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词条 A.M. Isayev Chemical Engineering Design Bureau
释义

  1. Products

     Current engines  Former engines 

  2. See also

  3. References

  4. External links

{{Infobox company
| name = A.M. Isayev Chemical Engineering Design Bureau
| logo = A.M._Isayev_Chemical_Engineering_Design_Bureau_logo.png
| logo_size = 150px
| logo_alt =
| logo_caption =
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| image =
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| image_caption =
| trading_name =
| native_name = Конструкторское бюро химического машиностроения имени A.M. Исаева
| native_name_lang = ru
| romanized_name = Chemical Engineering Design Bureau named after A.M. Isayev
| former_name = OKB-2
| type = subsidiary
| traded_as =
| ISIN =
| industry = {{ublist |Liquid rocket engine manufacturing| equipment for heat treatment of meat and fish| medical equipment| common consumption goods| }}
| genre =
| fate =
| predecessor = NII-88
| successor =
| founded = 1948 Podlipki, Soviet Union
| founder = Aleksei Mihailovich Isaev
| defunct =
| hq_location = 12 Bogomolov street, Korolyov (Russian: {{lang|ru|ул. Богомолова, д. 12, Королёв}})
| hq_location_city = Moscow region
| hq_location_country = Russia
| coordinates =
| num_locations =
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| area_served =
| key_people = Igor G. Panin
| products = {{ublist |S5.92 |KTDU-80 S5.142}}
| brands =
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| parent = Khrunichev State Research and Production Space Center
| divisions =
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| website = {{URL|http://kbhmisaeva.ru/|Official Website}}
| footnotes = [1][2][3][4]
| intl =
}}

The A.M. Isayev Chemical Engineering Design Bureau (Russian: {{lang|ru|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

Current engines

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[7]
    • S5.80
    • S5.92
    • S5.98
    • KVD-1
  • Propulsion Modules
    • KTDU-80
  • Experimental Engines
    • С5.86.1000-0

Former engines

Engines that are no longer produced.

  • Monopropellant Thrusters[8]
    • S5.70: Used on Phobos 1 spacecraft.
    • S5.70: Used on Phobos 1 spacecraft.
  • Bipropellant Thrusters[8]
    • 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.[10]
    • 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.[8]
  • Propulsion Modules
    • KTDU-35: Liquid rocket engine burning UDMH and AK27I in the gas generator cycle. Used on first generation Soyuz, and Progress.[8]
    • KTDU-426: Spacecraft version of the S5.79. Used on the Soyuz-T.
  • Military Missiles[8]
    • 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.[15][16]
    • S2.1150: An improved version of the S2.1100. Development years: 1958-1960. For use in the booster module of the Burya project.[15][16]
    • S2.1200
    • C5.1
    • S.5.6.0000.0
    • S5.15
    • C5.33
    • C5.33A C5.33M
    • S5.41
    • S5.44 5D25
    • S5.57
    • S5.44 5D25
    • 5D25N
    • C5.83
  • Rocket engines for ICBM and SLBM[8]
    • 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.
    • C5.3: 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.
    • 4D-10: 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.
    • 4D-10: 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.
    • 4D-76: 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.
    • 4D-76M: A UDMH/N2O4 burning engine in the gas generator cycle. Development years: 1969-1970 . Improved version of the 4D-76.
    • 4D-28: 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.
    • 3D-20: A UDMH/N2O4 burning engine in the staged combustion cycle. Development years: 1971-1973 . For use as main engine RSM-27U.
    • 3D-20: A UDMH/N2O4 burning engine in the gas generator cycle. Development years: 1971-1973 . For use as steering engine R-27U.
    • 3D-41: 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.
    • 3D-42: 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.
    • 3D-67?: 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.
    • 3D-36: A UDMH/N2O4 burning engine in the gas generator cycle. Development years: 1980-1986 . For use on warhead of the R-29RM.
    • ZD-38: 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.
    • 3D-39: 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

{{Portal|Companies}}
  • Isayev — Founder and director of the company until 1975.
  • 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

1. ^1 {{cite web|url=http://www.b14643.de/Spacerockets/Diverse/KB-Isayev_KDUs/index.htm |title=Spacecraft-propulsion blocks (KDU) from Isayev's design bureau (now KB KhimMash) |first=Norbert |last=Brügge |publisher=B14643.de |accessdate=2015-07-30 |deadurl=yes |archiveurl=https://web.archive.org/web/20150602231608/http://www.b14643.de/Spacerockets/Diverse/KB-Isayev_KDUs/index.htm |archivedate=2015-06-02 |df= }}
2. ^1 2 {{cite web|url=http://www.b14643.de/Spacerockets/Diverse/KB-Isayev_engines/index.htm |title=Some identified rocket-engines from Isayev's Design Bureau (now KB KhimMash) |first=Norbert |last=Brügge |publisher=B14643.de |accessdate=2015-07-30 |deadurl=yes |archiveurl=https://web.archive.org/web/20151017052056/http://www.b14643.de/Spacerockets/Diverse/KB-Isayev_engines/index.htm |archivedate=2015-10-17 }}
3. ^1 2 {{cite web |url=http://www.astronautix.com/astros/isayev.htm |title=Isayev |publisher=Encyclopedia Astronautica |accessdate=2015-07-30 |deadurl=yes |archiveurl=https://web.archive.org/web/20171108000000/http://www.astronautix.com/astros/isayev.htm |archivedate=2017-11-08 |df= }}
4. ^1 {{cite web |url=http://kbhmisaeva.ru/main.php?id=32 |title=Двигатели тягой от 250 кгс до 50 тс |trans-title=Engines with thrust of 250 kg to 50 tonnes |publisher=KB KhimMash |language=Russian |accessdate=2015-07-25}}
5. ^1 {{cite web |url=http://kbhmisaeva.ru/main.php?id=22 |title=Краткая история нашего предприятия |trans-title=A brief history of our company |publisher=KB KhimMash |language=Russian |accessdate=2015-07-30}}
6. ^1 {{cite web |url=http://kbhmisaeva.ru/main.php?id=28 |title=Руководство |trans-title=Leadership |publisher=KB KhimMash |language=Russian |accessdate=2015-07-30}}
7. ^1 {{cite web |url=http://kbhmisaeva.ru/main.php?id=23 |title=Основные направления деятельности |trans-title=Main Activities |publisher=KB KhimMash |language=Russian |accessdate=2015-07-30}}
8. ^1 {{cite web |url=http://kbhmisaeva.ru/main.php?id=27 |title=Этапы истории КБХМ им. А.М. Исаева |trans-title=Milestones A.M. Isayev KBKhM |publisher=KB KhimMash |language=Russian |accessdate=2015-07-30}}
9. ^1 2 {{cite web |url=http://kbhmisaeva.ru/main.php?id=33 |title=ЖРДМТ от 0,5 кгс до 250 кгс |trans-title=Small thrust jet engine from 0.5 kgf to 250 kgf |publisher=KB KhimMash |language=Russian |accessdate=2015-07-25}}
10. ^1 2 3 4 5 6 {{cite web |url=http://lpre.de/kbhm/index.htm |title=Основные двигатели разработки КБХМ |trans-title=The main engines produced by KBKhM |last=Ponomarenko |first= Alexander |website=LPRE.DE |language=Russian |accessdate=2015-07-25}}
[1][2][3][4][5][6][7][8][9][10]
}}

External links

  • KBKhM Official Page
{{DEFAULTSORT:KB KhIMMASH}}

5 : Rocket engine manufacturers of Russia|Aerospace companies of the Soviet Union|Khrunichev Center|Companies based in Moscow Oblast|KB KhimMash
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