History of liquid-propellant rocket engines in Russia, formerly the Soviet Union

被引：55
作者：
Sutton, GR
机构：
[1] The Boeing Company, Los Angeles, CA 90049, United States
来源：
JOURNAL OF PROPULSION AND POWER | 2003年 / 19卷 / 06期
关键词：
Combustion - History - Liquefied gases - Liquid propellants - Nozzles - Space flight;
D O I：
10.2514/2.6943
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
There have been many experimental and prototype liquid propellant rocket engines (LPREs) and engine components that were conceived, designed, built and tested, but for various reasons were never flown or produced in quantity, and most fell by the wayside. This paper covers some of the successful Russian LPREs. It also details a few other developments that have interesting technology or some historic significance.
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收藏
页码：1008 / 1037
页数：30
相关论文
共 48 条
[1]  
ANDRYEV AV, 1994, 943378 AIAA
[2]   From the history of research and design of Russian LOX/LH2 rocket engines [J].
Anufriev, VS ;
Goykhinberg, MM ;
Kalmykov, GP ;
Sirachev, MK .
ACTA ASTRONAUTICA, 1998, 43 (1-2) :19-21
[3]  
BIRIUKOV JV, 1997, AAS HIST SERIES, V19, P193
[4]  
BLAGONRAVOV AA, 1966, SOVIET ROCKETRY CONT
[5]  
*CHEM AUT DES BUR, 1997, RUSS SPAC B, V4
[6]  
DEMYENENKO YV, 2003, 20035072 AIAA
[7]  
DUSHKIN LS, 1986, 5 HIST S INT AC ASTR, V7, P79
[8]  
Gahun GG, 1989, CONSTRUCTION DESIGN
[9]  
GLUSHKO VP, 1975, DEV ROCKETRY SPACE E
[10]  
GLUSHKO VP, 1976, 16847 NASA TT F
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