T-4

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T-4

Mach 3 rocket carrier. Sukhoi experimental interceptor - delta wing with forward canards. A modification to be used as first stage in Sukhoi proposal for Spiral manned spaceplane project. Maximum release conditions: 25,000 kg at 3,000 kph at 20,000 m altitude

Status: Out of Production. Payload: 25,000 kg (55,000 lb). Thrust: 633.50 kN (142,416 lbf). Gross mass: 114,400 kg (252,200 lb). Unfuelled mass: 55,600 kg (122,500 lb). Specific impulse: 1,980 s. Specific impulse sea level: 1,800 s. Burn time: 5,400 s. Height: 44.50 m (145.90 ft). Diameter: 6.40 m (20.90 ft). Span: 22.00 m (72.00 ft). Location: 830.

No Engines: 4. Release velocity: 830 m/s (2,720 ft/sec). Release altitude: 20 m (65 ft). Release angle: 0 deg.

Country: Russia. Engines: RD-36-41. Propellants: Air/Kerosene.

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