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searching for Staged combustion cycle 11 found (154 total)

S5.98M (268 words) [view diff] no match in snippet view article find links to article

The S5.98M, also known as the 14D30, is a Russian rocket engine, currently powering the Briz upper stages. It was designed by KB KhIMMASH, the famous Isaev

KVD-1 (578 words) [view diff] no match in snippet view article find links to article

KVD-1 was an upper stage LOX/LH2 cryogenic engine developed by the Isayev Design Bureau (now KB KhIMMASH) of Russia in the early 1960s. It is a modified

TR-107 (248 words) [view diff] no match in snippet view article find links to article

The TR-107 was a developmental rocket engine designed in 2002 by Northrop Grumman for the NASA and DoD-funded Space Launch Initiative (SLI). Operating

BE-7 (452 words) [view diff] no match in snippet view article find links to article

The Blue Engine 7 is a liquid hydrogen/oxygen dual expander cycle engine for use with the Blue Moon family of lunar landers. The company utilizes additive

A.M. Isayev Chemical Engineering Design Bureau (1,334 words) [view diff] exact match in snippet view article find links to article

Project for the ICBM R-9B. 4D10: A UDMH/N2O4 burning engine in the staged combustion cycle. Development years: 1962-1968 . For use as main engine of the first

SpaceLiner (1,708 words) [view diff] exact match in snippet view article find links to article

reusable liquid rocket engine, which operates in the full-flow staged combustion cycle mode. Having a common engine design for both SpaceLiner stages

Venera 1 (878 words) [view diff] no match in snippet view article find links to article

directed towards Venus. The 11D33 engine was the world's first staged-combustion-cycle rocket engine, and also the first use of an ullage engine to allow

RD-0110 (1,183 words) [view diff] case mismatch in snippet view article find links to article

Retrieved 27 November 2024. "Turbopumps for Gas Generator and Staged Combustion Cycle Rocket Engines" (PDF). AIAA. July 2005. Retrieved 29 May 2015.

Impulse Space (1,230 words) [view diff] exact match in snippet view article find links to article

Mojave Air and Space Port facilities. Deneb is a 15,000 lbf (67 kN) staged combustion cycle engine that uses liquid oxygen (LOX) and methane as propellants

Space Shuttle (12,087 words) [view diff] no match in snippet view article find links to article

would be removed and replaced in between flights. The RS-25 is a staged-combustion cycle cryogenic engine that used liquid oxygen and hydrogen and had a

SpaceX Super Heavy (12,394 words) [view diff] exact match in snippet view article find links to article

directly below the launch pad. The Raptor engine uses a full-flow staged combustion cycle, which has both oxygen and methane-rich turbopumps. Before 2014