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Rocket Engine, Combustion Chamber, V-2

National Air and Space Museum

Object Details

Manufacturer
Linke-Hofmann Werke AG
Summary
With a thrust of 25 tons, the V-2 engine was the first large liquid-fuel rocket engine in the world and powered the world’s first ballistic missile, the German V-2 of World War II. The combustion chamber was the engine’s heart. Here, its liquid oxygen and water alcohol propellants entered through 18 injectors on the top and burned at about 2,700 ºC (4,900 ºF).
After the war, both the United States and the Soviet Union copied the V-2 engine, and it greatly influenced the development of large liquid-fuel rocket engines around the world. The U.S. Army probably captured this artifact in central Germany in spring 1945. The Smithsonian later obtained it from the U.S. Air Force.
Credit Line
Transferred from the U.S. Air Force
Inventory Number
A19730004000
Restrictions & Rights
Usage conditions apply
Type
PROPULSION-Rocket Engines
Materials
Overall, steel
Dimensions
Overall: 6ft 2in. x 3ft 7in. (187.96 x 109.22cm)
Country of Origin
Germany
See more items in
National Air and Space Museum Collection
National Air and Space Museum
Record ID
nasm_A19730004000
Metadata Usage (text)
Not determined
GUID (Link to Original Record)
http://n2t.net/ark:/65665/nv96172300c-44c4-4c85-a8b1-4900cbfb572d

Related Content

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    Air and Space Museum
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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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