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NIMBUS COMMAND SUBSYSTEMAll satellites have one common requirement, known as the command facility. This is usually a real-time direct RF link from a ground transmitter through the satellite receiver and decoder to a relay or controlled circuit. The more sophisticated research and operational satellites require a command facility which will permit storing of commands to activate systems at predetermined future times when the satellite is beyond the range of the command ground station. These satellites require an accurate clock and a source of precision frequencies.

In the Nimbus spacecraft, all these functions are performed by an integrated command and clock subsystem, which includes the command clock and clock-receiver modules in the spacecraft, plus the associated command ground station. This paper will describe the functions and features of these various equipment's.
Document ID
19630008738
Acquisition Source
Goddard Space Flight Center
Document Type
Conference Paper
Authors
J. J. Over
(Goddard Space Flight Center Greenbelt, Maryland, United States)
D. W. Gade
(California Computer Products, Inc. Greenbelt, MD, United States)
R. E. Trousdale
(California Computer Products, Inc. Greenbelt, MD, United States)
F. Wiley
(California Computer Products, Inc. Greenbelt, MD, United States)
J. Bunn
(RCA Greenbelt, MD, United States)
Date Acquired
August 1, 2013
Publication Date
January 1, 1962
Subject Category
Space Sciences
Meeting Information
Meeting: Nimbus Program Review
Location: Valley Forge, PA
Country: US
Start Date: November 13, 1962
End Date: November 15, 1962
Sponsors: Goddard Space Flight Center
Accession Number
63N18615
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
GROUND SUPPORT SYSTEM
COMMAND SYSTEM
NIMBUS SATELLITE
TIMING APPARATUS
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