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The design and reconstruction of the Viking Lander descent trajectoriesThe success of the Viking Mission is truly a major milestone in this country's planetary exploration program. This paper deals with the trajectory characteristics of the Viking Lander descent trajectories, beginning with the imposed requirements and constraints, the final preflight design based on the final hardware and operational capability, and ending with the actual performance achieved. A comparison between the predicted and actual trajectory characteristics is made to indicate the achieved accuracy and modeling fidelity. Also, estimates of the Martian environment derived from the entry-trajectory reconstruction process are presented.
Document ID
19780048019
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Euler, E. A.
(Martin Marietta Aerospace Denver, CO, United States)
Adams, G. L.
(Martin Marietta Aerospace Denver, CO, United States)
Hopper, F. W.
(Martin Marietta Aerospace Denver, Colo., United States)
Date Acquired
August 9, 2013
Publication Date
September 1, 1977
Subject Category
Astrodynamics
Accession Number
78A31928
Funding Number(s)
CONTRACT_GRANT: NAS1-9000
Distribution Limits
Public
Copyright
Other

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