Development of LOX/RP-1 engines for Saturn/Apollo launch vehicles.
The development of liquid rocket engines follow similar patterns regardless of engine size. During the development of the H-1 and F-1 engines, may problems were encountered. Mehtods of solving the combustion instability problem are discussed.; AIAA 4th Propulsion Joint Specialist Conference, Cleve...
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| Format: | Electronic |
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University of Alabama in Huntsville Archives
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| Online Access: | http://libarchstor2.uah.edu/digitalcollections/items/show/11057 |