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Experimental performance of the mixed-oxides-of-nitrogen-ammonia propellant combination in a 1000-pound-thrust rocket engine

机译：混合氧化氮 - 氨 - 推进剂组合在1000磅推力火箭发动机中的实验性能

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Tomazic, William A; Kinney, George R;
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年度 1955
页码 1-30
总页数 30
原文格式 PDF
正文语种 eng
中图分类工业技术;
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2. Correction Numerical and experimental investigations of the effect of repeated cyclic thermal loads on the strength of materials of recoverable liquid-propellant rocket engines [J] . Bubnov VI, Isakov DV, Lozino-Lozinskaya IG, Journal of engineering thermophysics . 2009,第1期

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3. Numerical and Experimental Investigations of the Effect of Repeated Cyclic Thermal Loads on the Strength of Materials of Recoverable Liquid-Propellant Rocket Engines [J] . V. I. Bubnov, D. V. Isakov, I. G. Lozino-Lozinskaya, Journal of engineering thermophysics . 2008,第4期

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5. Aluminum/hydrocarbon gel propellants: An experimental and theoretical investigation of secondary atomization and predicted rocket engine performance. [D] . Mueller, Donn Christopher. 1997

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Experimental performance of the mixed-oxides-of-nitrogen-ammonia propellant combination in a 1000-pound-thrust rocket engine

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