File:A4-Turbopumpe.jpg

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Deutsch: Treibstoff-Turbopumpe einer A4-Rakete, fotografiert im Historisch-Technischen Informationszentrum Peenemünde. Rot: Dampf, Blau: eine Seite Sauerstoff, eine Seite Alkohol. Förderleistung Alkohol: 55 Liter/s, Sauerstoff: 70 Liter/s. Drehzahl: 3800 U/min. Leistung: 580 PS
English: Propellant turbopump of an A4 rocket, photographed in the Peenemünde Information Centre for History and Technology. Red: steam, blue: one side liquid oxygen, one side alcohol. Flow rate: alcohol: 55 liters/s, liquid oxygen: 70 liters/s. Rotation speed: 3800 rpm. Power: 580 horsepower
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current13:39, 17 April 2006Thumbnail for version as of 13:39, 17 April 20062,272 × 1,704 (1.12 MB)Captain Crunch (talk | contribs){{Information| |Description=Treibstoff-Turbopumpe einer A4-Rakete, fotografiert im Historisch-Technischen Informationszentrum de:Peenemünde. Rot: Dampf, Blau: eine Se

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