C - Chemistry – Metallurgy – 06 – B
Patent
C - Chemistry, Metallurgy
06
B
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.
Elands Petrus Johannes Maria
Louwers Jeroen
Van Der Heijden Antonius Eduard Dominicus Maria
Bereskin & Parr Llp/s.e.n.c.r.l.,s.r.l.
Nederlandse Organisatie Voor Toegepast-Natuurwetenschappelijk On
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