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A test engine is on display at the Powerhouse Museum in Sydney, Australia. It was the 25th out of 114 research and development engines built by Rocketdyne and it was fired 35 times. The engine is on loan to the museum from the Smithsonian's National Air and Space Museum. It is the only F-1 on display outside the United States. [21]
Engine Origin Designer Vehicle Status Use Propellant Power cycle Specific impulse (s) [a] Thrust (N) [a] Chamber pressure (bar) Mass (kg) Thrust: weight ratio [b] Oxidiser: fuel ratio AJ-10-190 USA: Aerojet: Space Shuttle, Orion, Apollo CSM: Active Upper N 2 O 4 /MMH: Pressure-fed: 316 [1] 26,689 [1] 8.62 [1] 118 [1] 23.08: Archimedes New ...
English: Video of Apollo 11 engines during launch on 16th July 1969 from the Mobile Launcher. This footage takes place within approximately 30 seconds, camera E-8 captured on 16 mm film at 500 frames per second.
Pogo oscillation is a self-excited vibration in liquid-propellant rocket engines caused by combustion instability. [1] The unstable combustion results in variations of engine thrust, causing variations of acceleration on the vehicle's flexible structure, which in turn cause variations in propellant pressure and flow rate, closing the self-excitation cycle.
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This video frame shows S-II-S/D after it failed in final structural tests. These excerpts from Saturn V Quarterly Film Reports show SA-500D coming together for testing. In January 1966, the all-systems test S-II-T was re-designated S-II-T/D, so that it might be used for dynamic testing as well as engine firing.
AS-201 (Also known as SA-201, Apollo 1-A, or Apollo 1 prior to the 1967 pad fire), flown February 26, 1966, was the first uncrewed test flight of an entire production Block I Apollo command and service module and the Saturn IB launch vehicle. The spacecraft consisted of the second Block I command module and the first Block I service module.
BP-1210 Apollo 8 S-IVB rocket stage shortly after separation. The LM test article, a circular boilerplate model of the LM is visible with four triangular legs connecting it to the stage. BP-1210 was used in landing and recovery training and to test flotation devices. It is on display outside the Stafford Air & Space Museum. [20]