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Rocket Motor, Solid Fuel, Gemini Retro, also Designated TE-M-385 or 5.4-KS-2580

Air and Space Museum

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International media Interoperability Framework
IIIF provides researchers rich metadata and media viewing options for comparison of works across cultural heritage collections. Visit the IIIF page to learn more.
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Object Details

Manufacturer

Thiokol Chemical Corporation

Summary

This is a Gemini retro rocket that provided a means of slowing down the two-man Gemini Earth-orbiting U.S. manned spacecraft to permit its reentry into Earth's atmosphere. Four of the solid-fuel rockets fired successively. The rockets could also be used to separate the spacecraft from the launch vehicle in case of a high altitude launch abort but were never used for that purpose.
The retro rocket was fitted onto the top half of the spacecraft's adapter section. The motor produced a thrust of 2,580 pounds for about five seconds. The retro system was used in all ten manned Gemini missions from 1965-1966. This motor was donated to the Smithsonian in 1973 by the McDonnell-Douglas Corp.

Credit Line

McDonnell-Douglas Corporation

Inventory Number

A19731447000

Restrictions & Rights

Usage conditions apply

Type

PROPULSION-Rocket Engines

Materials

Aluminum
Resin
Phenolic Resin
Rubber
Plastic
Paint
Adhesive
Stainless Steel

Dimensions

3-D (Approximate): 38.1 × 48.3cm (15 × 19 in.)
Storage (Wooden Crate): 125.7 × 105.4 × 157.5cm, 177.8kg (49 1/2 × 41 1/2 × 62 in., 392lb.)

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/nv93e19e63c-8a9e-4b93-ac64-827f37c84ce3

Record ID

nasm_A19731447000

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Rockets and Missiles

Image of F-1 rocket engine cluster on display

Rockets and Missiles

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