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J-2 Rocket Engine
Conceptually similar
J-2 Thrust Chamber Production Line
J-2 Major Component Breakdown Illustration
F-1 Rocket Engine Test Fired at Edwards AFB
Saturn S-IVB Stage Moving from Vertical Test Stand to Building 45
Saturn S-IVB Stage Moving from Vertical Test Stand to Building 45
Technicians Assemble Saturn V first Stage
Saturn V first Stage Assembly at NASA Michoud
Saturn V Assembly
Saturn S-IVB Booser Rocket in Tow
Saturn S-IVB 2001 Rollout S IV B
Saturn V Rocket
Inspecting Saturn V first Stage
Saturn S-IVB Stage Move
Transporting Saturn S-IVB Third Stage Via Barge
Transporting Saturn S-IVB Third Stage
Saturn V Fuel Tank Dome
Boeing Huntington Beach Site Building 45 Saturn S-IVB DWD Sr., Jr. LBJ
S-IVB Saturn-IB Second Stage at the Unisphere, Queens, NY
Transporting Saturn S-IVB Third Stage
S-IVB Saturn-IB Second Stage in Hangar
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J-2 Thrust Chamber Production Line
January 18, 1966 Press Release: This is the production line for thrust chambers of hydrogen-fueled J-2 rocket engine that will launch first orbital flights of three astronauts in Apollo spacecraft, later will fly the spacecraft on its journey to the moon. J-2 develops 200,000 pounds of thrust. It is being produced at Canoga, Calif. plant of Rocketdyne, a division of North American Aviation, Inc., for NASA's Marshall Space flight Center. A single J-2 will power the S-IVB stage being built by Douglas Aircraft Company for the second stage of the Saturn IB vehicle and the third stage of Saturn V. Five J-2's will be used to produce 1,000,000 pounds of thrust in the S-II stage being built by North American's Space and Information systems Division for the second stage of the Saturn V moon-launch vehicle.
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Unique identifier
BI233544
Boeing ID
mfg-621-2
Type
Image
Size
2273px × 2833px 6MB
License type
RM
Keywords
1960s
abundance
adults
day
factories
factory workers
ground shots
interiors
J-2
maintenance
male
perspective lines
photos
repetition
rocket engine nozzles
rocket engines
viewed from above
vintage / retro
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