DocumentCode :
952105
Title :
Explorer Satellite Electronics
Author :
Victor, W.K. ; Richter, H.L. ; Eyraud, J.P.
Author_Institution :
Jet Propulsion Lab., California Inst. Tech., Pasadena, Calif.
Issue :
42403
fYear :
1960
Firstpage :
78
Lastpage :
85
Abstract :
A discussion is presented of the design restrictions and the philosophy which enabled the Explorer satellites to be first during the IGY to reveal the presence of a belt of intense cosmic radiation encircling the earth´s equator. In addition, an indication of the amount and momentum of cosmic dust in the solar system was obtained from the Explorers. Methods used to obtain reliability in the transducing and communications system are described, together with interpretations of space-environment information as deduced from the narrow-band telemetry.
Keywords :
Batteries; Earth; Instruments; Missiles; Nose; Payloads; Propulsion; Rockets; Satellite broadcasting; Temperature;
fLanguage :
English
Journal_Title :
Military Electronics, IRE Transactions on
Publisher :
ieee
ISSN :
0096-2511
Type :
jour
DOI :
10.1109/IRET-MIL.1960.5008205
Filename :
5008205
Link To Document :
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