DocumentCode :
938345
Title :
Placing the Satellite in Its Orbit
Author :
Rosen, Milton W.
Author_Institution :
Technical Director, Project VANGUARD, Naval Research Laboratory, Washington, D.C.
Volume :
44
Issue :
6
fYear :
1956
fDate :
6/1/1956 12:00:00 AM
Firstpage :
748
Lastpage :
751
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; Instruments; Kinetic energy; Navigation; Propellants; Rockets; Satellite broadcasting; Skin; Vehicles;
fLanguage :
English
Journal_Title :
Proceedings of the IRE
Publisher :
ieee
ISSN :
0096-8390
Type :
jour
DOI :
10.1109/JRPROC.1956.274966
Filename :
4052085
Link To Document :
بازگشت