Proton-PM

Short description: Subsidiary of Roscosmos

Proton-PM

Native name

| Протон-ПМ

Romanized name

| Proton-PM
Formerly| I.V. Stalin Plant No. 19
Type| Open joint-stock company
Industry|

* Liquid rocket engine manufacturing
* Aircraft engine manufacturing
* Turbopumps manufacturing
* Gas turbine power station production
* Metallurgical production

Founded| Perm, Russia (March 12, 1958 (1958-03-12))
Headquarters| 93, avenue Komsomolsky, Perm, 614990,

Perm

Russia

Key people

| Igor Arbuzov[1]
Products|

* RD-214
* RD-253 RD-275 RD-276 RD-191

Parent| Roscosmos[2]
Website| Official Website

OJSC Proton-PM (Russian: АО «Протон-ПМ») is a Russian engine and heavy machinery manufacturing plant. It is located in the city of Perm, in the Perm Krai, on the bank of the Kama River.[3] It started in 1958 as the specialized branch of Plant No. 19 named after I. V. Stalin for the manufacturing of the RD-214 rocket engine. In 1964 it was given made a separate entity then known as Second Production. In the later years, it has branched intro producing gas turbine power plants.[4][5][6]

## Contents

* 1 Products
* 1.1 Current engines
* 1.2 Former engines
* 1.3 Gas Turbines
* 2 See also
* 3 References
* 4 External links

## Products

### Current engines

Engines in current production at the plant:

* RD-276 the latest version of the RD-275.[7]
* RD-191 a liquid rocket engine, burning kerosene and LOX that powers the Angara (rocket) family of launch vehicles.[7]

### Former engines

Engines that are no longer produced at the plant.

* RD-214 a liquid rocket engine, burning AK-27I (a mixture of 73% Nitric acid \+ 27% N2O4 \+ iodine passivant and TM-185 (a kerosene and gasoline mix), that powered the R-12 and Kosmos-2.[5]
* RD-253 a liquid rocket engine, burning UDMH/N2O4 that powers the Proton first stage.[5]
* RD-275 an improved RD-253.[5]

### Gas Turbines

* Ural-2500 gas-turbine power station (2.55 MW/ 5.82 Gcal per hour),
* Ural-4000 gas-turbine power station (4.13 MW/ 8.3 Gcal per hour),
* Ural-6000 gas-turbine power station (6.14 MW/ 11.44 Gcal per hour),
* GTES-16PA gas-turbine power station (16.3 MW/ 19.48 Gcal per hour),
* GTES-25P gas-turbine power station (23.0 MW/ 26.1 Gcal per hour).
* GTU-32P (up to 34 40 MW)

## See also

* NPO Energomash -- The rocket engine designer that delegates some serial production to this plant.
* Khrunichev State Research and Production Space Center -- The Proton-M and Angara (rocket) manufacturer that delegate engine production to this plant.
* Aviadvigatel -- The corporate parent.

## References

1. ↑ "Management". OJSC Proton-PM. http://protonpm.com/corporate/about/management/. Retrieved 2015-07-21.
2. ↑ "Списки аффилированных лиц ПАО Протон-ПМ". http://www.disclosure.ru/issuer/5904006044/. Retrieved 7 May 2017.
3. ↑ "Contact". OJSC Proton-PM. http://protonpm.com/corporate/contacts/. Retrieved 2015-07-21.
4. ↑ "Current Projects". OJSC Proton-PM. http://protonpm.com/creator/projects/current/. Retrieved 2015-07-21.
5. ↑ 5.0 5.1 5.2 5.3 "History". OJSC Proton-PM. http://protonpm.com/corporate/about/history/. Retrieved 2015-07-21.
6. ↑ "Perm Motors Company". Global Security. http://www.globalsecurity.org/military/world/russia/pmz.htm. Retrieved 2015-07-21.
7. ↑ 7.0 7.1 "Production and industrial services". OJSC Proton-PM. http://protonpm.com/creator/production/produce_and_services/. Retrieved 2015-07-21.

## External links

* Proton-PM website

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