Stable-combustion oxidizer for hybrid rockets

Details Stable-combustion oxidizer for hybrid rockets Stable-combustion oxidizer for hybrid rockets

1998-02-20

2000-06-13

Kim, Ted

Power plants

Reaction motor

Method of operation

60251, 60259, F02K 972, F02K 950

Patent

active

06073437&

ABSTRACT:
A hybrid heater vaporization system (280, 380) including hybrid heaters (250, 350) can be used to vaporize liquid oxygen as it enters a motor (200, 300) to improve the combustion characteristics of a hybrid rocket (11). The motor (200, 300) preferably includes hybrid fuel both in a substantially cylindrical portion (216, 316) in the substantially cylindrical portion of the motor and a substantially multi-toroidal shaped portion (217, 316) in the forward end of the motor (200, 300). The vaporization system (280, 380) of the present invention finally makes hybrid rockets (11) practical for aerospace applications.

REFERENCES:
patent: 2408111 (1946-09-01), Traux et al.
patent: 2935846 (1960-05-01), Neale et al.
patent: 2996880 (1961-08-01), Greiner
patent: 3065596 (1962-11-01), Schultz
patent: 3098353 (1963-07-01), Abild
patent: 3136119 (1964-06-01), Avery
patent: 3170295 (1965-02-01), Dryden
patent: 3178885 (1965-04-01), Loughran
patent: 3295323 (1967-01-01), Holzman
patent: 3334489 (1967-08-01), Vilet
patent: 3340691 (1967-09-01), Mangum
patent: 3443475 (1969-05-01), Berton
patent: 3516251 (1970-06-01), Andrews et al.
patent: 3518828 (1970-07-01), Bradford et al.
patent: 3570249 (1971-03-01), Baum et al.
patent: 3595020 (1971-07-01), Untherhaching et al.
patent: 3613583 (1971-10-01), Lai et al.
patent: 3782112 (1974-01-01), Muzzy
patent: 3788069 (1974-01-01), Schmidt
patent: 3789610 (1974-02-01), Stone
patent: 3803858 (1974-04-01), Simon
patent: 3893294 (1975-07-01), Brunn et al.
patent: 3943706 (1976-03-01), Grafwallner et al.
patent: 4286431 (1981-09-01), Reichard et al.
patent: 4424679 (1984-01-01), Holzman
patent: 4589253 (1986-05-01), Wagner
patent: 5010730 (1991-04-01), Knuth et al.
patent: 5099645 (1992-03-01), Schuler et al.
patent: 5119627 (1992-06-01), Bradford et al.
patent: 5133183 (1992-07-01), Asaoka et al.
patent: 5152136 (1992-10-01), Chew et al.
patent: 5274998 (1994-01-01), Geisler
patent: 5339625 (1994-08-01), McKinney et al.
patent: 5471833 (1995-12-01), Pahl
patent: 5572864 (1996-11-01), Jones
patent: 5582001 (1996-12-01), Bradford et al.
patent: 5722232 (1998-03-01), Jones

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