 | |
| Country of origin | Soviet Union |
|---|---|
| First flight | 1967 |
| Designer | OKB-1, V. M. Melnikov |
| Manufacturer | Voronezh Mechanical Plant |
| Application | Upper Stage |
| Associated LV | N1, Proton-K, Proton-M, Zenit |
| Predecessor | S1.5400 |
| Status | In Production |
| Liquid-fuel engine | |
| Propellant | LOX / RG-1 |
| Cycle | Oxidizer-rich staged combustion |
| Configuration | |
| Chamber | 1 |
| Performance | |
| Thrust, vacuum | 79.46 kilonewtons (17,860 lbf) |
| Specific impulse, vacuum | 353 s |
| Burn time | up to 600 s |
| Dimensions | |
| Dry mass | 300 kilograms (660 lb) |
| Used in | |
| Block D | |
| References | |
| References | |
The RD-58 (Russian: Ракетный Двигатель-58, romanized: Raketnyy Dvigatel-58, lit. 'Rocket Engine 58', GRAU index: 11D58) is a rocket engine, developed in the 1960s by OKB-1, now RKK Energia. The project was managed by Mikhail Melnikov, and it was based on the previous S1.5400 engine, which was the first staged combustion engine in the world. The engine was initially created to power the Blok D stage of the Soviet Union's abortive N1 rocket. Derivatives of this stage are now used as upper stages on some Proton and Zenit rockets. An alternative version of the RD-58 chamber, featuring a shorter nozzle, was used as the N1's roll-control engine.
The RD-58 uses liquid oxygen as the oxidizer and RG-1 as fuel in an oxidizer-rich staged combustion cycle. It features a single gimbaled chamber, radial centrifugal pumps with auxiliary booster pumps, and an oxygen-rich preburner. Recent modifications include a lightweight carbon-composite nozzle extender developed by NPO Iskra.
The Buran spacecraft used two of an evolution of the RD-58M, called 17D12, as its main orbital correction engines. Instead of RG-1, it burned Syntin, and could be ignited 15 times. It is assumed that it was the base for the RD-58S, which had practically the same specifications and powered the Blok DM-2M. But the manufacturer states that the engine is compatible with both propellants.
The current version of the engine is the RD-58M (manufacturer designation 11D58M), which has slightly reduced thrust, but increased isp. An even newer version is under development and is known as the RD-58MF (manufacturer designation 11D58MF). It will reduce thrust to 49.03 kilonewtons (11,020 lbf) to keep the same length but increase expansion ratio to 500:1. This will enable it to gain 20s of isp (to an expected 372s). It will eventually fly on the Blok DM-03. This new version of the engine will be built in the Krasnoyarsk Machine-Building Plant. During a November 2014 interview, Vladimir Kolmykov, the Deputy General Director of the Chemical Division of Krasnoyarsk Machine-Building Plant, stated that the production of Block-DM was suspended during that year, but work on the stage and development of the RD-58MF will resume during 2015.
