Combined cycle missile engine system

Details Combined cycle missile engine system Combined cycle missile engine system

2007-11-08

2011-11-15

Kim, Ted (Department: 3741)

Power plants

Reaction motor

Interrelated reaction motors

C060S244000, C060S251000, C060S769000

Reexamination Certificate

active

08056319

ABSTRACT:
An insensitive combined cycle missile propulsion system includes a solid fuel contained within a first section of the missile, a liquid oxidizer contained within a second section of the missile and a solid oxidizer contained within a third section of said missile. A first conduit has a first valve communicating the fuel and the oxidizer and a second conduit, spatially removed from the first conduit, has a second valve communicating the fuel and the oxidizer. An inlet system for delivering atmospheric oxygen for combustion with the fuel rich gases generated within the missile and a nozzle exhausts combustion products that result from combustion of the fuel, the liquid and solid oxidizers, and air.

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