DocumentCode :
386909
Title :
Placing the satellite in its orbit
Author :
Rosen, Mark
Author_Institution :
Naval Research Laboratory, Washington, DC, USA
Volume :
4
fYear :
1966
fDate :
21-25 March 1966
Firstpage :
103
Lastpage :
107
Abstract :
The VANGUARD satellite launching vehicle is a three-stage rocket of which the first two stages are guided and the third stage is maintained in a fixed orientation while it is firing. The first stage, an improved Viking, serves primarily to raise the remaining stages to altitude. The second stage, another liquid-propellant rocket, contains the guidance for the three-stage vehicle and, in addition, supplies some of the propulsive energy. The third stage, a solid-propellant rocket, is ejected from the second stage at orbital altitude and provides about half of the required orbital velocity. The VANGUARD launching vehicle system was chosen from a number of possible two- and three-stage vehicle combinations. It represents the smallest satellite launching vehicle consistent with the present state of rocket development.
Keywords :
Earth; Helium; Inductors; Kinetic energy; Navigation; Propulsion; Rockets; Satellite broadcasting; Skin; Vehicles;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
1958 IRE International Convention Record
Conference_Location :
New York, NY, USA
Type :
conf
DOI :
10.1109/IRECON.1956.1150453
Filename :
1150453
Link To Document :
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