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Flight problem evaluation for Space Shuttle OrbiterThe flight problems experienced with the reusable Space Shuttle Orbiter have decreased during subsequent flights of each vehicle. By comparison to first flights of previous vehicles, the problems encountered on the initial flight of each new vehicle entering the fleet decreased. This improvement in turn has reduced the turnaround time between flights significantly and thus greatly enhanced the increased Space Shuttle launch frequency. The reusable manned space vehicle concept necessitated the development of a flight problem recognition and resolution system which would enable a thorough and timely vehicle turnaround flow. Flight evaluation, testing, and repair of manned spacecraft to enhance reliability and to ensure mission success is a unique activity. Real-time recognition of the flight problem, prompt isolation of the cause, and timely implementation of the corrective action are the keys to maintaining an operational fleet. Examples of flight problems that have been encountered as well as the corrective actions implemented during the first 24 Space Shuttle missions are presented. The corrective actions taken to preclude problem recurrence include modifications of hardware designs, manufacturing processes, flight software, test methods, and operational procedures.
Document ID
19880046551
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Mechelay, Joseph E.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Ward, Robert J.
(NASA Johnson Space Center Houston, TX, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1987
Subject Category
Space Transportation
Meeting Information
Meeting: Aerospace Testing Seminar
Location: Los Angeles, CA
Country: United States
Start Date: March 10, 1987
End Date: March 12, 1987
Accession Number
88A33778
Distribution Limits
Public
Copyright
Other

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