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Mars lander deorbit trajectory analysisMars lander deorbit trajectory sensitivity analysis for fixed flight path and communications angles at atmospheric entry, comparing with Monte Carlo simulation
Document ID
19710037931
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Euler, E. A.
Date Acquired
August 6, 2013
Publication Date
January 1, 1971
Publication Information
Publisher: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS,
Subject Category
Space Sciences
Report/Patent Number
AIAA PAPER 71-190
Report Number: AIAA PAPER 71-190
Meeting Information
Meeting: AEROSPACE SCIENCES MEETING
Location: NEW YORK, NY
Start Date: January 25, 1971
End Date: January 27, 1971
Sponsors: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS
Accession Number
71A18628
Funding Number(s)
CONTRACT_GRANT: NAS1-9000
Distribution Limits
Public
Copyright
Other

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