Thermal control of monopropellant catalytic decomposition hydrazine engines in important portion of space propulsive system.
单组元肼分解发动机的热控制与热分析是空间推进系统重要组成部分。
Nanometer metal powders also have catalytic effects on the thermal decomposition of AP/HTPB solid propellant.
纳米金属粉对AP/HTPB推进剂的热分解同样具有一定的催化效果。
The present electrode had the characters of low platinum loading and high catalytic performance which was higher than counter electrodes prepared by thermal decomposition and platinum foil.
所制备的电极具有载铂量低、催化活性高的特性，比纯铂片对电极以及热解法制备的载铂对电极具有更高的活性。
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