Evolution of Space Shuttle Range Safety Ascent Flight Envelope Design
Author(s) -
Joan D. Brewer,
Jerel G. Davis,
Christopher Glenn
Publication year - 2011
Publication title -
nasa sti repository (national aeronautics and space administration)
Language(s) - English
Resource type - Conference proceedings
DOI - 10.2514/6.2011-7191
Subject(s) - space shuttle , aerospace engineering , envelope (radar) , range (aeronautics) , aeronautics , computer science , flight safety , space (punctuation) , physics , engineering , radar , operating system
For 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 45 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.
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