The S1.5400 (

GRAU The Main Missile and Artillery Directorate of the Ministry of Defense of the Russian Federation (), commonly referred to by its transliterated acronym GRAU (), is a department of the Russian Ministry of Defense. It is subordinate to the Chief of ...

Index 11D33) was a

Soviet The Union of Soviet Socialist Republics. (USSR), commonly known as the Soviet Union, was a List of former transcontinental countries#Since 1700, transcontinental country that spanned much of Eurasia from 1922 until Dissolution of the Soviet ...

single-nozzle liquid-propellant rocket engine burning

liquid oxygen Liquid oxygen, sometimes abbreviated as LOX or LOXygen, is a clear cyan liquid form of dioxygen . It was used as the oxidizer in the first liquid-fueled rocket invented in 1926 by Robert H. Goddard, an application which is ongoing. Physical ...

and

kerosene Kerosene, or paraffin, is a combustibility, combustible hydrocarbon liquid which is derived from petroleum. It is widely used as a fuel in Aviation fuel, aviation as well as households. Its name derives from the Greek (''kērós'') meaning " ...

in an oxidizer-rich

staged combustion cycle The staged combustion cycle (sometimes known as topping cycle, preburner cycle, or closed cycle) is a power cycle of a bipropellant rocket engine. In the staged combustion cycle, propellant flows through multiple combustion chambers, and is th ...

, the first rocket engine to use this cycle in the world. It was designed by V. M. Melnikov, an alumnus of Isaev, within Korolev's

Bureau Bureau ( ) may refer to: Agencies and organizations *Government agency *Public administration * News bureau, an office for gathering or distributing news, generally for a given geographical location * Bureau (European Parliament), the administra ...

, for the Molniya fourth stage, the Block-L. It was the first Soviet engine designed for start and restart in vacuum, and had the highest ''I''_sp at the time of its deployment. Its development took from 1958 to 1960. The first production run was started in May 1960, and it passed all the firing tests. Its first flight failed before the Block-L was activated. The first success was in a Venera flight during 1961. Between 1961 and 1964, it went through an improvement program that culminated in the S1.5400A1 version (GRAU Index 11D33M). It improved thrust from to and ''I''_sp from 338.5 s to 340 s while keeping the same mass. The engine used titanium alloy in its main combustion chamber to tolerate temperatures of up to . The turbopump initial spin-up is pyrotechnic. The engine is attached to a Cardan suspension, which enables it to gimbal up to 3° in two axes.

References

External links

RSC Energia Corporation Home Page
{{Rocket engines Rocket engines of Russia Rocket engines of the Soviet Union Rocket engines using kerosene propellant Rocket engines using the staged combustion cycle Energia rocket engines

See also

References

External links