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1.
公开(公告)号:EP0959058A1
公开(公告)日:1999-11-24
申请号:EP98201696.6
申请日:1998-05-20
摘要: 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.
摘要翻译: 本发明涉及一种用于火箭发动机,气体发生器和类似装置的固体推进剂,其包含硝基甲酸a和不饱和羟基封端的烃化合物的固化组合物。