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The lunar hopping transporterResearch on several aspects of lunar transport using the hopping mode is reported. Hopping exploits the weak lunar gravity, permits fuel economy because of partial recompression of propellant gas on landing, and does not require a continuous smooth surface for operation. Three questions critical to the design of a lunar hopping vehicle are addressed directly in this report: (1) the tolerance of a human pilot for repeated accelerations; (2) means for controlling vehicle attitude during ballistic flight; and (3) means of propulsion. In addition, a small scale terrestrial demonstrator built to confirm feasibility of the proposed operational mode is described, along with results of preliminary study of unmanned hoppers for moon exploration.
Document ID
19730007490
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Degner, R.
(Stanford Univ. CA, United States)
Kaplan, M. H.
(Stanford Univ. CA, United States)
Manning, J.
(Stanford Univ. CA, United States)
Meetin, R.
(Stanford Univ. CA, United States)
Pasternack, S.
(Stanford Univ. CA, United States)
Peterson, S.
(Stanford Univ. CA, United States)
Seifert, H.
(Stanford Univ. CA, United States)
Date Acquired
September 2, 2013
Publication Date
July 1, 1971
Subject Category
Facilities, Research, And Support
Report/Patent Number
NASA-CR-130010
SUDAAR-428
Accession Number
73N16217
Funding Number(s)
CONTRACT_GRANT: NGR-05-020-258
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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