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Rocketdyne LR-101

The Rocketdyne LR-101 is a fixed thrust, single start vernier thruster developed by Rocketdyne in the mid-to-late fifties and used in the Atlas, Thor and Delta launch vehicles until 1990.

Variants
Due to several modifications the LR-101 underwent over the years, there are many different variants of this engine (LR101-NA-3, LR101-NA-7, LR101-NA-9, LR101-NA-11, == Role in experimental rocketry ==
Role in experimental rocketry
The LR-101 is one of the most common vernier thrusters utilized in American rocketry and has become a sought-after object for item collectors and builders of amateur rockets. Rocket engineer Robert C. Truax, who had led the initial design studies for the PGM-17 Thor missile had planned on propelling his 'X-3 Volksrocket' with four Rocketdyne LR-101 engines, but despite many test firings the rocket never left the ground. On the 'Galactic Aztec', the engine used RP-2 (Kerosene) as a propellant instead of RP-1, which was utilized in the SM-65 Atlas and PGM-17 Thor ballistic missiles as well as the later commercial Delta rockets. ==See also==
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