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Single-Grain Dual-Thrust Motor

The propellant grain is composed of an (( -84) as an oxidizer and pu (0.16) as a fuel. The burning rate and characteristics are shown as a function of pressure [Pg.416]

1 Mass Generation Rate and Mass Discharge Rate [Pg.417]

See other pages where Single-Grain Dual-Thrust Motor is mentioned: [Pg.420]    [Pg.414]    [Pg.420]    [Pg.420]    [Pg.414]    [Pg.420]    [Pg.414]    [Pg.414]    [Pg.414]    [Pg.414]   


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Dual-thrust motor

Single-grained

Thrust

Thrust, thrusting

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