Main-stage solid-propellant rocket motor design

Details Main-stage solid-propellant rocket motor design Main-stage solid-propellant rocket motor design

1991-01-03

1992-08-04

Carone, Michael J.

Power plants

Reaction motor

Solid propellant

60255, F02K 918, F02K 934

Patent

active

H00010820

ABSTRACT:
A ballistic missile main-stage solid-propellant rocket motor; including a propellant grain configuration tailored to provide required missile ballistic performance, having a center bore, major and minor rear fin slots, and a silver eliminator bore enlargement; utilizing a forward pressure equalizing flap; and designed to accommodate severe operating conditions.

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