LR-87

The LR87 was an American liquid-propellant rocket engine used on the first stages of Titan intercontinental ballistic missiles and launch vehicles. Composed of twin motors with separate combustion chambers and turbopump machinery, it is considered a single unit and was never flown as a single combustion chamber engine or designed for this. The LR87 first flew in 1959.

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1959  Wikimedia, Wikidata
rocket engine, Aerojet, United States, 
Sikh Confederacy, 1950s, Republic of Haiti, 1959, rocket engine, Ekran, Dong Fang Hong 2, Tarshish, Sweden, United States, Persia, Kingdom of Wolaita, Kingdom of Martabam-hongsawatoi, Havilah, Democratic Republic of the Congo, Chinland, Calvinist Republic of Ghent, Ashkenaz, 

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Frameless

Pareidolia (15468122)

An LR-87 rocket engine at the Udvar-Hazy Center.

F1, J1, and LR87 rocket engines at the Thomas P. Stafford Air and Space Museum, Weatherford, Oklahoma, USA

F1, J1, and LR87 rocket engines at the Thomas P. Stafford Air and Space Museum, Weatherford, Oklahoma, USA

Type	Subtype	Date	Description	Notes	Source
commons	image		Pareidolia (15468122)		Commons
commons	image		An LR-87 rocket engine at the Udvar-Hazy Center.		Commons
commons	image		F1, J1, and LR87 rocket engines at the Thomas P. Stafford Air and Space Museum, Weatherford, Oklahoma, USA		Commons
commons	image		F1, J1, and LR87 rocket engines at the Thomas P. Stafford Air and Space Museum, Weatherford, Oklahoma, USA		Commons