Booster rocket engine using gaseous hydrocarbon in...

Details Booster rocket engine using gaseous hydrocarbon in... Booster rocket engine using gaseous hydrocarbon in...

2008-06-24

2008-06-24

Kim, Ted (Department: 3746)

Power plants

Reaction motor

Method of operation

C060S258000, C060S259000, C060S260000, C060S267000

Reexamination Certificate

active

07389636

ABSTRACT:
A process and a system for delivering a propellant combination to a rocket engine is described. The process comprises the steps of providing a flow of a hydrocarbon propellant fuel, raising the pressure of the hydrocarbon propellant fuel, cracking the hydrocarbon propellant fuel in a cracker, introducing the cracked hydrocarbon propellant fuel into a combustion chamber of the rocket engine and introducing an oxidizer into the combustion chamber. A system for performing the process is also described.

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patent: 6470670 (2002-10-01), Maeding

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