Hydrazinium nitroformate based high performance solid...

C - Chemistry – Metallurgy – 06 – B

Patent

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C06B 47/08 (2006.01) C06B 25/36 (2006.01)

Patent

CA 2333211

The present invention is directed to a solid propellant for rocket motors, gas generators and comparable devices, comprising a cured composition of hydrazinium nitroformate and an unsaturated hydroxyl terminated hydrocarbon compound.

La présente invention a trait à un ergol solide pour moteurs-fusées, générateurs de gaz et autres dispositifs comparables, qui comporte une composition durcie de nitroformate d'hydrazinium et un composé d'hydrocarbure à terminaison hydroxyle insaturé.

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