bigger hammer in reserve. This test is during a wheel offloading, where we hold the spacecraft steady with thrusters while dumping the momentum from the reaction wheels. The thruster burns are quite small.
If this hammer doesn't work, they might do the same thing but during an orbit correction maneuver. An OCM is usually a bigger burn, proportional to the amount of delta-V(elocity) that flight dynamics decides we need to get back into our correct orbit.
It still seems unlikely to help. But what the heck. The PFS team is operating their instrument on Mars Express, but it isn't like their too busy to do this test. And the flight control team is probably starting to get bored. Can't hurt to try it.
So we'll kick it. And in the noble and honorable tradition of engineering, if it doesn't do what we want then we'll kick it harder. While calling it a naughty name.
PFS Still Non-Operational
The PFS scanner was commanded during recent momentum dumps (wheel off-loadings). Reaction wheels speed up in order to capture unwanted spacecraft momentum and maintain pointing; when the wheels are slowed back down to their zero level (generally once a day), thrusters are fired to hold the spacecraft steady. It was hoped that the physical shock of the thruster firings, performed at the same time the scanner was commanded to move, might jog the scanner lose.
However, kicking the scanner in this way didn't work. No more tests are planned, that I'm aware of. The orbit correction maneuvers, which I thought might be tried, turn out to be smaller than the wheel off-loadings. So trying them is not thought likely to help.
So, we'll have to see if the PFS team can come up with another Hail Mary pass, or if this is the end.
Thanks for the update, though I wish the news was better. I guess the problem with moving parts is that they sometimes aren't moving parts.....
I work on an ESA project, but I'm an American. I'm afraid I don't know any European sports idioms.
I was trying to think of what the football (soccer) equivalent of a "Hail Mary" would be myself but couldn't. I think this reflects the poor state of my sports knowledge and of European slang.
Thanks again for all your inside reporting, cndwrld.
I'm afraid I don't know any European sports idioms.
Try Sven Goran Erikson. Oh, sorry, idioms... I thought you said something else...
Based on a casual Google, perhaps ESA might consider launching the aforementioned individual on a purely ballistic intercept trajectory with VEX in order to jar PFS loose...didn't see a whole lotta love there, Stu!
Coordinated observations of Venus between VEX and Messenger
The ESA web page for the Messenger fly-by is now up, on the ESA Space Science page, at
http://www.esa.int/esaSC/index.html
If you click on the third story, labeled, "Venusian rendezvous results: chapter one", you go to the dedicated fly-by page at:
http://www.esa.int/esaSC/SEMVN4HYX3F_index_0.html
The fly-by page can also be reached from the dedicated Venus Express page at:
http://www.esa.int/SPECIALS/Venus_Express/index.html
500 days at Venus, and the surprises keep coming
http://www.esa.int/esaCP/SEMNOCMPQ5F_index_0.html
...Some of the first detailed analyses are now being completed and will soon be published in acclaimed scientific journals...
Venus Express Status
At the end of the last Cebreros pass in the reporting period (DOY 251, 15:00z) Venus Express was orbiting Venus at 52.0 million km from the Earth. The one-way signal travel time was 172 seconds.
Overall, the spacecraft is performing well, and most of the instruments are working great. During MTP 018, which is finishing this week, we completed 500 orbits and have sent to Earth around 1 Terabit of data so far.
Of the four science operations engineers, two are now moved to the European Space and Astronomy Centre near Madrid, Spain. Another will join them in October. And I expect to move down from The Netherlands sometime in January. Within the next half year, all of ESA's planetary science operations, as well as their astronomy science operations, will be based at ESAC, Spain.
on 23/08/07, DOY 235, we performed an S-Band test. As you may recall, our S-Band downlink on the main antenna HGA-1 is very much reduced in output. Tests had earlier shown that the problem was definitely in the HGA-1; these tests confirmed that it was in the antenna itself, but there's no telemetry on the antenna. It is possible that some physical deformation took place, but anything is just speculation. 14. VMOC has scheduled a mapping and calibration of the S-Band downlink, which will occur in MTP021. The calibration put out a carrier over the S-band HGA-1 output, and slew the spacecraft back and forth past the Earth. Since the downlink is so reduced, we will need a 70 meter antenna to pick up the carrier very well, so we will do the test using the Canberra DSN to capture the downlink signal strength. We can then look for distortions in the signal pattern.
The S-band calibration slot is currently scheduled for Orbit 584, DOY 330, on 26-Nov-07 between 00:30 and 04:00Z.
It will take place over the Canberra DSN antenna, towards the end of the visibility period and coming up directly before the Cebreros AOS. It will occupy the pericenter arc, with some margin due to its relatively long duration (3hr 30min).
The calibration is HOT (sun exposure on sensitive faces), and so there can be no hot observations prior to it in orbit 584 and we must be thermally recovered from any previous observations. The recovery time from the calibration is covered within the following Cebreros pass, which will allow hot observations to resume as normal in Orbit 585. The VMC camera was approved for observations during the antenna calibration, as the +Z axis will be pointing at the planet.
We need the S-band for bi-static radar observations. That's where they point the big antenna at the surface of Venus, blast out the carrier signal (but in a very stable oscillator mode) and catch the reflections on Earth using a DSN antenna. Without the S-Band, they can't correct out for the Earth's atmospheric distortion. They thought they could use models to do it, but I guess it didn't work out as well as hoped. In the mean time, we aren't doing any BSR observations. Since we seldom get the right geometry to do them, we are not missing many. But then again, there aren't many to miss.
On August 23rd, the spacecraft came into view at the Cebreros station bearing bad news. There had been some type of problem wtih a solar array drive motor, during the observations, and the system had switched to the B side units. The spacecraft controllers and engineers cleaned it up and reset everything. Now they needed to figure out why it happened, since the A side stuff seemed to be just fine.
They didn't have long to wait to get more data. The next day, on 24/08/07, DOY 236, VEX came back into Earth view with the same problem, only worse. The solar array drive electronics (SADE) showed a motor with a failed status and a mispointing between the two solar panels. The control team manually switched off all the payload and as much power-sucking stuff as possible, and cleaned it back up again. Given that it happened twice in two days, the spacecraft left Earth pointing and with payload off until it was figured out.
This is believed to be related to a known MEX anomaly, which uses the same motors and electronics. The anomaly testing was completed, after a couple days of the spacecraft being left Earth pointing with the payload off. The solar panel pointing has been successfully corrected. I haven't seen a full report on the problem yet, but it hasn't come back.
In other Payload Activities, the ASPERA nuetral and charged particle detector, MAG magnetometer, SPICAV stellar/solar spectrometer and VMC camera seem to be working well.
And the VIRTIS imaging spectrometer? Well, not so much. Virtis is in two wholly separate parts: the M and H instruments. The M instrument has a large field of view (FOV), the H a very small one. They both need to be cooled prior to use of the IR detectors, and use motors to move the cooling fluid around. It was noted by the Flight Control team that one of the motor telemetry channels went out of limits. And that is when they noticed that the cooler motor currents had been fluctuating wildly for some time, just not out of limits. A test that included the VIRTIS H cooler was performed on DOY 251. Otherwise only Virtis M part has been operated during this period as the failure on H cooler is still under investigation. And since the cooler motors are the same, M is operated in a somewhat limited mode. So far, it seems that the M motor is not effected. Testing on the H motor continues, to try and characterize it. The Virtis instrument team is really good, so we trust them to do a good characterization, and we'll see if we can do anything or not. We can run the motor the way it is, of course. But once it fails, no coolant motor means no coolant, which means no crycooler cooling, which means Virtis-H IR detector data.
To summarize, things go well but not perfectly. Keeps it interesting.
Nature Papers
On 29 November 2007, a special issue of Nature magazine will highlight the first major papers from each of the instruments on the Venus Express mission. A press conference is planned for 28 November to highlight the release.
Should be a great issue.
Hooray hooray hooray! According to what Hakan Svedhem told me, waiting for this publication has been a logjam that prevented more science from coming out (not necessarily by press releases, I mean as presentations by scientists at meetings). It will be a great relief to see some Venus Express results in publication.
cndwrld, does your posting of this date mean that all of the teams have gotten their papers submitted?
--Emily
Yes, my understanding is that everything is in, accepted and ready to go. Given the history of this issue, I wouldn't say that nothing can go wrong now. But we hope that it is finally going to happen. Three months into the Extended Mission, it would be nice to see something published....
Venus Express Status on 30 October 2007
For those interested, here's an update on Venus Express. The Flight
Control Team publishes regular updates on the web at:
http://sci.esa.int/science-e/www/object/index.cfm?fobjectid=41488
The Main bus activity last week, on mission day 710, 19/10/2007, DOY 292
was the switch to quadrature offset (tilted) operations by the loading of
fake ephemereids. The process was fully automated following the
experience of the quadrature entry. For a two week period when
the Sun-Venus-Earth angle is 90 degrees, the Sun can fall directly
into the VMC field of view, which has no shutter, when we are Earth
poinging. The spacecraft needs to be rolled 10 degrees and maintained
there when in Earth pointing, which was not a planned state when the
spacecraft was developed. To do this, fake information (ephemerides)
are loaded; the spacecraft uses the same positioning system, but the
references are shifted by 10 degrees. The fake ephemeris was applied
after the science observations, and just before the acquisition of signal
(AOS) at the Cebreros ground station near Madrid. This 10 degree roll
also means that the Sun is kept for very long exposures on surfaces
that we normally keep cool. This means that for two weeks, our Earth
pointings (which should be cool and allow us to cool down) are hot
(so that cooling takes place during the normal science observation
periods). It is all quite messy, but doing it the second time was
much easier. We are in the transition to exit the quadrature period,
and only have to do this for a couple weeks.
We also switched from the small high gain antenna (HGA-2) to the bigger
one (HGA-1). The smaller one has to be used during quadrature because
of the Sun exposure angles on the spacecraft, to keep the Sun off of
the cooling arrays. Now we're back on the big dish, so our data rate
goes up. That's always a good thing. The TM bit rate starting on Orbit
549 (22-Oct-2007, DOY 295) was 38 Kpbs. After the antenna swap,
the bit rate went to 228 Kbps. But as Venus will be moving away
from Earth now, our data rate soon begins dropping a lot. The low point
comes in about May 2008, when we hit Superior Conjunction.
At the end of the Cebreros pass on Orbit 548 (21-Oct-2007, DOY 294),
at 18:00z, Venus Express was orbiting Venus at 94.6 million km from
the Earth. The one-way signal travel time was 315 sec.
The operations of the VIRTIS imaging spectrometer were disabled for the
past month. Really unusual currents in the cooling motors was detected
last month by the Flight Control Team in Darmstadt, Germany. To be safe,
the instrument was shut down except for unusually interesting
observations. The Virtis team in Frascati (Rome) has worked with the
motor manufacturer, and new procedures to use the motors were developed.
After which, the manufacturer changed their minds and decided that the
old procedures were better and safer. Operations are expected to
resume next week or the week after.
The rest of the instrument observations have been taking place routinely,
with the occasionaly glitch here and there.
Current NTO (Oxidizer) Mass (Kg): 46.761
Current MMH (Fuel) Mass (Kg): 29.514
During the NASA Phoenix mission's final approach to Mars, ESA will
support NASA by performing Delta-DOR measurements in order to get the
best positioning data possible. Venus Express was used as a test of the
Delta DOR procedures at the end of September and early October,
performing three Delta-DOR tests. The results show that we are still
at Venus.
The special issue of Nature magazine on Venus Express results is
expected to be published on 29 November, and should be accompanied by
a press conference the day before. The last paper was accepted
yesterday, so it should be all finalized. However, it has taken so
long to get these papers submitted that I'll believe it when I get
a hard copy in my hands.
The VEX teams are starting to get pretty good images of the surface
of Venus, through the frequency 'windows'. Hopefully a few web images
will come out before too long.
There are four science operations engineers working on Venus Express.
As of last week, three of the four have been re-located to work at
The European Space Astronomy Centre (ESAC) near Madrid. The fourth
engineer (me) will be moving at the end of January. All the ESA planetary
science operations will soon be based there. As a consequence, the
facility's name is expected to change, to The European Planetary and
Space Astronomy Centre (EPSAC).
Thanks for the update, CND. Sounds like good things are coming in about a month...looking forward to the surface imagery! Will be interesting to compare it to Magellan radar data.
There are a few things still orbiting Mars that we do not hear from either;)
I'm at ESTEC now, in Holland. And I am definitely going to miss this place, both ESTEC and Holland. The Netherlands is a wonderful place, Leiden a beautiful, fun town.
I can't afford to live in Madrid, so it will be nearby. If Spain and the new town aren't wonderful, too, 'll be very upset.
Stellar Occultation Studies at three planets
The Principal Investigator for on of the Venus Express instruments has written a short brief about the use of stellar occulation measurements being performed by European spacecraft now at three planets: Venus, Earth and Mars. You can read the release at:
http://www.esa.int/SPECIALS/Venus_Express/SEMEH3FWB8F_0.html
Eleven VEX Papers On-Line
On the ESA Science and Technology page for Venus Express, eleven papers have been put on line. They cover the seven science instruments, the spacecraft, the ground segment and mission planning, science data handling and science planning.
They can be accessed by going to the VEX Science web page at
http://sci.esa.int/science-e/www/area/index.cfm?fareaid=64
and then clicking on 'Publications' under the 'Services' header at the lower left.
VMC surface images http://www.esa.int/esaSC/SEM57353R8F_index_0.html.
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