Proton-PM

Proton-PM is a Russian aerospace and heavy-machinery manufacturing enterprise based in Perm, on the Kama River in Perm Krai. Its industrial identity was established in 1958, when it began as a specialized branch of Plant No. 19 named after I. V. Stalin, created to manufacture the RD-214 liquid-fuel rocket engine. The plant formed part of the Soviet Union's wider effort to build a domestic production base for ballistic missiles, space-launch vehicles, and associated propulsion systems. In 1964, the operation became a separate entity known as Second Production. Over subsequent decades, its role expanded beyond the manufacture of individual rocket engines. Proton-PM became associated with serial production of propulsion systems designed by specialist aerospace organizations, particularly NPO Energomash, and with engines used in major Russian launch-vehicle programs. Its production history includes the RD-214, RD-253, and RD-275 families. The RD-253 and its improved RD-275 derivative were used with the Proton launch-vehicle program, while the RD-191, a kerosene-and-liquid-oxygen engine, is associated with the Angara family of launch vehicles. The company also diversified into stationary gas-turbine equipment and power-generation systems. Its industrial portfolio includes the Ural series of gas-turbine power stations, as well as larger GTES and GTU systems intended for combined electricity and heat production. This combination of aerospace manufacturing and energy equipment reflects Proton-PM's position as a specialized production enterprise rather than a consumer-facing brand. Its products are sold or supplied primarily through institutional, governmental, aerospace, defense, and industrial relationships. Proton-PM operates within the Russian aerospace and engine-manufacturing system and is identified in reference material as a corporate parent or affiliated enterprise of Aviadvigatel. The plant's work is closely connected with Russian launch-vehicle manufacturers and engine designers, including the production of engines for programs associated with the Proton and Angara families. Its public profile is therefore defined less by independent brand marketing than by its role in national aerospace and heavy-industry supply chains. The available reference material does not establish a complete ownership history, current executive roster, financial profile, or a definitive corporate website. It does, however, identify the Perm plant as an active producer of rocket engines and gas-turbine power equipment. Proton-PM's principal significance lies in its long-running manufacturing capability: it links Soviet-era missile and space propulsion production with later Russian launch systems and industrial power technologies.

Proton-PM traces its origins to 1958, when a specialized branch of Plant No. 19 in Perm was established to manufacture the RD-214 liquid-fuel rocket engine. The facility was created during the Soviet expansion of missile and space technology production. Its location in Perm provided access to an established heavy-industrial base and river-linked manufacturing infrastructure. In 1964, the operation was separated from its original organizational structure and became known as Second Production. The plant subsequently developed into a dedicated producer of rocket engines and heavy industrial equipment. Its historical output included the RD-214, which powered the R-12 and Kosmos-2 systems, and the RD-253, associated with the first stage of the Proton launch vehicle. An improved version, the RD-275, followed in the same general propulsion lineage. The enterprise's role was primarily manufacturing rather than independent engine design. Specialist design organizations, including NPO Energomash, developed important propulsion systems, while production was assigned to manufacturing plants such as Proton-PM. This division of labor made the Perm operation part of a broader aerospace production network supporting Soviet and later Russian launch programs. In the post-Soviet period, Proton-PM continued to participate in Russian aerospace manufacturing and expanded its industrial range. The RD-191 became one of the key newer engines associated with the plant. It uses kerosene and liquid oxygen and powers the Angara family of launch vehicles. The RD-276, described as the latest version of the RD-275, represents the continued development of the plant's liquid-fuel propulsion production capabilities. Alongside aerospace work, Proton-PM developed and manufactured gas-turbine power-generation equipment. Its portfolio includes Ural-2500, Ural-4000, Ural-6000, GTES-16PA, GTES-25P, and GTU-32P systems. These products are intended for industrial electricity and heat generation and broaden the enterprise's customer base beyond launch-vehicle programs. The plant is located in Perm on the bank of the Kama River and is identified in the reference material as being connected with Aviadvigatel. Its continuing importance comes from the combination of long-term rocket-engine manufacturing experience, participation in major Russian launch systems, and production of stationary gas-turbine equipment. Publicly available material supplied for this dossier does not provide a reliable current executive list, detailed ownership structure, financial results, or campaign history.

• 1964

  The operation becomes a separate entity

  [1]Proton-PMen.wikipedia.org

  The plant is separated organizationally and becomes known as Second Production.

• 1958

  Specialized rocket-engine production begins

  [1]Proton-PMen.wikipedia.org

  A specialized branch of Plant No. 19 in Perm begins manufacturing the RD-214 liquid-fuel rocket engine.

• Production expands to Proton-family propulsion

  [1]Proton-PMen.wikipedia.org

  The plant manufactures RD-253 and RD-275 rocket engines associated with the Proton launch-vehicle program.

• Diversification into gas-turbine power systems

  [1]Proton-PMen.wikipedia.org

  Proton-PM develops a range of stationary gas-turbine power stations and industrial turbine units.

• RD-191 production for the Angara family

  [1]Proton-PMen.wikipedia.org

  The plant is identified as a producer of RD-191 liquid-oxygen and kerosene engines used by the Angara launch-vehicle family.

A specialized Russian aerospace and industrial manufacturing enterprise serving launch-vehicle propulsion programs and stationary gas-turbine power generation.

• Liquid-fuel rocket engine

  RD-276

  The RD-276 is identified as the latest version of the RD-275 engine family. It belongs to Proton-PM's liquid-fuel rocket-propulsion portfolio and represents the continuation of the plant's production work on engines derived from the RD-253 line.

• Liquid-fuel rocket engine

  RD-191

  The RD-191 is a liquid-fuel rocket engine that burns kerosene and liquid oxygen. Proton-PM is identified as a production site for the engine, which powers the Angara family of launch vehicles.

• Liquid-fuel rocket engine

  RD-214

  The RD-214 was an early rocket engine manufactured at the Perm facility. It used a hypergolic oxidizer-fuel combination and powered the R-12 and Kosmos-2 systems. It is no longer listed as being in current production.

• Liquid-fuel rocket engine

  RD-253

  The RD-253 is a liquid-fuel engine associated with the first stage of the Proton launch vehicle. It used unsymmetrical dimethylhydrazine and nitrogen tetroxide and formed a major part of the plant's historical aerospace manufacturing role.

• Liquid-fuel rocket engine

  RD-275

  The RD-275 is an improved development of the RD-253 and was produced for the Proton launch-vehicle propulsion family. It has subsequently been superseded in the listed product range by the RD-276.

• Industrial power-generation equipment

  Ural gas-turbine power stations

  The Ural-2500, Ural-4000, and Ural-6000 systems are gas-turbine power stations designed to produce electricity and useful heat. The listed configurations range from smaller industrial installations to systems with higher electrical and thermal output.

• Industrial gas-turbine equipment

  GTES and GTU systems

  Proton-PM's industrial turbine range includes GTES-16PA, GTES-25P, and GTU-32P systems. These units extend the company's activities from aerospace propulsion into stationary power generation for industrial applications.

1. 1Proton-PMen.wikipedia.org