首页> 美国政府科技报告 >Experimental research and design planning in the field of liquid-propellant rocket engines conducted between 1934 - 1944 by the followers of F. A. Tsander

【24h】

Experimental research and design planning in the field of liquid-propellant rocket engines conducted between 1934 - 1944 by the followers of F. A. Tsander

机译：1934年至1944年由F. a. Tsander的追随者在液体推进剂火箭发动机领域进行的实验研究和设计规划

获取原文

页面导航

摘要
著录项
相似文献
相关主题

摘要

The development of the following Liquid-Propellant Rocket Engines (LPRE) is reviewed: (1) an alcohol-oxygen single-firing LPRE for use in wingless and winged rockets, (2) a similar multifiring LPRE for use in rocket gliders, (3) a combined solid-liquid propellant rocket engine, and (4) an aircraft LPRE operating on nitric acid and kerosene.

著录项

作者
Dushkin, L. S.;
展开▼
作者单位

展开▼
年度 1977
页码 1-19
总页数 19
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
HISTORIES; LIQUID PROPELLANT ROCKET ENGINES; ROCKET ENGINE DESIGN; U.S.S.R. SPACE PROGRAM; PROPULSION SYSTEM CONFIGURATIONS; ROCKET PLANES; ROCKET PROPELLANTS;

机译：历史;液体推进剂火箭发动机;火箭发动机设计; U.s.s.R.空间计划;推进系统配置;火箭飞机;火箭推进剂;

相似文献

外文文献
专利

1. 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

机译：校正数值和实验研究对重复循环热负荷对可回收液 - 推进剂火箭发动机材料强度的影响
2. 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

机译：反复循环热负荷对可回收液体推进火箭发动机材料强度影响的数值和实验研究
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

机译：反复循环热负荷对可回收液体推进火箭发动机材料强度影响的数值和实验研究
4. Experimental Evaluation of Rational Pre-launch Acceleration Parameters to Provide Liquid-Propellant Rocket Sustainer Engine Launch in Microgravity [C] . V.B. Sapozhnikov, A.V. Korolkov, A.A. Malashin, Academic Space Conference . 2019

机译：Rational预推出加速度参数的实验评估，提供液体推进剂的液体推进式火箭持有子发动机发射
5. Erratum to: “Numerical and experimental investigations of the effect of repeated cyclic thermal loads on the strength of materials of recoverable liquid-propellant rocket engines” [O] . V. I. Bubnov, D. V. Isakov, I. G. Lozino-Lozinskaya, 2009

机译：误解：“对重复循环热负荷对可回收液 - 推进式火箭发动机材料强度的数值和实验研究”

Experimental research and design planning in the field of liquid-propellant rocket engines conducted between 1934 - 1944 by the followers of F. A. Tsander

摘要

著录项

相似文献

相关主题

期刊订阅