Missile thrust system and valve with refractory piston cylinder

Fluid handling – With casing – support – protector or static constructional... – Jacketed

Reexamination Certificate

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C251S368000, C060S254000, C420S433000, C148S407000

Reexamination Certificate

active

06895991

ABSTRACT:
An improved pneumatic valve and a missile with an improved thrust directional valve. In one embodiment, a refractory material lining for a pneumatic valve enables better valve operation and better valve performance. A thin-wall cylindrical sleeve of rhenium or other suitable refractory metal is located inside a cylinder. A valve piston may then travel within the refractory sleeve with greater reliability and better operation. The refractory sleeve cylinder lining can be subject to high temperatures at a rapid rate and remain operational. Under such a hostile environmental, including corrosive/erosive environments created by the passage of hot propellant gasses, the refractory cylinder sleeve has a more reliable operational life and is lighter in weight than conventional valves made entirely of refractory metals.

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