Test Program

W S Haywood; Hugh C Halliday

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NASA NTRS · 19650002608

Test Program

W S Haywood·Hugh C Halliday

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Abstract

A 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.

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W S Haywood, Hugh C Halliday. 1964-11-01. Test Program. https://ntrs.nasa.gov/citations/19650002608

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