Space Shuttle Standard Launch Window

861649

10/01/1986

Authors
Abstract
Content
To 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° inclination orbits. The window consists of two time periods, each 2-hr long and centered at 0023 and 1223 Greenwich mean time, and extends unchanged throughout the year.
Meta TagsDetails
DOI
https://doi.org/10.4271/861649
Pages
10
Citation
DeAtkine, D., "Space Shuttle Standard Launch Window," SAE Technical Paper 861649, 1986, https://doi.org/10.4271/861649.
Additional Details
Publisher
Published
Oct 1, 1986
Product Code
861649
Content Type
Technical Paper
Language
English