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D-1
Russian tactical ballistic missile. Korolev design for a 'long range' rocket prior to orders to copy the V-2. The 1000 kg rocket would have a range of 32 km. Wingspan 1.0 m; 370 kg propellants; minimum range 12.8 km; maximum velocity 854 m/s; maximum altitude 12.5 km.

Status: Design 1944. Payload: 500 kg (1,100 lb). Gross mass: 1,000 kg (2,200 lb). Height: 4.24 m (13.91 ft). Diameter: 0.48 m (1.58 ft).

Maximum range: 32 km (19 mi).

Subtopics

D-2 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.

D-7 Kosberg isopropyl nitrate monopropellant rocket engine. Missile by Toropov. Out of Production. Intended for air-air missile by I I Toropov. Uncooled thrust chamber. Sea level thrust 11.8 kN.

Family: Early Rocketry, tactical ballistic. Country: Russia. Agency: Korolev bureau. More at: 10938. Bibliography: 283.

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