V-2 Combustion Chamber at the Udvar-Hazy Center

V-2 Combustion Chamber at the Udvar-Hazy Center
With a thrust of 25 tons, the V-2 motor was the world's first large, liquid-fuel rocket engine, and it powered the world's first ballistic missile, the German V-2 of World War II.
  • WEB10833-2008

  • Copyright/Owner: Smithsonian Institution
  • Source: National Air and Space Museum, Smithsonian Institution
  • Photographer: Dane Penland
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