Abstract
A self-sufficient pressurized rover needs adequate power and energyto providelife support, communications, science, and mobility. The Compass Team performed a study investigating how a dynamic radioisotope power system (DRPS)might fulfill thoseneeds. The teamassessed impacts ofradiationonthe crewas wellas how tointegrate such a system. Three 1.2 kWe DRPS systems provide sufficient power forallbutmobilityand a batterysystemis used (charged bytheDRPS)to provide the roughly10kWe power for severalhoursof driving per day. By carrying the Pu238 externally, about2 maway fromthe pressurevessel, the crew cansafelyoperatethevehicle for many weeks. An external radiator is needed to support the Stirling power systems. The totalPu238 loadis around 20kg [48general purpose heat sources (GPHS)], which is slightly less than that carried by the Cassini spacecraft. Alternate power options of stand-alone fuel cells and solar arrays found that these systems were heavier, harder to operate, and/or had limited operating times. The DRPS option is truly a stand-alone solution to pressurized rover operation on Mars or the Moon.
Original language | English |
---|---|
Title of host publication | Proceedings of Nuclear and Emerging Technologies for Space, NETS 2022 |
Publisher | American Nuclear Society |
Pages | 263-270 |
Number of pages | 8 |
ISBN (Electronic) | 9780894487828 |
DOIs | |
State | Published - 2022 |
Event | 2022 Nuclear and Emerging Technologies for Space, NETS 2022 - Cleveland, United States Duration: May 8 2022 → May 12 2022 |
Publication series
Name | Proceedings of Nuclear and Emerging Technologies for Space, NETS 2022 |
---|
Conference
Conference | 2022 Nuclear and Emerging Technologies for Space, NETS 2022 |
---|---|
Country/Territory | United States |
City | Cleveland |
Period | 05/8/22 → 05/12/22 |
Funding
This conceptual design wa s performed for the RPS office, STMD, a nd the Mars Assessment Team. The Compass Team wishes to thank the support of Michelle Rucker, Ta ylor Phillips-Hungerford, Bret Dra ke, a nd Jeff George of NASA-JSC for their pa rticipation in this design.