D-2

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D-2

Part of D-1

Russian tactical ballistic missile. Korolev design for a 'long range' rocket prior to orders to copy the V-2. Extended-range winged version of the D-1. The 1200 kg rocket would have a range of 76 km. Wingspan 1.5 m; 370 kg propellants; minimum range 20 km; maximum velocity 628 m/s; maximum altitude 10.7 km.

Status: Design 1944. Payload: 500 kg (1,100 lb). Gross mass: 1,200 kg (2,600 lb). Height: 4.55 m (14.92 ft). Diameter: 0.48 m (1.58 ft).

Maximum range: 76 km (47 mi).

Subtopics

D-2 engine Polyarniy LOx/Kerosene rocket engine. R-3. Out of Production. Competing engine for 3000 km range IRBM design to study problems of long-range rockets. Developed from April 1947 until cancellation.

Family: Early Rocketry, tactical ballistic. Country: Russia. Agency: Korolev bureau. Bibliography: 283.

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