Hybrid rocket combustion enhancement

Details Hybrid rocket combustion enhancement Hybrid rocket combustion enhancement

1989-08-24

1996-12-10

Jordan, Charles T.

Power plants

Reaction motor

Solid and fluid propellant

60207, 60211, 60219, 60250, F02K 928

Patent

active

055820018

ABSTRACT:
The combustion of a hybrid engine is improved by continuously injecting into a precombustion chamber a hypergolic fluid such as triethyl aluminum which exothermically reacts with and vaporizes the oxidizer such as liquid oxygen. The prevaporized oxidizer evenly combusts the solid propellant grain to develop thrust.

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patent: 3782112 (1974-01-01), Muzzy
patent: 4038321 (1977-07-01), Thatcher et al.
patent: 4176637 (1979-12-01), Cole
patent: 4723736 (1988-02-01), Rider
patent: 4771601 (1988-09-01), Spies
patent: 4880185 (1989-11-01), Apfel

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