Rocket Engine, Liquid Fuel, XLR-91, Second Stage, Titan I Missile
Single nozzle, bell-shaped combustion chamber, with longitudinally-arranged cooling tubes only visible in throat area of nozzle; nozzle, widely flared, with plumbing and pumps in back; some blue fittings.
Created by
NASM Conservation Unit
Date Created
11/30/2017
Source
Smithsonian National Air and Space Museum
Keywords
Engines; Military; Missiles; Rockets; Space
Rights and Restrictions
Not determined
For more information, visit the Smithsonians Terms of Use.