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Ignition Delay Measurements of Liquid Hypergolic Bipropellants under Inert and Active Atmospheres at Ordinary Combustion Pressures of Rocket Motors

机译：火箭电机普通燃烧压力下惰性和活性环境下液体高温百分点液体高温百分点的点火延迟测量

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Akira Iwama; Kiroku Yamazaki;
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年度 1963
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1. Nonaborane and Decaborane Cluster Anions Can Enhance the Ignition Delay in Hypergolic Ionic Liquids and Induce Hypergolicity in Molecular Solvents [J] . Parker D. McCrary, Patrick S. Barber, Steven P. Kelley, Inorganic Chemistry: A Research Journal that Includes Bioinorganic, Catalytic, Organometallic, Solid-State, and Synthetic Chemistry and Reaction Dynamics . 2014,第9期

机译：九硼烷和十硼烷簇阴离子可增强高离子离子液体的点火延迟并诱导分子溶剂中的超高极性
2. A LINEAR STABILITY ANALYSIS OF OSCILLATORY COMBUSTION INDUCED BY COMBUSTION TIME DELAYS OF LIQUID OXIDIZER IN HYBRID ROCKET MOTORS [J] . Takakazu Morita, Koki Kitagawa, Toru Shimada, International journal of energetic materials and chemical propulsion . 2014,第1期

机译：混合火箭发动机液化剂燃烧时间延迟引起的振荡燃烧线性稳定性分析。
3. Hypergolic ignition delay studies of solidified ethanol fuel with hydrogen peroxide for hybrid rockets [J] . John Jerin, Nandagopalan Purushothaman, Baek Seung Wook, Combustion and Flame . 2020,第Feba期

机译：混合火箭氢过氧化氢固体乙醇燃料的高压点火延迟研究
4. Thrust Prediction Model for Varying Chamber Pressure for a Hypergolic Bipropellant Liquid Rocket Engine [C] . P. Arun Kumar, C. Rajeev Senan, B. Ajith, International Conference on Innovative Design , Analysis and Development Practices in Aerospace and Automotive Engineering . 2019

机译：用于高胆玻璃液体火箭发动机的不同室压力的推力预测模型
5. Effects of impingement and shear upon the ignition of hypergolic rocket bipropellants. [D] . Funk, John. 2003

机译：冲击和剪切对高目标火箭双推进剂着火的影响。
6. Transformation of Combustion Nanocatalysts inside Solid Rocket Motor under Various Pressures [O] . Jun-Qiang Li, Linlin Liu, Xiaolong Fu, 2019

机译：固体火箭发动机内燃烧纳米催化剂在不同压力下的转化
7. Effect of Some Parameters on the Ignition Delay of Hypergolic Bipropellants (II) The Variation under Pressurized Atmosphere [O] . Akira Iwama, Kiroku Yamazaki 1960

机译：一些参数对高胆伏特（II）加压气氛中的变化的影响

Ignition Delay Measurements of Liquid Hypergolic Bipropellants under Inert and Active Atmospheres at Ordinary Combustion Pressures of Rocket Motors

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