Federal State Unitary Enterprise Research and Development Institute of Mechanical Engineering
Native name | ФГУП «Научно-исследовательский институт машиностроения» |
|---|---|
Romanized name | FSUE “Research and Development Institute of Mechanical Engineering” |
Formerly called | OKB-2 |
| Federal State Unitary Enterprise | |
| Industry |
|
| Predecessor | NII-1 of Moscow |
| Founded | September 1, 1958 in Soviet Union |
| Founder | Mikhail G. Mironov |
| Headquarters | Builders Street 72 (Russian: ул. Строителей, 72), Nizhnyaya Salda, Sverdlovsk Oblast, Russia |
Key people |
Anatoly Long, Director of the Institute Adolf I. Razzhigaev Chief Engineer |
| Products |
|
| Parent | Russian Federal Space Agency |
| Website | Officila Website |
|
Footnotes / references [1][2][3][4][5] | |
FSUE “Research and Development Institute of Mechanical Engineering” (Russian: ФГУП «Научно-исследовательский институт машиностроения»), also known as NIIMash, is a Russian rocket engine design and manufacturing company specialized in small thrusters. It is located in the city of Nizhnyaya Salda, Sverdlovsk Oblast. It started as the B-175 factory of the NII-1 research institute, where Mikhail G. Mironov directed the development of liquid rocket engines research and testing.
Products
NIIMash has an extensive experience in design of testing stands, measurement and control as well as certifications. They also have a line of custom built air separation plants. They also have extensive experience in rotational forming of metals. The list of space rated products is extensive and is the following:
Current Propulsion Products
Engines in current production:[6][7]
- Propulsion
- Experimental Reactive Control System Module
- KDU 11D414NS
- Fobos-Grunt Sample Return Spacecraft Propulsion System
- Fobos-Grunt Spacecraft Thruster Modules
- Thrusters
- MD5 (AKA RDMT-5): Cold gas thruster.
- MD08 (AKA RDMT-8): Cold gas thrusters used on the Ekspress satellite series.
- MD08-02 (AKA RDMT-8-02): Cold gas thruster: Used on the Fobos-Grunt Sample Return Spacecraft.
- 11D428A-16 (AKA RDMT-135M): 135 N (30 lbf) N2O4/UDMH thruster. Used on the KTDU-80.
- 11D428AF-16: N2O4/UDMH thrusters used by the Fobos-Grunt space mission.
- 11D457: 53.9 N (12.1 lbf) N2O4/UDMH thrusters used by the Resurs-DK No.1.
- 11D457F: 54 N (12 lbf) N2O4/UDMH thrusters used by the Fobos-Grunt space mission.
- 11D458 (AKA RDMT-400): 392 N (88 lbf) N2O4/UDMH thrusters used by the Functional Cargo Block based modules and the Briz upper stage.[8]
- 11D458F (AKA RDMT-400F): 382 N (86 lbf) N2O4/UDMH thrusters used by the Fobos-Grunt space mission.
- 11D458M (AKA RDMT-400M): 392.4 N (88.2 lbf) N2O4/UDMH thrusters used by the Briz-M upper stage.
- 17D16 (AKA RDMT-200K): 200 N (45 lbf) GOX/Kerosene thruster. Used the Buran DO thrusters.
- 17D58E: N2O4/UDMH thrusters used by the Briz-M upper stage.
- 17D58EF: N2O4/UDMH thrusters used by the Fobos-Grunt space mission.
- Experimental thursters
- Propellant tanks & high pressure gas vessels
- Composite high pressure Xenon storage tank: Xenon storage unit for electric propulsion spacecrafts.
- Composite Vessel: General high pressure vessel used on the Fobos-Grunt mission.
- Monopropellant Tank with Stiff-Plastic Separation Device (Diaphragm): Monopropellant storage unit used on the Fobos-Grunt mission.
- Bipropellant Tank with Stiff-Plastic Separation Devices (Diaphragms): Bipropellant storage unit used on communications satellites.
- Solenoid Valves
- RT.200:
- 18RT.200:
- 16RT.200:
- 12RT.200:
- 6RT.200:
- Flow stabilizers
- CP1: 2.43 g (0.086 oz) per second of hypergolic propellant flow.
- CP2: 23.5 g (0.83 oz) per second of hypergolic propellant flow.
- CP3: 63 g (2.2 oz)/87 g (3.1 oz)/345 g (12.2 oz)/470 g (17 oz) per second of hypergolic propellant flow.
- CP4: 60 g (2.1 oz) per second of air/nitrogen/oxygen/hydrogen flow.
Former Propulsion Products
Engines that are no longer produced.[9]
- RDMT-0.4X: N2O4/UDMH rocket engine.
- RDMT-0.8: Nitrogen and helium cold gas thruster.
- RDMT-12: N2O4/UDMH rocket engine.
- RDMT-50: N2O4/UDMH rocket engine.
- RDMT-100: N2O4/UDMH rocket engine.
- RDMT-135 (AKA 11D428A): 135 N (30 lbf) N2O4/UDMH rocket engine. Used on the Soyuz 7K-S, KTDU-426 and initial KTDU-80.
- RDMT-200: 200 N (45 lbf) N2O4/UDMH thruster used on the Almaz space stations.[10]
- RDMT-400A: Experimental version of the RDMT-200 with Niobium combustion chamber.[11]
- RDMT-400X: Experimental version of the RDMT-200 with Carbon combustion chamber.[12]
See also
- NII-1 — The research institute where NIIMash started.
- Russian Federal Space Agency — The corporate parent of KB KhIMMASH.
References
- ↑ "История" [History] (in Russian). Keldysh Research Center. Retrieved 2015-07-30.
- ↑ "История" [History] (in Russian). NIIMash. Retrieved 2015-07-30.
- ↑ "Руководители" [Leaders] (in Russian). NIIMash. Retrieved 2015-07-30.
- ↑ "Находящиеся в ведении Роскосмоса" [Administered by the Russian Federal Space Agency] (in Russian). Roscosmos. Retrieved 2015-07-30.
- ↑ "Предприятие НИИМАШ, значение предприятия в разработке ракетных двигателей" [Enterprise NIIMash, the value of the enterprise in the development of rocket engines] Check
|url=value (help). салдинская-история.рф (in Russian). Retrieved 2015-07-30. - ↑ "Двигатели 1944-2000: Аавиационные, Ракетные, Морские, Промышленные" [Aviadvigatel 19442-2000: Aviation, rocketry, naval and industry] (PDF) (in Russian). pp. 140–144. Retrieved 2015-07-25.
- ↑ "Products". NIIMash. Retrieved 2015-07-30.
- ↑ "RDMT-400". Encyclopedia Astronautica. Retrieved 2015-07-30.
- ↑ "NII Mash". Encyclopedia Astronautica. Retrieved 2015-07-30.
- ↑ "RDMT-200". Encyclopedia Astronautica. Retrieved 2015-07-30.
- ↑ "RDMT-400A". Encyclopedia Astronautica. Retrieved 2015-07-30.
- ↑ "RDMT-400X". Encyclopedia Astronautica. Retrieved 2015-07-30.
External links
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