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Acceptance test procedure for shuttle actuators simulator (elevon subsystem)The acceptance test procedure is described for the Lockheed Electronics Elevon Servoactuator Simulator to be used in the Shuttle Avionics Integration Laboratory (SAIL). The intent of this acceptance test procedure is to comply with the technical Shuttle Actuators Simulator Requirements. Acceptance tests will be performed on each Elevon Servoactuator Simulator.
Document ID
19760021152
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Barr, J. (Lockheed Electronics Co. Houston, TX, United States)
Date Acquired
September 3, 2013
Publication Date
April 1, 1976
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
LEC-8124
JSC-11095
NASA-CR-147830
Report Number: LEC-8124
Report Number: JSC-11095
Report Number: NASA-CR-147830
Accession Number
76N28240
Funding Number(s)
CONTRACT_GRANT: NAS9-12200
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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