Fuel strip

Power plants – Reaction motor – Solid and fluid propellant

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Details

60253, 60257, 60260, F02K 928

Patent

active

057181136

ABSTRACT:
A fuel member comprises a continuous, elongated, flexible and combustible structural component that has a length to width of ratio greater than 100:1, and contains within the structural component, either as a part thereof or as a separate component, an oxidizer in an amount sufficient to support combustion of the fuel member. The fuel member is essentially self-supporting in that it does not require containment tanks or rigid encasement, and therefore is particularly suitable for use in single stage, reusable rocket propulsion systems.

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Table I Experimental hybrid combustion studies; Hetrogeneous Combustion; Edited by Wolfhard, Glassman, and Green Jr.; pp. 476, 477; Academic Press; New York/London 1964.
The Chemistry of Propellants; Agard Combustion and Propulsion Panel, Paris France; Jun. 8-12, 1959; Penner and Ducarme, Ed.; pp. 378, 379; Pergamon Press; Oxford et al.; 1960.
A Solid-Liquid Rocket Propellant System; Moore and Berman; Jet Propulsion, Nov. 1956; pp. 965-968.

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