KT-2A (original) (raw)

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KT-2A

Part of DF-31

KT-2 & KT-2A

Heavy all-solid propellant Chinese launch vehicle. Model first displayed at Wuzhai in the fall of 2002. Consists of two parallel first-stage booster motors derived new the first stage motor of the KT-1, a larger-diameter core second stage motor like that of the KT-2, a new larger-diameter third stage motor, and an enormous new fairing. All figures are rough estimates.

AKA: Kaituozhe-2A;SLV-2A. Status: Development ended 2002. Payload: 2,000 kg (4,400 lb). Gross mass: 80,000 kg (176,000 lb). Height: 30.00 m (98.00 ft). Diameter: 2.70 m (8.80 ft). Span: 6.70 m (21.90 ft). Apogee: 500 km (310 mi).

LEO Payload: 2,000 kg (4,400 lb) to a 500 km orbit at 98.00 degrees.

Family: all-solid, orbital launch vehicle. Country: China. Agency: KT, Space Solid Fuel Rocket Carrier Co Ltd.

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