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J-2 Rocket Engine 
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J-2 Thrust Chamber Production Line
J-2 Thrust Chamber Production Line 
J-2 Thrust Chamber Production Line
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Saturn S-IVB Stage Moving from Vertical Test Stand to Building 45
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Transporting S-IVB Saturn-IB Second Stage Via Barge
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S-IVB Saturn-IB Second Stage
S-IVB Saturn-IB Second Stage 
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J-2 Major Component Breakdown Illustration

Rocketdyne J-2 rocket engines powered numerous Saturn rocket stages for the Apollo space flight program. A J-2 developed 200,000 pounds of thrust.
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Unique identifier BI233540 
Boeing ID 507-321-703 
Type Image 
Size 2642px × 1815px   4MB 
License type RM 
Keywords
1960s
close-ups
complexity
detail views
illustrations
J-2
photo illustrations
rocket engine nozzles
rocket engines
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