Precision controlled variable thrust solid propellant rocket...

Details Precision controlled variable thrust solid propellant rocket... Precision controlled variable thrust solid propellant rocket...

F - Mech Eng,Light,Heat,Weapons

42

B

89/3.5

F42B 15/00 (2006.01) F02K 9/76 (2006.01) F02K 9/80 (2006.01)

Patent

CA 2018999

ABSTRACT A multiple stage solid rocket motor is operated in a manner designed to control its mass discharge profile. This is accomplished by providing means for igniting one stage and then igniting a subsequent stage while the first continues to burn.

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