Europa Orbiter, Speculation, updates and discussion |
Europa Orbiter, Speculation, updates and discussion |
Sep 15 2005, 07:12 PM
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Member Group: Members Posts: 134 Joined: 13-March 05 Member No.: 191 |
There has been lots of discussion of a mission to Europa in the excellent thread on the Juno mission. I thought that since a Europa mission seems to be once again becoming a possibility, it deserved its own thread for news, updates and discussion. I thought I'd kick things off with a summary of past efforts on a Europa mission, and on where things stand now. If I make a mistake, please correct me!
In the course of its prime and extended missions, Galileo found evidence of liquid water under the icy surface of the planet. Planning began on a Europa Orbiter mission, with a projected arrival date of 2008, to confirm the presence of the ocean, characterize the thickness of the icy crust and identify places for a future landing. One thing to note about these earlier plans: they included a direct trajectory to Jupiter, presumably to minimize mission duration and qualms about RTGs re-entering Earth atmosphere after some (highly unlikely) targeting mishap. But NASA lacked a nice category of missions to place the Europa Orbiter in. Eventually it got lumped together with Pluto Express and Solar Probe in a Outer Solar System program labelled "Fire and Ice", a term which also got applied to the Galileo Europa Mission extension. Without a solid program to support it, (like Mars Exploration, Great Observatories, or Discovery) the mission looked like an orphan. As Bruce Moomaw has well documented, attempts to kill off the Pluto mission led to a tug of war between NASA, the planetary scientists and the public, resulting in Congressional directives to NASA. Pluto Express became the Pluto/Kuiper Belt Explorer and then New Horizons and New Frontiers 1. (New Frontiers 2 is of course Juno.) But the cost for the Europa mission continued to rise, and the launch date recede, as the difficulty of radiation shielding and the large delta-v requirements hit home, and the mission's public profile fell. The launch date moved to 2010 and the costs moved over a $1b. Then along came Sean O'Keefe and JIMO, a justification for the Prometheus program through developing nuclear electric propulsion, not with RTGs, but with an in-space fission reactor. Launch got moved to 2011, then 2012, while the cost went even further through the roof. With the arrival of Mike Griffin, JIMO was cancelled. As Griffin said to Congress, "It was not a mission, in my judgment, that was well-formed." But interest in a Europa mission remained and remains strong. In 2003 the National Academy of Science's Decadal Survey flatly stated that a Europa Orbiter was the top priority for the next Large scale (aka Flagship) mission. (See page 196 of the report.) NASA's current Solar System Exploration Roadmap reaffirmed a Europa orbiter as the next flagship mission. The question as always is money. As Administrator Griffin said, "The Science Mission directorate wants to do a Europa mission, the National Academy of Sciences wants to do a Europa mission, I want to do a Europa mission. When we can afford it in the budget, we'll do it." Evidence of that support beyond rhetoric and reports trickled out with a letter from Andy Danzler, NASA's Solar System chief, to the Outer Planets Assessment Group (OPAG). He reported that he had "funded a team to take a quick look at the boundary conditions of a mission to Europa, that is, how much power, mass, travel time, etc. for various realistic scenarios. For planning purposes, this group is looking at launch dates in the 2012-2015 range, although the later dates are more likely in terms of funding." For funding details however, we have to wait for the FY 2007 budget. OK, now the good stuff. The latest meeting of OPAG included reports on a Reference Design for the mission. A kind of first draft which establishes a baseline which can be tweaked and modified to extract the best science return. There are many things to like about this draft design: * The mission is now permitted to use Earth flybys, and uses a proven trajectory, the same as used by Galileo (Venus-Earth-Earth Gravity Assist). This allows a BIG increase in the available mass. * The orbiter uses RTGs, but not super advanced ones that require further years of development. * The orbiter is similar to Cassini in appearance, with 2 engines, a cylindrical tank structure, RTGs at the base, the magetometer boom at the top, and space for a lander bolted to side. The similarities may make it easier to convince Congress that this is something NASA knows how to do. The most obvious configuration change is with science payload and HGA having switched places, and the addition of a radar array. And there looks like a camera the size of MRO's HiRISE! * The mission is definitely Flagship in scope with a launch mass of over 7000 kg on a heavy lift launch vehicle. For comparison Cassini was 5712 kg at launch on a Titan IV, and Galileo was 2223 kg when launched using the Shuttle and an Inertial Upper Stage. * There is a good opportunity for ESA participation with the lander and science instruments. NASA/ESA co-operation is on the agenda for the next OPAG meeting. * The mission does not assume big upgrades to the Deep Space Network. If the Next Generation DSN does come along, that's just gravy. * Despite the Europa focus, the mission appears to give at least part of a Galilleo II style tour with multiple flybys of the outer Galileans over 18 months. Only Io will have to wait. The OPAG Europa working group is also expected to present further work at the next meeting in October. More details will emerge then. I think there is room for cautious optimism on this mission. While we won't be seeing a mission launch for at least another 7 years, the combined weight of the planetary science community does tend to get it's way in the long run. I think the momentum is finally starting to build. |
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Guest_BruceMoomaw_* |
Dec 4 2005, 06:41 AM
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QUOTE (mars loon @ Dec 3 2005, 02:43 PM) Bruce, what month in 2004 was that? Also, hard to say if you used the best approach with the editors. Did you consider 2 versions? one short, one long. In your opinion did they retain the best stuff? or would you have preferred alternate surgery? I/we can sympathize with your pain and torment. My MER story -- along with a 1-page piece on Stardust's comet flyby, during which I expressed my belief in a theory of the craters which I gather is still not proven, but still seems to me probable -- is in the April 2004 issue. Both then and this time, from the very first they warned me that the final article wouldn't be allowed to go over about 2000 words. I never dreamed I'd have such trouble deciding what to cut out. I was somewhat disappointed that the finished product for MER-A simply didn't include any news you couldn't have gotten from other articles on the subject, but with that short length you just couldn't do much else. The only thing that made me really grind my teeth was that the editor took it on himself to insert a passage in which he listed a bunch of elements and described them as "minerals", thus leaving me holding the bag for looking like a scientific illiterate. On the bright side, while I hung around JPL for the first 11 post-landing days, I finished the article just before Spirit's computer crisis, which would probably have led me to include a gloomy passage on how the mission was Certainly Doomed. |
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Guest_Richard Trigaux_* |
Dec 6 2005, 04:38 PM
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Here
Russia Plans "Long-Lived" Venus Probe was dicussed the idea of using unconventionnal electronics to sustain the high temperatures (460°C) at the surface of Venus. There was mainly three methods proposed: -unconventionnal semiconductors -micro-sized vacuum tubes implemented witht he techniques of integrated circuits -micro-sized electrostatic relays I note that the two latest proposals are also suited to resist to high radioactivity levels, so that they will be a good solution for a Europa orbiter (and even a Io orbiter) by increasing reliability and removing the weigh of shielding. Developing such techniques will need only a series of small scale test, and then after a relatively short period of large scale development, in a total duration which is not uncompatible with the launching of the mission. |
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