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Preliminary flight trajectories for the Apollo Soyuz test projectPreliminary data are documented for a typical launch window opening, a typical in-plane case, and a typical launch window closing trajectory, not necessarily in the same daily launch window, for the Apollo Soyuz test project mission. The Soyuz will be launched first and the Apollo will be launched on the first opportunity, 7 hours 21 minutes later. If the Apollo is unable to be launched on the first opportunity, four additional opportunities are available at 30 hours 56 minutes, 54 hours 31 minutes, 78 hours 05 minutes, and 101 hours 40 minutes. If the Apollo cannot be launched in this time frame, no further attempt will be made to launch and rendezvous with the first Soyuz. Soyuz will then be deorbited; however, a second Soyuz was made available for the same purposes.
Document ID
19740002666
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Brooks, J. D. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 3, 2013
Publication Date
April 1, 1973
Subject Category
Space Sciences
Report/Patent Number
NASA-TM-X-64737
Accession Number
74N10779
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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