Combustible outgassing material lined altitude compensating...

Details Combustible outgassing material lined altitude compensating... Combustible outgassing material lined altitude compensating...

2001-08-29

2010-10-19

Eldred, J. Woodrow (Department: 3641)

Aeronautics and astronautics

Aircraft propulsion

Launching

C244S171100, C244S172200, C060S242000, C060S233000, C060S255000, C060S251000

Reexamination Certificate

active

07815146

ABSTRACT:
A fixed sized bell rocket nozzle is lined with a layer of combustible material that is ignited during launch ignition and burns to outgas into the rocket exhaust for spatially variably confining the exhaust and perfecting an effective variably sized altitude compensating exhaust nozzle that maximizes lift during the launch of a spacecraft into orbit.

REFERENCES:
patent: 4821510 (1989-04-01), Graser et al.
patent: 5579635 (1996-12-01), Miskelly et al.
patent: 6220852 (2001-04-01), Moore
patent: 6233919 (2001-05-01), Abel et al.

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