Media Information

 
 
 
Collection:
NASA Marshall Space Flight Center Collection
Name of Image:
F-1 Engine
Full Description:
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 of Image:
1963-01-01
Category:
Saturn Apollo Program
term:
Saturn V
term:
F-1 Engine
term:
S-IC stage
facet_what:
Saturn
facet_what:
Apollo 8
facet_where:
Saturn
facet_where:
Marshall Space Flight Center (MSFC)
facet_when:
December 1968
facet_when_year:
1968
Reference Number:
MSFC-75-SA-4105-2C
MIX #:
6413912
NIX #:
MSFC-6413912
MSFC Negative Number:
6413912
UID:
SPD-MARSH-6413912
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