Defining the Mars Ascent Problem for Sample Return
Lifting geology samples off of Mars is both a daunting technical problem for propulsion experts and a cultural challenge for the entire community that plans and implements planetary science missions. The vast majority of science spacecraft require propulsive maneuvers that are similar to what is done routinely with communication satellites, so most needs have been met by adapting hardware and methods from the satellite industry. While it is even possible to reach Earth from the surface of the moon using such traditional technology, ascending from the surface of Mars is beyond proven capability for either solid or liquid propellant rocket technology. Miniature rocket stages for a Mars ascent vehicle would need to be over 80 percent propellant by mass. It is argued that the planetary community faces a steep learning curve toward nontraditional propulsion expertise, in order to successfully accomplish a Mars sample return mission. A cultural shift may be needed to accommodate more technical risk acceptance during the technology development phase.
- Research Organization:
- Lawrence Livermore National Laboratory (LLNL), Livermore, CA
- Sponsoring Organization:
- USDOE
- DOE Contract Number:
- W-7405-ENG-48
- OSTI ID:
- 945705
- Report Number(s):
- LLNL-CONF-406145
- Country of Publication:
- United States
- Language:
- English
Mars sample return, a concept point design by Team-X (JPL's advanced project design team)
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conference | January 2002 |
Technology development plans for the Mars Sample Return mission
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conference | January 2005 |
Mars Ascent Vehicle Key Elements of a Mars Sample Return Mission
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conference | January 2006 |
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