Rocket-ramjet engine casing port closure

Power plants – Reaction motor – Method of operation

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Details

60245, 137 151, F02K 718

Patent

active

057848777

ABSTRACT:
The present invention discloses a composite material closure as a port cover for a rocket-ramjet engine and a method of transitioning between rocket booster operation and ramjet operation. The composite material closure is made to be coextensive with an insulating lining of the casing of the rocket-ramjet engine. Pyrotechnic charge devices are associated with the composite material closure and ignited to cut there-through and form an opening in the closure for air flow during ramjet operation.

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patent: 4841724 (1989-06-01), Hall et al.
patent: 5347807 (1994-09-01), Brossier et al.

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