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Space research and SpartanFor a number of years, space research has been primarily conducted with sounding rockets and orbiting satellites. The use of satellites has disadvantages related to cost and the long lead time from design to launch, while a drawback in the case of sounding rockets is the short flight time of only a few minutes. The development of the Shuttle led to the proposal to employ for space research an autonomous free-flying payload deployed and recovered by the Shuttle. The proposed payload, called SPEAR (Small Payload Ejection and Recovery), looked very much like a rocket payload. Subsequently, the payload developed into a more compact form, and its name became Spartan-1. Attention is given to the demands of space research, the Spartan-1 payload, the payload functional control system, the thermal control system, the Spartan-1 mission, and the future of Spartan.
Document ID
19850037643
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Cruddace, R. G.
(Naval Research Lab. Washington, DC, United States)
Fritz, G. G.
(U.S. Navy, Naval Research Laboratory, Washington DC, United States)
Shrewsberry, D. J.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1985
Subject Category
Space Sciences (General)
Report/Patent Number
AIAA PAPER 85-0502
Accession Number
85A19794
Distribution Limits
Public
Copyright
Other

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