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.
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. Download Citation
Author(s):
Martin Bradish, Obed Sands, Ted Wright, Casey Bakula, Daniel Oldham, William Ivancic, Michael Lewis, Joseph Klebau, Nicholas Tollis, Andrew Jalics
Affiliated:
NASA, NASA Glenn Reseach Center, SAIC NASA GRC, Vantage Partners Limited
Pages: 16
Event:
SAE 2014 Aerospace Systems and Technology Conference
ISSN:
0148-7191
e-ISSN:
2688-3627
Related Topics:
Assembling
Avionics
Computer software and hardware
Spacesuits
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