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Rocket Engine, Liquid Fuel, Reaction Control System (RCS), SE8-9, for Apollo 4

National Air and Space Museum
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Object Details

Manufacturer
Rocketdyne Division, Rockwell International
Summary
This is a Reaction Control System (RCS) rocket engine for the yaw control of the Apollo space craft. It was flown on Apollo 4, launched in November 1967. This was the first flight of the Saturn V in which the Command Model (CM) made three orbits followed by a successful reeentry and splashdown. It was a crucial mission and verified the first "all up" test of all stages of the the Saturn V. The RCS system consisted of twelve engines in all operating in tandem. The system produced small pulses or bursts thrusts as needed over a 30 minute mission period. The pulses placed the CM in its proper position for re-entry into the Earth's atmosphere. This RCS was transferred to the Smithsonian in 1977 by the NASA Johnson Space Flight Center.
Credit Line
Transferred from NASA, Johnson Space Center.
Inventory Number
A19770883000
Restrictions & Rights
Usage conditions apply
Type
PROPULSION-Rocket Engines
Materials
Aluminum
Wood
Steel
Electrical Components
Plastic
Synthetic Fibers
Adhesive Tape
Ink
Dimensions
3-D (Overall): 30.5 × 21.6 × 17.8cm (1 ft. × 8 1/2 in. × 7 in.)
Country of Origin
United States of America
See more items in
National Air and Space Museum Collection
National Air and Space Museum
Record ID
nasm_A19770883000
Metadata Usage (text)
Not determined
GUID (Link to Original Record)
http://n2t.net/ark:/65665/nv9cfa94548-73ab-4632-b252-f54d14b7124c

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