F-1 Engines on the Saturn S-IC Stage
Each of the five liquid kerosene (RP-1) and liquid oxygen (LOX) fueled F-1 engines were capable of delivering 1.5 million pounds of takeoff thrust, for a combined thrust of 7.5 million pounds during the boost phase. (Jason Perlow)
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BTW - those r... (Read the rest) - Posted by: jackgrat Posted on: 07/16/09 You are currently: a Guest | Log in | Terms of Use
Saturn Rocket Engines
lpkelley63 | 07/16/09
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got that right
pgit | 07/16/09
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RE: Werner von Braun and the S-IC Stage (Rocketdyne F-1 and J-2 Rocket Engine Development and Testing)
lpkelley63 | 07/16/09
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I agree
Baer | 07/16/09
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RE: Werner von Braun and the S-IC Stage (Rocketdyne F-1 and J-2 Rocket Engi
GpaKen | 07/16/09
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Saturn V Shocked the World
jackgrat | 07/16/09
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