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The Evolution of the Viking Landing GearThe primary function of the landing gear is to dissipate touchdown energy in a controlled fashion that minimizes the landing shock for onboard components while maximizing ground clearance and the probability of landing stability over the range of possible surface and touchdown parameter variations. Many other mission requirements and constraints were translated into the evolving Viking landing gear design as they arose. Hence, design considerations included such factors as prelaunch heat sterilization and noncontamination of the Martian landing site, gear stowage and deployment, terminal descent engine shutdown initiation, structural load attenuation, hard/soft landing surface capability, reliability, weight, and post-landed stability.
Document ID
19760021205
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Pohlen, J. C.
(NASA Langley Research Center Hampton, VA, United States)
Maytum, B. D.
(NASA Langley Research Center Hampton, VA, United States)
Ramsey, I. W.
(NASA Langley Research Center Hampton, VA, United States)
Blanchard, U. J.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 8, 2013
Publication Date
July 1, 1976
Publication Information
Publication: JPL 10th Aerospace Mech. Symp.
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
76N28293
Funding Number(s)
CONTRACT_GRANT: NAS1-9000
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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