Thermal pyrolysis and combustion of HTPB-based solid fuels for hybrid rocket motor applications
32nd Joint Propulsion Conference and Exhibit ; 1996 ; Lake Buena Vista , FL , U.S.A.
1996-01-01
Conference paper
Electronic Resource
English
Development of a N2O/HTPB hybrid rocket motor
AIAA | 1997
|Combustion performance and scale effect from N2O/HTPB hybrid rocket motor simulations
Online Contents | 2013
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