Advanced Spacesuit Avionics Subsystem Integration Testing

Paper #:
  • 2014-01-2150

Published:
  • 2014-09-16
Citation:
Bradish, M., Sands, O., Wright, T., Bakula, C. et al., "Advanced Spacesuit Avionics Subsystem Integration Testing," SAE Technical Paper 2014-01-2150, 2014, https://doi.org/10.4271/2014-01-2150.
Pages:
16
Abstract:
This paper summarizes the Power, Avionics and Software (PAS) 1.0 subsystem integration testing and test results that occurred in August and September of 2013. This paper covers the capabilities of each PAS assembly to meet integration test objectives for non-safety critical, non-flight, non-human-rated hardware and software development. This test report is the outcome of the first integration of the PAS subsystem and is meant to provide data for subsequent designs, development and testing of the future PAS subsystems. The two main objectives were to assess the ability of the PAS assemblies' to exchange messages and to perform audio tests of both inbound and outbound channels. This paper describes each test performed, defines the test, the data, and provides conclusions and recommendations.
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