DocumentCode
2433506
Title
Prospecting Rovers for Lunar Exploration
Author
Graham, Jerry B.
Author_Institution
Marshall Space Flight Center, Huntsville
fYear
2007
fDate
3-10 March 2007
Firstpage
1
Lastpage
11
Abstract
A study of rover options for exploring the permanently shadowed regions of the lunar environment is presented. The potential for nearly continuous solar illumination and the possible existence of substantial water ice deposits focus the exploration planner´s attention on the polar regions of the Moon. These regions feature permanently shadowed craters that, remote sensing data suggest, may contain water ice. This water ice, if present, can be converted to fuel cell reactants, breathing oxygen, potable water, and rocket propellant, all vital resources for the ultimate exploration of the moon and the solar system. To provide early ground truth on the existence and abundance of this water ice for subsequent mission planning purposes, the NASA lunar precursor robotics program (LPRP) sponsored a study of potential prospecting rover concepts as one part of the LPRP-2 pre-phase A studies. Numerous vehicle configurations were conceptualized to support a suite of prospecting and scientific measurement equipment for sustained operations in a permanently shadowed crater. Trades and analyses were performed for key functions including mobility, power, and thermal management. Rover options in the 400 to 530 kg class are developed which are capable of either confirming the presence of water ice at the poles or conclusively demonstrating its absence.
Keywords
aerospace robotics; lunar surface; mobile robots; planetary rovers; Moon; NASA Lunar Precursor Robotics Program; lunar exploration; mission planning; rovers; water ice; Fuel cells; Ice; Lighting; Moon; Propulsion; Remote sensing; Rockets; Solar system; Thermal management; Water resources;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace Conference, 2007 IEEE
Conference_Location
Big Sky, MT
ISSN
1095-323X
Print_ISBN
1-4244-0524-6
Electronic_ISBN
1095-323X
Type
conf
DOI
10.1109/AERO.2007.352706
Filename
4161280
Link To Document