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The ascent propulsion system (APS) or lunar module ascent engine (LMAE) is a fixed-thrust hypergolic rocket engine developed by Bell Aerosystems for use in the Apollo Lunar Module ascent stage. It used Aerozine 50 fuel, and N 2 O 4 oxidizer. Rocketdyne provided the injector system, at the request of NASA, when Bell could not solve combustion ...
The ascent stage contained the crew cabin, instrument panels, overhead hatch/docking port, forward hatch, optical and electronic guidance systems, reaction control system, radar and communications antennas, ascent rocket engine and propellant to return to lunar orbit and rendezvous with the Apollo Command and Service Modules.
Busek is also preparing a 600 Watt iodine Hall thruster system for future Discovery Class missions. [17] Other publicized Busek technologies include RF ion engines [18] and a resistojet rocket. [19] Another focus is CubeSat propulsion, proposed for the 2018 Lunar IceCube mission. [20]
Descent stage may have hit the Moon, ascent stage in heliocentric orbit. Snoopy is the only flown LM ascent stage known to have survived intact (possibly asteroid 2018 AV2 [52]). LM-5 Eagle: Apollo 11: July 16, 1969 Descent stage on lunar surface in Sea of Tranquility, ascent stage left in lunar orbit (could be still orbiting the moon [53]) LM ...
Apollo 9 (March 3–13, 1969) was the third human spaceflight in NASA's Apollo program.Flown in low Earth orbit, it was the second crewed Apollo mission that the United States launched via a Saturn V rocket, and was the first flight of the full Apollo spacecraft: the command and service module (CSM) with the Lunar Module (LM).
The GPIM system flew aboard the small Ball Configurable Platform 100 (BCP-100) spacecraft bus. [ 6 ] [ 11 ] Aerojet Rocketdyne was responsible for the development of the propulsion system payload, and the technology demonstration mission employed an Aerojet-developed advanced monopropellant payload module as the sole means of on-board propulsion.
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