Solid rocket motor fire tests - Phases 1 and 2

JHU/APL conducted a series of open-air burns of small blocks (3 to 10 kg) of solid rocket motor (SRM) propellant at the Thiokol Elkton MD facility to elucidate the thermal environment under burning propellant. The propellant was TP-H-3340A for the STAR 48 motor, with a weight ratio of 71/18/11 for t...

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Bibliographische Detailangaben

Hauptverfasser:	Chang, Y, Hunter, L W, Han, D K, Thomas, M E, Cain, R P, Lennon, A M
Format:	Tagungsbericht
Sprache:	eng
Online-Zugang:	Volltext
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