| 摘要 |
This invention relates to a process for the spontaneous catalytic decomposition of rocket propellants containing hydrazine or mixtures of hydrazine and hydrazine nitrate. The catalyst used in this invention retains its activity after exposure to the propellant flame environment thereby permitting multiple starts of a rocket engine. The catalyst consists of molybdenum metal and cobalt metal coated on a high surface area support body such as alumina.
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