Turbo-rocket thruster

Details Turbo-rocket thruster Turbo-rocket thruster

1999-05-27

2000-11-21

Thorpe, Timothy S.

Power plants

Reaction motor

Turborocket

F02K 500

Patent

active

061486094

ABSTRACT:
A turbo-rocket thruster is disclosed in which the turbine compressor is used to intake and compress a gaseous fuel for combustion with a stored oxidizer injected into the compressed gaseous fuel stream. The compressor stage is driven by the turbine stage, which is driven by burning gaseous fuel passing across the turbine blades. The burned gases are then expanded through an exhaust nozzle and thereby ejected to produce reaction thrust.

REFERENCES:
patent: 3849662 (1974-11-01), Blaskowski et al.
patent: 4212160 (1980-07-01), Blaskowski
patent: 4224790 (1980-09-01), Christensen
patent: 5012640 (1991-05-01), Mirville
patent: 5014507 (1991-05-01), Rice
patent: 5014508 (1991-05-01), Lifka
patent: 5063734 (1991-11-01), Morris
patent: 5101622 (1992-04-01), Bond
patent: 5778658 (1998-06-01), Lamando

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