AJ10 - Wikipedia
The AJ10 is a hypergolic rocket engine manufactured by Aerojet Rocketdyne (previously Aerojet). It has been used to propel the upper stages of several launch vehicles, including the Delta II and Titan III.
AJ10 - Encyclopedia Astronautica
AJ10-104 Aerojet Nitric acid/UDMH rocket engine. Stainless steel version of the basic Able engine, uprated to increase thrust 34.7 kN to 37.0 kN and to increase the duration 2-1/2 times First flight 1960.
AJ10-118K - Encyclopedia Astronautica
Aerojet N2O4/Aerozine-50 rocket engine. Pressure-fed engine, optimized for altitude operation, used in Delta K stage from 1989. Not regeneratively cooled; used a rubber modified silica phenolic ablative at the combustion flame front.
Orion主引擎:AJ10 - 哔哩哔哩
航天飞机退役以后AJ10-190装在了Orion飞船上，所以还可以被称为OME(Orion Main Engine)，将推动未来的Artemis计划。 NASA也已经与Aerojet Rocketdyne签订了6亿美元的合同用于发展，设计并制造Artemis 7-14共8次任务的OME(非常离谱的价格，即使考虑上以后生成的价格会更低)。
Aerojet Rocketdyne has bipropellant in-space rocket engines ranging in thrust level from 2.5-lbf thrust to 6,000-lbf thrust. Bipropellant engines produce thrust when two propellant valves open and liquid fuel (typically monomethyl hydrazine, or hydrazine) and liquid oxidizer (nitrogen tetroxide) hypergolically ignite in the chamber.
Aerojet - AJ10-137 Apollo Service Module Engine - NASA …
Nov 1, 2009 · The general configuration of the SPS engine was 20,000 pounds of thrust, with a chamber pressure of 100 psi and specific impulse (Isp) of 314.5. The very large nozzle had an area ratio of 62.5:1 (exit area to throat area). The propellants were nitrogen tetroxide (also known as N2O4 and nitrous oxide) and A-50. A-50 was a hydrazine family fuel.
Aerojet AJ10-118K - Purdue University
Engine statistics; Specification; Applications: Delta II,III,IV EELV second stage: Propellants: Aerozine 50/N2O4: Thrust in Vacuum: 9753 lb: Isp in vacuum(s) 320.5 s
AJ10-118 - Encyclopedia Astronautica
Aerojet Nitric acid/UDMH rocket engine. Out of Production. Engine originally developed for the Vanguard launch vehicle, and then for use on the Able and Delta upper stages and as the Apollo Service module engine.
AJ10 - WikiMili, The Best Wikipedia Reader
Jul 15, 2024 · The AJ10 is a hypergolic rocket engine manufactured by Aerojet Rocketdyne (previously Aerojet). It has been used to propel the upper stages of several launch vehicles, including the Delta II and Titan III.
Remembering the Giants: Apollo Rocket Propulsion Development
Nov 1, 2009 · Remembering the Giants: Apollo Rocket Propulsion Development Topics discussed include: Rocketdyne - F-1 Saturn V First Stage Engine; Rocketdyne - J-2 Saturn V 2nd & 3rd Stage Engine; Rocketdyne - SE-7 & SE-8 Engines; Aerojet - AJ10-137 Apollo Service Module Engine; Aerojet - Attitude Control Engines; TRW - Lunar Descent Engine; and Rocketdyne ...
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