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Fuel Level Measurement On Spacecraft, discussion & ideas
Doug M.
post Sep 7 2012, 07:44 AM
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We got answers!

Here's what the good people at Mars Outreach have to say.

QUOTE
1) As of today (having just completed an Orbit Trim Maneuver (OTM)), Odyssey has 17.3 kg, +3.0 / -5.0 propellant.

2) 1.9 kg is obligated for a follow-on OTM in January 2014. Odyssey utilizes approximately 1 kg / year and historically has budgeted 1 kg / year for unexpected safing events. So, propellant life should be between 5.2 to 9.2 years. These numbers are based on no onboard anomalies that would require propellant above the safing budget, no changes in Odyssey's basic operations (three operating reaction wheels, high gain antenna and solar array servos (motors) continue to function normally, etc.) and no further programmatic maneuvers. Consideration is being given to performing a procedure in the future that has the potential to refine the +3 / -5 uncertainty of fuel remaining.

When prop is exhausted, the mission ends because the spacecraft is no longer able to desaturate the reaction wheels and / or provide thruster control; the spacecraft can no longer be pointed to maintain communications and solar panel illumination.

3) The statement is basically correct: THEMIS, which is comprised of two imagers, visible and infrared, and two instruments of the Gamma Ray Suite, High Energy Neutron Detector and the Neutron Spectrometer, all continue to operate and gather science data. The Gamma Ray Spectrometer of the Gamma Ray Suite and Marie have both been decommissioned.


Thanks again for your questions and your interest in Mars exploration!


Wow! Okay, so what comes to mind from this?

Well, the first thing is that there's an awfully large uncertainty in the amount of fuel left. 17.3 kg +3 / -5 ? The range of uncertainty is almost half the total amount of fuel. I wonder why; and I also wonder what the "procedure" might be to narrow the range.

Second is, they have a fair amount of propellant left -- enough for at least another five years of operation. So, barring mechanical failure, Odyssey should see the arrival of MAVEN (2014) and quite possibly of Mars Insight (September 2016 if they make their launch window) and ExoMars Part One (ditto).



Doug M.


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Posts in this topic
- Doug M.   Fuel Level Measurement On Spacecraft   Sep 7 2012, 07:44 AM
- - mcaplinger   QUOTE (Doug M. @ Sep 7 2012, 12:44 AM) Th...   Sep 7 2012, 01:24 PM
- - djellison   The challenges on keeping track on the exact amoun...   Sep 7 2012, 01:53 PM
- - mcaplinger   Re Stardust: good reference on that in http://www....   Sep 7 2012, 02:10 PM
|- - stevesliva   QUOTE (mcaplinger @ Sep 7 2012, 09:10 AM)...   Sep 7 2012, 08:06 PM
- - djellison   Oh - glad something got published on that - thanks...   Sep 7 2012, 02:23 PM
|- - Tom Tamlyn   QUOTE The range of uncertainty is almost half the ...   Sep 7 2012, 03:30 PM
- - Greenish   Also note that the initial propellant load was 348...   Sep 7 2012, 02:56 PM
- - nprev   Pure speculation here...but I wonder if a good mea...   Sep 7 2012, 03:54 PM
|- - Paolo   QUOTE (nprev @ Sep 7 2012, 05:54 PM) I ca...   Sep 7 2012, 04:07 PM
- - djellison   The problem with the thrust/acceleration problem i...   Sep 7 2012, 04:21 PM
|- - RoverDriver   QUOTE (djellison @ Sep 7 2012, 09:21 AM) ...   Sep 7 2012, 05:12 PM
- - nprev   Ah. Did not realize that thruster performance pred...   Sep 7 2012, 04:30 PM
- - nprev   Could be, Paolo. I'm forced to question wheth...   Sep 7 2012, 05:37 PM
|- - Doug M.   QUOTE (nprev @ Sep 7 2012, 06:37 PM) The ...   Sep 7 2012, 06:05 PM
||- - RoverDriver   QUOTE (Doug M. @ Sep 7 2012, 10:05 AM) If...   Sep 7 2012, 06:17 PM
|- - RoverDriver   QUOTE (nprev @ Sep 7 2012, 09:37 AM) Coul...   Sep 7 2012, 06:13 PM
- - nprev   New topic for this old problem.   Sep 7 2012, 06:30 PM
- - chris   While Googling for information on the design of sp...   Sep 10 2012, 11:44 AM
- - Tom Dahl   There is an entertaining video clip on the psi-pci...   Sep 10 2012, 04:41 PM


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