Application of the Saderholm erosive burning model to nozzleless solid propellant rocket motors

This paper demonstrates the ability of the Saderholm erosive burning model, when coupled with the Air Force Rocket Propulsion Laboratory Nozzleless Rocket Motor Internal Ballistics Computer Program, to predict the ballistic performance of six nozzleless rocket motors of three designs loaded with thr...

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Veröffentlicht in:	Journal of spacecraft and rockets 1984-01, Vol.21 (1), p.41-46
Hauptverfasser:	Mikkelsen, Clark D, Roys, G. Patrick
Format:	Artikel
Sprache:	eng
Schlagworte:	ballistics Erosive burning flames modeling propellants Rocket engines rockets Solid propellants space technology
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description	This paper demonstrates the ability of the Saderholm erosive burning model, when coupled with the Air Force Rocket Propulsion Laboratory Nozzleless Rocket Motor Internal Ballistics Computer Program, to predict the ballistic performance of six nozzleless rocket motors of three designs loaded with three nonaluminized HTPB propellants. The paper describes the Saderholm erosive burning model, the six nozzleless test motors, and the ballistics prediction methodology.
doi_str_mv	10.2514/3.8605
format	Article
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source	Alma/SFX Local Collection
subjects	ballistics Erosive burning flames modeling propellants Rocket engines rockets Solid propellants space technology
title	Application of the Saderholm erosive burning model to nozzleless solid propellant rocket motors
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