AEROJET ROCKETDYNE – Titan Liquid Rocket Engine


Description:

Throughout the years, Titan played a major role as a U.S. launch vehicle and was uprated several times resulting in the Titan IV. Vacuum thrusts for storable Titan Stage 1 engine systems range from 474,000.bf for Titan II to 548,000 lbf for Titan IV. Vacuum thrusts for Stage 2 engine systems range from 100,000 lbf for Titan II to 105,000 lbf for Titan IV.

Specifications

Official Page Product
February 22, 2014 |
Epiq Space

Epiq Space

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