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HYPERGOLIC IGNITION SYSTEM FOR GELLED ROCKET PROPELLANT
HYPERGOLIC IGNITION SYSTEM FOR GELLED ROCKET PROPELLANT
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机译:胶凝火箭推进剂超高压点火系统
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摘要
The present invention provides a composition and a system for hypergolic ignition of rocket propellant. The composition includes the suspension of catalytic or reactive particles in a gelled fuel. The catalytic or reactive particles initiate a reaction upon contact with an oxidizer.
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