DocumentCode
2097880
Title
Flight performance of the ERTS-1 spacecraft power system
Author
Kirpich, A. ; Lamnin, M. ; Thierfelder, H. ; Wise, D.
Author_Institution
General Electric Company
fYear
1973
fDate
11-13 June 1973
Firstpage
30
Lastpage
40
Abstract
The initial spacecraft of the Earth Resources Technology Satellite Program, ERTS-1, was launched on July 23, 1972, and has provided broad earth resource data for use by numerous governmental and scientific agencies. This paper reports on the basic design and flight performance to date of the ERTS-1 power system. The design is based on earlier Nimbus spacecraft power system configurations with modifications introduced to provide increases in average and peak power capabilities. Data is presented showing overall design performance in terms of allowable load duty cycles, solar array capability, and battery charge and discharge behavior. Of special interest is the effect of solar flare activity occurring on August 3 to 7, 1972, in abruptly reducing the solar array output. After 10 months in orbit sufficient power remains for another 18 months of ERTS operation.
Keywords
Arrays; Batteries; Earth; Orbits; Payloads; Power systems; Space vehicles;
fLanguage
English
Publisher
ieee
Conference_Titel
Power Electronics Specialists Conference, 1973 IEEE
Conference_Location
Pasadena, California, USA
ISSN
0275-9306
Type
conf
DOI
10.1109/PESC.1973.7065166
Filename
7065166
Link To Document