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Test ProgramA test program was set up early in the Explorer XIII program to simulate as nearly as possible all expected environmental conditions to which the spacecraft would be subjected during the ascending phase of the trajectory and while in orbit. These tests included spin, acceleration, thermal-vacuum, vibration, and shock. Functional tests were performed on individual modules of the telemeter system. The test procedure started with breadboard construction of telemeter components. Circuits were evaluated in this phase, and components chosen for prototype construction. Prior to the prototype environmental tests, it was found desirable to construct a mock-up structure for preliminary evaluation of the spacecraft hardware.
Document ID
19650002608
Acquisition Source
Langley Research Center
Document Type
Other - Technical Report
Authors
W S Haywood
(Langley Research Center Hampton, United States)
Hugh C Halliday
(Langley Research Center Hampton, United States)
Date Acquired
August 2, 2013
Publication Date
November 1, 1964
Publication Information
Publication: The Micrometeoroid Satellite Explorer XIII (1961 CHI)
Publisher: National Aeronautics and Space Administration
Subject Category
Spacecraft Design, Testing and Performance
Report/Patent Number
NASA-TN-D-2468
Accession Number
65N12209
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
Explorer XIII Satellite
Environmental Testing
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