This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com

astronautix.com 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.
Back to Index
Last update 12 March 2001.
Definitions of Technical Terms.
Contact Mark Wade with any corrections or comments.
Conditions for use of drawings, pictures, or other materials from this site..
© Mark Wade, 2001 .