Liquid oxidizer immersion type hybrid rocket

Details Liquid oxidizer immersion type hybrid rocket Liquid oxidizer immersion type hybrid rocket

1995-05-11

1997-12-09

Koczo, Michael

Power plants

Reaction motor

Solid and fluid propellant

60253, F02K 970

Patent

active

056947690

ABSTRACT:
A liquid oxidizer immersion hybrid rocket having a combustion chamber, a porous fuel material placed in the combustion chamber, a liquid oxidizer filled into pores of the porous fuel material, and two holding plates provided in the combustion chamber so as to hold opposite ends of the porous fuel material respectively. The porous fuel material comprises a large number of layers stacked one another in an axial direction of the combustion chamber.

REFERENCES:
patent: 3159104 (1964-12-01), Hodgson
patent: 3203174 (1965-08-01), Sutherland
Flittie, K.J., et al., "Hybrid Booster Strap-Ons for the Next Generation nch System", AIAA 93-2269, AIAA/SAE/ASME/ASEE 29th Joint Propulsion Conference and Exhibit, Jun. 28-30, 1993/Monterey, CA.
McFarlane, J.S., et al., "Design and Testing of AMRCO's 250,000 lbf Thrust Hybrid Motor", AIAA 93-2551, AIAA/SAE/ASME/ASEE 29th Joint Propulsion Conference and Exhibit, Jun. 28-30, 1993/Monterey, CA.
Goldberg, B., et al., "Preliminary Results of NASA/Industry Hybrid Propulsion Program", AIAA 92-3299, AIAA/SAE/ASME/ASEE 28th Joint Propulsion Conference and Exhibit, Jul. 6-8, 1992/Nashville, TN.

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