CC0 · no rights reserved
Rocket Engine, Liquid Fuel, Apollo Lunar Module Descent Engine
From the collection of National Air and Space Museum. Free to download, adapt and use — no permission needed.
About this work
This is a Descent Engine designed by Space Technology Laboratories as used on the Project Apollo Lunar Excursion Module (LM) to land on the Moon. The engine could be throttled between 1,000 and 10,000 pounds of thrust and was also the first gimballed and throttable rocket engine used on a spacecraft.
National Air and Space Museum’s own descriptionSubjects
Credit lineRocket Engine, Liquid Fuel, Apollo Lunar Module Descent Engine. Space Technology Laboratories (STL). National Air and Space Museum, Transferred from the National Aeronautics and Space Administration. CC0.
Similar works
Continental XR-1740-2, Sleeve Valve, Radial 14 Engine
Rocket Engine, Liquid Fuel, Apollo Lunar Module Ascent Engine
Rocket Engine, Liquid Fuel, Navajo Missile
Left R-2800-43 Engine, Martin B-26B-25-MA "Flak-Bait"
Nakajima Ha 105 Toku, Radial 14 Engine
Commerical Crew Program (CCP) Astronauts visit Aerojet Rocketdyn