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on the basis of nitroform hochleistungsfesttreibstoff hydrazine
on the basis of nitroform hochleistungsfesttreibstoff hydrazine
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机译:基于硝基仿高性能固体推进剂肼
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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.
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