This page no longer updated from 31 October 2001. Latest version can be found at LR-87-3

LR-87-3 Engine
LR-87-3 Engine -

Credit: Bob Fortune. 25,362 bytes. 266 x 343 pixels.

Manufacturer Name: AJ23-130. Government Designation: LR-87-3. Designer: Aerojet. Used on stages: Titan 1-1. Used on launch vehicles: Juno V-A, Juno V-B, Saturn A-1, Super-Jupiter, Titan 1. Propellants: Lox/Kerosene Thrust(vac): 74,842 kgf. Thrust(vac): 733.90 kN. Isp: 290 sec. Isp (sea level): 256 sec. Burn time: 138 sec. Mass Engine: 839 kg. Diameter: 1.5 m. Length: 3.1 m. Chambers: 1. Chamber Pressure: 40.00 bar. Area Ratio: 8.00. Oxidizer to Fuel Ratio: 1.91. Thrust to Weight Ratio: 89.20. Country: USA. Status: Out of Production. Comments: Titan 1 Surplus Flight Engines were available for various uses in the 1960's.
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Last update 12 March 2001.
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