Rocketdyne Division, Rockwell International Corporation Search this
Chamber and nozzle coolant passages 347 stainless steel. Propellant tanks, lines, and valves, stainless steel. Pumps, aluminum alloys; turbine, Hastealloy. Injector, OHFC copper and 347 stainless steel.
Combustion chamber made of 292 stainless steel tubes. The assembly, except for inlet manifold, was furnaced brazed with gold brazing alloy. Injectors, furnaced brazed.
Dessicant holders on each side of rocket plumbing, with red plastic protective covers; bundle of wires in white plastic isulation adjacent to red desicant holders; another bundle of wires with white plastic insulation, in back of plumbing,
Overall: 5ft 3 1/2in. x 4ft 5 3/4in. x 8ft 4in. (161.3 x 136.5 x 254cm)
Country of Origin:
United States of America
Transferred from the National Aeronautics and Space Administration
Restrictions & Rights:
Do not reproduce without permission from the Smithsonian Institution, National Air and Space Museum