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United States engines

11 articles

Aerojet Rocketdyne

Aerojet Rocketdyne was an American rocket propulsion manufacturer formed in 2013 by the merger of Aerojet and Pratt & Whitney Rocketdyne, acquired by L3Harris in 2023.

Demonstration Rocket for Agile Cislunar Operations

The Demonstration Rocket for Agile Cislunar Operations (DRACO) was a United States program led by DARPA with NASA to demonstrate a nuclear thermal rocket engine in orbit, planned for 2027.

Gerard W. Elverum

Gerard W. "Jerry" Elverum was an American rocket-propulsion engineer who directed TRW's Apollo Lunar Module descent engine, the throttleable engine that landed astronauts on the Moon.

Jack Parsons

Jack Parsons, born Marvel Whiteside Parsons (1914–1952), was an American rocket propulsion engineer who co-founded Aerojet and JPL and invented the first castable composite solid rocket propellant.

NERVA

NERVA (Nuclear Engine for Rocket Vehicle Application) was a joint NASA and Atomic Energy Commission program, from 1961 to 1973, to develop a nuclear thermal rocket engine.

RL10

The RL10 is an American liquid-hydrogen and liquid-oxygen upper-stage rocket engine developed by Pratt & Whitney, first flown in 1963 and still in production today.

Robert H. Goddard

Robert H. Goddard, also known as Robert Hutchings Goddard, was an American physicist who flew the world's first liquid-propellant rocket in 1926 and is called the father of modern rocketry.

Robert L. Sackheim

Robert L. Sackheim was an American space propulsion engineer who spent 35 years at TRW before serving as chief engineer for space propulsion at NASA's Marshall Space Flight Center.

Rocketdyne

Rocketdyne is an American rocket engine manufacturer founded in 1955, known for the engines that powered the Redstone missile, Saturn rockets, the Space Shuttle, and NASA's Space Launch System.

Rocketdyne F-1

The Rocketdyne F-1 was a kerosene and liquid oxygen rocket engine, developed by Rocketdyne to power the first stage of the Saturn V Moon rocket.

Rocketdyne J-2

The Rocketdyne J-2, also known as the J-2 engine, was an American rocket engine burning liquid oxygen and liquid hydrogen that powered the upper stages of the Saturn IB and Saturn V during Apollo.