Hypergolic ignition systems bear many resemblances to hybrid rockets. 自然式点火系统在很多方面与混合型火箭相似。
A set of device was established in order to test and compare hypergolic dela... 研究表明,过氧化氢/醇类这种新型双组元推进剂具有良好的自燃和点火特性。
C6H15N and HNO3-27S can be used as hypergolic propellant in rocket engines. 三乙胺和硝酸-27S作为自燃推进剂可应用于火箭发动机中。
Experimental studies of a gas generator based on hydrogen peroxide and hypergolic ethanol[J]. 引用该论文 陈志强;廖达雄;刘宗政;符松.
The effort of spray characteristic on rocket engine combustion stability for hypergolic propellant (MMH/NTO) was studied. 用数值方法研究了一甲基肼/四氧化二氮自燃推进剂（MMH/NTO）喷雾液滴直径对火箭发动机燃烧稳定性的影响。
Louis Larosiliere , Ron Litchford , San-Mou Jeng. Hypergolic Bipropellant Spray Combustion and Flow Modeling in Rocket Engines[R]. AIAA 90-2238. 庄逢辰.;液体火箭发动机喷雾燃烧的理论、模型及应用[M]
