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Evolution of Space Shuttle Range Safety Ascent Flight Envelope DesignFor every space vehicle launch from the Eastern Range in Florida, the range user must provide specific Range Safety (RS) data products to the Air Force's 45th Space Wing in order to obtain flight plan approval. One of these data products is a set of RS ascent flight envelope trajectories that define the normal operating region of the vehicle during powered flight. With the Shuttle Program launching 135 manned missions over a 30-year period, 135 envelope sets were delivered to the range. During this time, the envelope methodology and design process evolved to support mission changes, maintain high data quality, and reduce costs. The purpose of this document is to outline the shuttle envelope design evolution and capture the lessons learned that could apply to future spaceflight endeavors.
Document ID
20110014078
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Brewer, Joan
(United Space Alliance Houston, TX, United States)
Davis, Jerel
(United Space Alliance Houston, TX, United States)
Glenn, Christopher
(NASA Johnson Space Center Houston, TX, United States)
Date Acquired
August 25, 2013
Publication Date
January 1, 2011
Subject Category
Space Transportation And Safety
Report/Patent Number
JSC-CN-24283
JSC-CN-24228
Report Number: JSC-CN-24283
Report Number: JSC-CN-24228
Meeting Information
Meeting: AIAA Space 2011 Conference
Location: Long Beach, CA
Country: United States
Start Date: September 26, 2011
End Date: September 29, 2011
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Public Use Permitted.
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