NASA NTRS · 19760021152
Acceptance test procedure for shuttle actuators simulator (elevon subsystem)
Abstract
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.
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Barr, J.. 1976-04-01. Acceptance test procedure for shuttle actuators simulator (elevon subsystem). https://ntrs.nasa.gov/citations/19760021152
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