DocumentCode
2789122
Title
To Europa and beyond (enabled by a small-RPS)
Author
Balint, Tibor S.
Author_Institution
Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA
fYear
2005
fDate
5-12 March 2005
Firstpage
1061
Lastpage
1068
Abstract
Solar System Exploration (SSE) to the Outer Planets requires internal power sources, since external power generation, relying on solar power, is not very effective or practical. One of the scientifically interesting destinations in this region is Jupiter´s moon Europa, where a lander would require internal power sources, such as batteries or radioisotope power systems (RPS) to achieve mission success. This paper discusses a Europa lander concept as a potential adjunct element to NASA´s proposed Jupiter Icy Moons Orbiter (JIMO) mission. The lander would operate on the surface for 3 to 14 days, performing astrobiology, geophysics and geological-compositional measurements as defined by the JIMO Science Definition Team (SDT). The power system trade study for this concept compares small-RPSs up to ∼50 We against primary batteries. Additional SSE destinations are also outlined, where small-RPSs provide a viable option to accomplish science and mission objectives.
Keywords
Jupiter; planetary satellites; radioisotope thermoelectric generators; space research; space vehicle power plants; Europa; JIMO Science Definition Team; JIMO mission; Jupiter Icy Moons Orbiter; external power generation; internal power sources; outer planets; radioisotope power systems; small-RPS; solar power; solar system exploration; Batteries; Jupiter; Moon; Performance evaluation; Planets; Power system measurements; Radioactive materials; Solar energy; Solar power generation; Solar system;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace Conference, 2005 IEEE
Conference_Location
Big Sky, MT
Print_ISBN
0-7803-8870-4
Type
conf
DOI
10.1109/AERO.2005.1559396
Filename
1559396
Link To Document