A.M. Isayev Chemical Engineering Design Bureau
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Native name | Конструкторское бюро химического машиностроения имени A.M. Исаева |
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Romanized name | Chemical Engineering Design Bureau named after A.M. Isayev |
Formerly | OKB-2 |
Company type | subsidiary |
Industry |
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Predecessor | NII-88 |
Founded | 1948 Podlipki (Korolyov), Soviet Union |
Founder | Aleksei Mihailovich Isaev |
Headquarters | 12 Bogomolov street, Korolyov (Russian: ул. Богомолова, д. 12, Королёв), , |
Key people | Igor G. Panin |
Products | |
Parent | Khrunichev State Research and Production Space Center |
Website | Official Website |
Footnotes / references [1][2][3][4] |
The A.M. Isayev Chemical Engineering Design Bureau (Russian: Конструкторское бюро химического машиностроения имени A.M. Исаева), also known as KB KhimMash or just KBKhM, is a Russian rocket engine design and manufacturing company. It is located in the city of Korolyov. It started as the OKB-2 division of the NII-88 research institute, where A.Isaev directed the development of liquid rocket engines for ballistic missile submarines.
Products
[edit]Current engines
[edit]Engines in current production:
- Monopropellant Thrusters[5]
- DOT-5
- DOT-25
- MLC-10
- MLC-50
- Bipropellant Thrusters[5]
- S5.142 (DST-25)
- DST-50
- DST-100
- DST-100A
- DST-200
- DST-200A
- DMT-6
- DMT-500
- DMT-600
- DMT-1000
- DMT-2200
- Main propulsion[6]
- Propulsion Modules
- Experimental Engines
- S5.86.1000-0
Former engines
[edit]Engines that are no longer produced.
- Monopropellant Thrusters[7]
- Bipropellant Thrusters[7]
- S5.144: Used on the control module 17D61 of the Ikar.
- S5.205
- Orbit Correction Engines
- S5.4: Liquid engine burning TG-02 and AK20F in the gas generator cycle. Used to deorbit Vostok, Voskhod and Zenit.[8]
- S5.35: Backup engine of the KTDU-35.
- S5.53: Orbital correction engine for the lunar version of the Soyuz.
- S5.60: Main engine of the KTDU-35.
- S5.66: Maneuvering engine version for the Salyut 1 and Salyut 4 stations. Also was composed of primary and secondary engines.
- S5.79: Pressure-fed rocket engine burning N2O4/UDMH. Used as the main orbital engine of Salyut-6, Salyut-7, Mir Core Module and Zvezda.[7]
- Propulsion Modules
- KDU-414: Pressure-fed liquid rocket engine burning UDMH and RFNA. Used on early soviet deep space probes.
- KTDU-35: Liquid rocket engine burning UDMH and AK27I in the gas generator cycle. Used on first generation Soyuz, and Progress.[7]
- KTDU-425: Pump-fed liquid rocket engine. Used on the 4MV bus employed by unmanned Mars and Venus probes.
- KTDU-426: Spacecraft version of the S5.79. Used on the Soyuz-T.[9]
- Military Missiles[7]
- RD-1
- RD-1M
- Y-1250
- U-400-10
- PT 45-2
- SU-1500
- Y-2000
- S09.19A?
- S09.29A S09.29.0-0
- S09.29D
- S09.29B
- S09.29.0-OV?
- S09.29.0-OV?
- S2.145
- S2.145
- S2.168A
- S2.168B
- S2.219
- S.911.0100 S2.219?
- S2.244
- S2.258
- S2.260
- S2.268
- S2.514
- S2.711
- S2.711V S2.711V1
- S2.720
- S2.720.A2
- S2.720M
- S2.721 S2.721V
- S2.722
- S2.722V
- S2.726
- S2.727
- S2.751V?
- S2.1100: A TG-02/AK20K burning engine. Development years: 1955–1958. For use in the booster module of the Burya intercontinental cruise missile project.[10][11]
- S2.1150: An improved version of the S2.1100. Development years: 1958–1960. For use in the booster module of the Burya project.[10][11]
- S2.1200
- S5.1
- S.5.6.0000.0
- S5.15
- S5.33
- S5.33A S5.33M
- S5.41
- S5.44 5D25
- S5.57
- S5.44 5D25
- 5D25N
- S5.83
- Rocket engines for ICBM and SLBM[7]
- S2.253 (8D511): A kerosene/AK20 burning engine in the pressure fed cycle. Development years: 1951-1955 . For use in first versions of Scud-A. Ignition by hypergolic start fuel TG-02.
- S2.253A: A kerosene/AK-20 burning engine in the pressure fed cycle. Development years: 1953-1959 . For use in the RSM-11FM. Ignition by hypergolic start fuel TG-02.
- S2.713: A TG-02/AK27I burning engine in the gas generator cycle. Development years: 1956-1961 . For use in the R-13. It included a fixed nozzle and four verniers.
- S5.2 (9D21): A TM-185/AK-27I burning engine in the gas generator cycle. Development years: 1959-1962 . For use in the R-17.
- S5.3: A TG-02/AK-27I burning engine in the gas generator cycle. Development years: 1958-1963 . For use in the R-21.
- S5.3M: A TG-02/AK-27I burning engine in the gas generator cycle. Development years: 1960. Project for the ICBM R-9B.
- 4D10: A UDMH/N2O4 burning engine in the staged combustion cycle. Development years: 1962-1968 . For use as main engine of the first stage of R-27. First engine submerged in the propellant tank.
- 4D10: A UDMH/N2O4 burning engine in the gas generator cycle. Development years: 1963-1968 . For use as the steering engine of the first stage of the R-27. Submerged in the propellant tank.
- 4D76: A UDMH/N2O4 burning engine in the gas generator cycle. Development years: 1964-1971 . For use as main engine of the second stage of R-29. Submerged in the propellant tank.
- 4D76M: A UDMH/N2O4 burning engine in the gas generator cycle. Development years: 1969-1970 . Improved version of the 4D-76.
- 4D28: A UDMH/N2O4 burning engine in the gas generator cycle. Development years: 1968-1970 . For use on the second stage of the rocket RSM-27K.
- 3D20: A UDMH/N2O4 burning engine in the staged combustion cycle. Development years: 1971-1973 . For use as main engine RSM-27U.
- 3D20: A UDMH/N2O4 burning engine in the gas generator cycle. Development years: 1971-1973 . For use as steering engine R-27U.
- 3D41: A UDMH/N2O4 burning engine in the gas generator cycle. Development years: 1973-1975 . For use on the second stage of R-29R. Submerged in the propellant tank.
- 3D42: A UDMH/N2O4 burning engine in the gas generator cycle. Development years: 1973-1975 . For use on warhead of the R-29R . Four fixed main combustion chambers and four verniers.
- 3D67?: A UDMH/N2O4 burning engine in the gas generator cycle. Development years: 1976-1980 . For use on warhead of the R-39. Dual-mode rocket engine with multiple regimen.
- 3D36: A UDMH/N2O4 burning engine in the gas generator cycle. Development years: 1980-1986 . For use on warhead of the R-29RM.
- 3D38: A UDMH/N2O4 burning engine in the staged combustion cycle. Development years: 1980-1986 . For use on the second stage R-29RM. Submerged in the propellant tank.
- 3D39: A UDMH/N2O4 burning engine in the staged combustion cycle. Development years: 1980-1986 . For use on the third stage R-29RM. Submerged in the propellant tank.
See also
[edit]- NII-88 — The research institute where KB KhimMash started as OKB-2 division.
- Khrunichev State Research and Production Space Center — The corporate parent of KBKhM.
- United Rocket and Space Corporation — The government owned corporate entity that will encompass all aerospace corporations in Russia.
References
[edit]- ^ "Краткая история нашего предприятия" [A brief history of our company] (in Russian). KB KhimMash. Archived from the original on 19 August 2011.
- ^ "Руководство" [Leadership] (in Russian). KB KhimMash. Archived from the original on 23 April 2013.
- ^ "Основные направления деятельности" [Main Activities] (in Russian). KB KhimMash. Archived from the original on 19 August 2011.
- ^ "Этапы истории КБХМ им. А.М. Исаева" [Milestones A.M. Isayev KBKhM] (in Russian). KB KhimMash. Archived from the original on 23 April 2013.
- ^ a b "ЖРДМТ от 0,5 кгс до 250 кгс" [Small thrust jet engine from 0.5 kgf to 250 kgf] (in Russian). KB KhimMash. Archived from the original on 23 April 2013.
- ^ "Двигатели тягой от 250 кгс до 50 тс" [Engines with thrust of 250 kg to 50 tonnes] (in Russian). KB KhimMash. Archived from the original on 23 April 2013.
- ^ a b c d e f Ponomarenko, Alexander. "Основные двигатели разработки КБХМ" [The main engines produced by KBKhM]. LPRE.DE (in Russian). Retrieved 2015-07-25.
- ^ Brügge, Norbert. "Spacecraft-propulsion blocks (KDU) from Isayev's design bureau (now KB KhimMash)". B14643.de. Archived from the original on 2015-06-02. Retrieved 2015-07-30.
- ^ "Двигатели 1944-2000: Аавиационные, Ракетные, Морские, Промышленные" [Aviadvigatel 19442-2000: Aviation, rocketry, naval and industry] (PDF) (in Russian). pp. 75–81. Retrieved 2015-07-25.
- ^ a b "Isayev". Encyclopedia Astronautica. Archived from the original on 2016-08-08. Retrieved 2015-07-30.
- ^ a b Brügge, Norbert. "Some identified rocket-engines from Isayev's Design Bureau (now KB KhimMash)". B14643.de. Archived from the original on 2015-10-17. Retrieved 2015-07-30.