Rocket nozzles for unconventional vehicles

Number of patents in Portfolio can not be more than 2000

United States of America Patent

PATENT NO 8601787
APP PUB NO 20120233983A1
SERIAL NO

13462909

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ATTORNEY / AGENT: (SPONSORED)

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Abstract

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Improved rocket nozzle designs for vehicles with nozzles embedded in or protruding from surfaces remote from the desired thrust axis. The nozzle configurations are for rocket vehicles where the nozzles are not located at the optimal thrust axis of the vehicle. Two examples include nozzles located on the forward end of the vehicle (also called tractor nozzles) and attitude control nozzles located on the periphery of the vehicle. More particularly, the disclosed nozzle shapes enhance the axial thrusts and/or maneuver torques on the vehicle. These unconventional nozzle shapes improve vehicle performance.

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Patent Owner(s)

Patent OwnerAddress
AEROJET ROCKETDYNE INCP O BOX 13222 SACRAMENTO CA 95813-6000

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Bulman, Melvin J Orangevale, US 34 300

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