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A technique for lifting entry and terminal phase system optimization for the 1975 Mars Viking landerLifting entry and terminal phase system optimization for 1975 Mars Viking lander, considering graphical tradeoff approach including design parameter and atmosphere model variations
Document ID
19710056474
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
French, C. E.
Howard, D. A.
Zeiner, H. N.
Date Acquired
August 6, 2013
Publication Date
August 1, 1971
Publication Information
Publisher: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS,
Subject Category
Space Vehicles
Report/Patent Number
AIAA PAPER 71-922
Report Number: AIAA PAPER 71-922
Meeting Information
Meeting: GUIDANCE, CONTROL AND FLIGHT MECHANICS CONFERENCE
Location: HEMPSTEAD, NY
Start Date: August 16, 1971
End Date: August 18, 1971
Sponsors: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS
Accession Number
71A37171
Funding Number(s)
CONTRACT_GRANT: NAS1-9000
Distribution Limits
Public
Copyright
Other

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