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MISDAS - A mechanical impact system design for Apollo-type spacecraft.Mechanical impact attenuation system for Apollo spacecraft provides stable land landing platform, noting deployed heat shields, extended legs, pneumatic bags, etc
Document ID
19670050694
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Bernstein, A. I.
Musicman, A. S.
Date Acquired
August 3, 2013
Publication Date
June 1, 1967
Publication Information
Publication: /AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS
Subject Category
Space Vehicles
Report/Patent Number
AIAA PAPER 66-989
Report Number: AIAA PAPER 66-989
Accession Number
67A29423
Funding Number(s)
CONTRACT_GRANT: NAS9-4915
Distribution Limits
Public
Copyright
Other
Keywords
APOLLO SPACECRAFT
LANDING SYSTEM
SYSTEM STABILITY
IMPACT DAMAGE

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