SATELLITE TESTING PROCEDURES INCLUDING EN- VIRONMENTAL CONDITIONS FOR PAYLOAD EQUIPMENT AND ASSEMBLED PAYLOADS,

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Abstract:

This document establishes the procedure and environment to be used in satellite electronic equipment and assembled payload testing. These tests are formulated specifically to establish the ability of the equipment to withstand, with out performance degradation, storage, handling, transportation, pre-launching preparations, launching, orbital injection and sustained orbit. Author

Author(s):
Schreiber, M. A.
Author Organization(s):
JOHNS HOPKINS UNIV SILVER SPRING MD APPLIED PHYSICS LAB
Supplementary Note:
Supersedes TG-416A.
Annotation:
Satellite testing procedures environmental conditions for payload quipment and assembled payloads.
Pagination:
0023

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
TG416B
Contract/Grant Number(s):
NOw62 0604
 Subject Terms
Modernization Areas:
Space
Communities of Interest:
Space
Descriptor(s):
PAYLOAD, VIBRATION, SOLID PROPELLANT ROCKET ENGINES, COMBUSTION
Keyword(s):
SCOUT, X 248 MOTORS
Report Date:
1963 May 01