Applying Boeing Commercial Airplane automated test and checkout techniques to reusable space propulsion systemsAutomated test and checkout computer tools that have been developed for commercial and military aircraft are presently shown to be applicable to reusable launch vehicle and spacecraft propulsion systems, for the sake of reductions in maintenance personnel and calendar time. Attention is given to the potential uses of the Programmable Engine Tester and the Integrated Functional Test System in the context of SSME problems. It is found that while direct application of existing automated checkout systems would be difficult, future spacecraft propulsion technology can be designed for integral operation with such systems.
Document ID
19930032407
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Wilkinson, Calvin L. (NASA Langley Research Center Hampton, VA, United States)
Alyea, Dian (Boeing Defense & Space Group Seattle, WA, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1991
Publication Information
Publication: In: Annual Health Monitoring Conference for Space Propulsion Systems, 3rd, Cincinnati, OH, Nov. 13, 14, 1991, Proceedings (A93-16401 04-20)