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Type: High-Altitude Reconnaissance Aircraft Origin: Deutsches Forschungsinstitut für Segelflugzeug Models: V1, V2 and A-series First Flight: N/A Service Delivery: N/A Final Delivery: N/A Total Production: N/A Powerplant: Model: Walter 109-509 Type: Rocket Numer: One Thrust: 3,630 lb. (1650 kg.) Dimensions: Wing span: 57 ft. 7¼ in. (17.56m) Length: 34 ft. 8½ in. (10.58m) Height: N/A Wing Surface Area: N/A |
Weights: Empty: 3,650 lbs. (1642 kg.) Maximum: 9,280 lbs. (4210 kg.) Performance: Maximum speed at high altitude: 559 mph (900 kph) Service Ceiling: 92,021 ft. (25,000m) Maximum Range (combining gliding & powered): 652 miles (1050 km) Armament: None Comments: Made almost entirely of wood with a detatchable cockpit. Launched from Do 217K parent aircraft. Only unpowered flights were made before test airfield was over run by Allied Troops. |
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