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Rocket Motor, Solid Fuel, Ullage, also Designated TX-280

Air and Space Museum

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International media Interoperability Framework
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Object Details

Manufacturer

Thiokol Chemical Corporation

Summary

This Ullage solid fuel rocket motor was used on the third stage of the Saturn V launch vehicle that took men to the Moon in Project Apollo. It was one of two such motors fired during the separation of the vehicle's second and third stages. The thrust of the Ullage produced an additional acceleration of the stage during stage separation.
This momentum helped shift the liquid oxygen and liquid hydrogen propellants toward the ends of their tanks in preparation for their entry into the combustion chamber of the main J-2 engine. The Ullage motor produced a thrust of 3,420 pounds. The term "ullage" comes from an old French word, "eullage" meaning "to fill a wine cask." The motor was donated to the Smithsonian in 1976 by Thiokol.

Credit Line

Gift of Thiokol Chemical Corporation

Inventory Number

A19760836000

Restrictions & Rights

Usage conditions apply

Type

PROPULSION-Rocket Engines

Materials

Ferrous Alloy
Non-Magnetic White Metal
Paint
Plaster(?)

Dimensions

3-D: 94 × 21.6cm (3 ft. 1 in. × 8 1/2 in.)

Country of Origin

United States of America

See more items in

National Air and Space Museum Collection

Data Source

National Air and Space Museum

Metadata Usage

Not determined

Link to Original Record

http://n2t.net/ark:/65665/nv9023b112b-53c1-4761-9b33-3c85b94de0b4

Record ID

nasm_A19760836000

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Rockets and Missiles

Image of F-1 rocket engine cluster on display

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