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Solid Propellant Rocket Motors

Published online by Cambridge University Press:  04 July 2016

W. R. Maxwell  and
G. H. S. Young
W. R. Maxwell
Affiliation:
Rocket Propulsion Establishment, Westcott
G. H. S. Young
Affiliation:
Explosives Research and Development Establishment, Waltham Abbey
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Extract

A solid propellant rocket motor consists essentially of a propellant charge in a container fitted with an expansion nozzle and igniter. Since, before a rocket motor can be designed, it is necessary to have some knowledge of the properties of the propellant to be used, a description will first be given of the propellants which are currently available.

Type
Astronautics and Guided flight Section
Information
The Aeronautical Journal , Volume 65 , Issue 604 , April 1961 , pp. 252 - 262
Copyright
Copyright © Royal Aeronautical Society 1961

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References

1.Mishuck, E. and Carleton, L. T. (1960). Ind. Eng. Chem., Vol. 52, p. 755, 1960.CrossRefGoogle Scholar
2.Smith, Thor L. (1960). Ind. Eng. Chem., Vol. 52, p. 776, 1960.CrossRefGoogle Scholar
3.Young, G. H. S. (1959). Chemistry of Propellants. A.G.A.R.D. Meeting, June 1959, Pergamon Press, p. 285, 1960.Google Scholar
4.Anon, . (1960). Missiles and Rockets, Vol. 7, No. 9, p. 47, 1960.Google Scholar