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31 Δεκ 2014 · One of the Manuals of the Rocketdyne F-1 Engine that powered the First Stage of the Saturn V, the S-IB.
13 Μαΐ 2021 · Silverstein insisted that the F-1 should produce 1.5M lbT, same as the total thrust of the Saturn IB. He also insisted this should be accomplished by scaling up existing ballistic missile technology to produce a conservative design reliable enough for human flight.
Become familiar with the Saturn V Stage I (S-IC) major structural components: ¾Forward Skirt ¾Oxidizer Tank ¾Intertank ¾Fuel Tank ¾Thrust Structure Gain a general understanding of the Stage I subsystems: ¾Fuel ¾Oxidizer ¾Instrumentation ¾Flight Control ¾Environmental Control ¾Electrical ¾Control Pressure ¾Ordinance
13 Μαΐ 2021 · The F-1 had two identical fuel valves that directed fuel to the thrust chamber. The valves were hydraulically operated, spring-loaded-closed, pressure-balanced, fail-to-the-run-position, poppet-type valves having quick response and low delta-P operating characteristics.
Capture knowledge about the F-1, Understand the mechanical layout of the engine and the hardware designs, Test components to understand the F-1 engine performance, Help the team to design a new, improved, large LOX/RP engine.
25 Δεκ 2020 · F-1 Rocket Engine Technical Manual Supplement (R-3896-1A)_page_numbers.json download 69.5K F-1 rocket engine operating instruction technical_page_numbers.json download
This diagram is from the Saturn V Flight Manual SA-509. It reflects the post-SA-501 (the Apollo 4 mission), F-1 configuration with rigid propellant high-pressure ducts. This diagram is also rotated approximately 90° compared to the diagram above.
