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Space Shuttle standard launch windowTo maximize the efficiency of the Space Transportation System as a shared cargo launch system and to enhance the mixability and launch opportunities for payloads carried on the Space Shuttle, the National Aeronautics and Space Administration has developed a shared cargo standard launch window. The launch window is based on the transfer orbit sun angle requirements of an established, common class of geosynchronous communications satellites. This standard window is applicable to mixed cargoes launched from the John F. Kennedy Space Center into 28.5 deg inclination orbits. The window consists of two time periods, each 2 hrs long and centered at 0023 and 1223 Greenwich mean time; it extends unchanged throughout the year.
Document ID
19870045314
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Deatkine, David D.
(NASA Johnson Space Center Houston, TX, United States)
Date Acquired
August 13, 2013
Publication Date
October 1, 1986
Subject Category
Space Transportation
Report/Patent Number
SAE PAPER 861649
Report Number: SAE PAPER 861649
Accession Number
87A32588
Distribution Limits
Public
Copyright
Other

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