Encyclopedia Astronautica
RD-0101


Kosberg Lox/Alcohol rocket engine. 39.2 kN. E-50A aircraft by Mikoyan. Out of Production. Chamber pressure 42,7 - 22,1 bar. Specific impulse 255 - 248,5 sec. Isp=255s.

Application: E-50A aircraft by Mikoyan.

Throttled thrust(vac): 19.600 kN (4,406 lbf). Chamber Pressure: 42.70 bar.

AKA: SK1; RD-0101.
Status: Out of Production.
Thrust: 39.20 kN (8,813 lbf).
Specific impulse: 255 s.
Burn time: 300 s.
First Launch: 1954-58.

More... - Chronology...


Associated Countries
See also
Associated Manufacturers and Agencies
  • Kosberg Russian manufacturer of rocket engines. Kosberg Design Bureau, Russia. More...

Associated Propellants
  • Lox/Alcohol Liquid oxygen was the earliest, cheapest, safest, and eventually the preferred oxidiser for large space launchers. Its main drawback is that it is moderately cryogenic, and therefore not suitable for military uses where storage of the fuelled missile and quick launch are required. Alcohol (C2H5OH) was the fuel used for the German V-2 rocket, and the first derivative rocket engines in the United States, Soviet Union, and China used it as well. Better performance was achieved by increasing the alcohol concentration in the post-war engines. But after better-performance rocket-grade kerosene was developed by Rocketdyne in the REAP program of 1953, use of alcohol was abandoned. More...

Bibliography
  • Golubev, A A, KB KhimAvtomatiki - Straniy Istorii, Vol. 1, Voronezh 1995 via Dietrich Haeseler.
  • Siddiqi, Asif A, Soviet Space Web Page, 1999 via Dietrich Haeseler. Web Address when accessed: here.
  • Ivanenko, V N, "O Zhizn i Deyatelnosti S.A. Kosberg", Issled. Po Ist. I Teorii Razv. Aviat. i Raketo-Kosm. Nauki i Tekhniki, AN SSSR, Moscow 1986.

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