Lockheed Martin Corporation

Herbert Stephens Jones

Darren Andrew Kearney

Rory Nell McLeod

Ryan Earl Roberts

Joseph Paul Arves

A rocket engine ( ) generates a flow of hot propulsion fluid through a nozzle ( N) for generating propulsive thrust along a thrust vector Hybrid exhaust gas generators ( ) have their exhausts ( ) through the side of the nozzle. Each gas generator includes a fuel grain ( ) and a source of oxidizer ( ). The fuel grain is kept hot by either or both (a) direct radiation or conduction from the hot propulsion fluid, or (b) by a trickle of oxidizer. The fuel grain can thus react quickly to a substantial flow of oxidizer.

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Lacombe, LA, United States of America

Herbert Stephens Jones