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A mobile planetary lander utilizing elastic loop suspensionEfforts to increase the cost effectiveness of future lunar and planetary rover missions have led to the mobile lander concept, which replaces the landing legs of a soft-lander craft with a compact mobility system of sufficient strength to withstand the landing impact. The results of a mobile lander conceptual design effort based on existing NASA-Viking '75 hardware are presented. The elastic loop concept, developed as a post-Apollo rover technology, is found to meet stringent stowage, traction, power and weight requirements.
Document ID
19760021186
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Trautwein, W.
(Lockheed Missiles and Space Co. Huntsville, AL, United States)
Date Acquired
August 8, 2013
Publication Date
July 1, 1976
Publication Information
Publication: JPL 10th Aerospace Mech. Symp.
Subject Category
Mechanical Engineering
Accession Number
76N28274
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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