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Rover deployment system for lunar landing mission.

Authors :
Sutoh, Masataku
Hoshino, Takeshi
Wakabayashi, Sachiko
Source :
Acta Astronautica. Sep2017, Vol. 138, p454-461. 8p.
Publication Year :
2017

Abstract

For lunar surface exploration, a deployment system is necessary to allow a rover to leave the lander. The system should be as lightweight as possible and stored retracted when launched. In this paper, two types of retractable deployment systems for lunar landing missions, telescopic- and fold-type ramps, are discussed. In the telescopic-type system, a ramp is stored with the sections overlapping and slides out during deployment. In the fold-type system, it is stored folded and unfolds for the deployment. For the development of these ramps, a design concept study and structural analysis were conducted first. Subsequently, ramp deployment and rover release tests were performed using the developed ramp prototypes. Through these tests, the validity of their design concepts and functions have been confirmed. In the rover release test, it was observed that the developed lightweight ramp was sufficiently strong for a 50-kg rover to descend. This result suggests that this ramp system is suitable for the deployment of a 300-kg-class rover on the Moon, where the gravity is about one-sixth that on Earth. The lightweight and sturdy ramp developed in this study will contribute to both safe rover deployment and increase of lander/rover payload. [ABSTRACT FROM AUTHOR]

Details

Language :
English
ISSN :
00945765
Volume :
138
Database :
Academic Search Index
Journal :
Acta Astronautica
Publication Type :
Academic Journal
Accession number :
124474096
Full Text :
https://doi.org/10.1016/j.actaastro.2017.06.019