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SCHEMES OF EXPERIMENTAL UNITS WITH PUMP-FEED SYSTEM COMPONENTS FUEL FOR TESTING OF PROPULSION SYSTEM UNITS OF ROCKET-SPACE SYSTEMS
https://doi.org/10.15518/isjaee.2016.09-10.82-094
Abstract
The creation of advanced rocket engines for rocket-space systems requires a large amount of autonomous tests of combustion chambers and gas generators in the experimental units with a pressure and pump-feed systems components of rocket fuel. The article describes the experimental units with the use of turbopump assembly with recirculating and closed loops of cord and different power schemes gas generator turbine drive unit, the recommendations for stabilization startup and modes of testing.
About the Authors
A. V. Galeev
Moscow Aviation Institute (National Research University)
Russian Federation
Russian Federation
4 Volokolamskoe drive, Moscow, GSP-3, A-80, 125993
Information about the author: postgraduate of “Management of operation of RSS” department of Moscow Aviation Institute (National Research University).
Education: Moscow Aviation Institute, 2014. Research area: theory and practice ground tests of rocket engines and propulsion systems.
Publications: 7.
A. G. Galeev
Research and Testing Center of rocket and space industry
Russian Federation
Russian Federation
9 Babuskinskaya, G. Peresvet. Moscow region, 141320
Information about the author: D.Sc. (engineering), professor, Laureate of USSR Council of Ministers in the field of science and technology, member of the RACTs, Chief Researcher of the PCF “SIC RSI”, professor of “Management of operation of RSS” of Moscow Aviation Institute (National Research University); scientific and pedagogical experience is 43 years. Participated in working out a number of systems for missile and space programs «Space-1», «Space-3», «N1L3», «EnergiaBuran», «GSLV», «Angara» and others.
Education: Kazan Aviation Institute, 1961. Research area: theory and practice ground tests of rocket engines and movingenforcement units; hydro and gas dynamics processes in power plants; research in the field of hydrogen technology.
Publications: more than 200, including 7 monographs, 6 textbooks, 44 patents for inventions.
V. V. Rodchenko
Moscow Aviation Institute (National Research University)
Russian Federation
Russian Federation
4 Volokolamskoe drive, Moscow, GSP-3, A-80, 125993
Information about the author: D.Sc. (engineering), professor, Honorary Worker of Higher School, member of the K.E. Tsiolkovsky Russian Academy of Cosmonautics, the Deputy Head of the “Management of operation of RSS” department of Moscow Aviation Institute (National Research University); scientific and pedagogical experience is more than 40 years. He was a leader and participated in the implementation of a number of contractual works on the orders of the industry, including the following programs: “EnergiaBuran”, “Highway”, “The blue”, etc.
Education: Moscow Aviation Institute, 1970. Research area: theory and practice of jet devices that can move in the ground at high speeds; testing of complex technical systems.
Publications: more than 180, including 7 monographs, 9 textbooks, 4 patents for inventions.
References
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Review
For citations:
Galeev A.V., Galeev A.G., Rodchenko V.V. SCHEMES OF EXPERIMENTAL UNITS WITH PUMP-FEED SYSTEM COMPONENTS FUEL FOR TESTING OF PROPULSION SYSTEM UNITS OF ROCKET-SPACE SYSTEMS. Alternative Energy and Ecology (ISJAEE). 2016;(9-10):82-94. (In Russ.) https://doi.org/10.15518/isjaee.2016.09-10.82-094
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