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Saturn V F-1 Engine - Saturn Apollo Program

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Saturn V F-1 Engine - Saturn Apollo Program

description

Summary

A close-up view of the F-1 Engine for the Saturn V S-IC (first) stage depicts the complexity of the engine. Developed by Rocketdyne under the direction of the Marshall Space Flight Center, the F-1 engine was utilized in a cluster of five engines to propel the Saturn V's first stage, the S-IC. Liquid oxygen and kerosene were used as its propellant. Initially rated at 1,500,000 pounds of thrust, the engine was later uprated to 1,522,000 pounds of thrust after the third Saturn V launch (Apollo 8, the first marned Saturn V mission) in December 1968. The cluster of five F-1 engines burned over 15 tons of propellant per second, during its two and one-half minutes of operation, to take the vehicle to a height of about 36 miles and to a speed of about 6,000 miles per hour.

date_range

Date

01/01/1963
place

Location

Marshall Spaceflight Center, Huntsville, Madison County, Alabama, United States, 3580834.63076, -86.66505
Google Map of 34.6307645, -86.665052
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Source

NASA
copyright

Copyright info

Public Domain Dedication (CC0)

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