Mach 3 rocket carrier. Loaded/empty mass 114,400/55,600 kg. Thrust 633.50 kN. Specific impulse 1980 seconds. 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
No Engines: 4. Release velocity: 830 m/s (2,720 ft/sec). Release altitude: 20 m (65 ft). Release angle: 0 deg.
Location: 830.
Status: Out of Production.
Gross mass: 114,400 kg (252,200 lb).
Unfuelled mass: 55,600 kg (122,500 lb).
Payload: 25,000 kg (55,000 lb).
Height: 44.50 m (145.90 ft).
Diameter: 6.40 m (20.90 ft).
Span: 22.00 m (72.00 ft).
Thrust: 633.50 kN (142,416 lbf).
Specific impulse: 1,980 s.
Specific impulse sea level: 1,800 s.
Burn time: 5,400 s.
More... - Chronology...
Associated Countries
Associated Engines
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RD-36-41 Lyulka turbojet engine. 158.4 kN. T-4. Out of Production. Used in Sukhoi March 3 aircraft. Thrust is maximum sea level thrust; specific impulse is sea level value at that thrust. Isp=1980s. More...
Associated Propellants
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Air/Kerosene Ambient air (78 % nitrogen, 21% oxygen, etc.) is scooped up by air intakes and used in turbojet, turbofan, ramjet, scramjet, or other airbreathing engines. It is used to burn aviation-grade kerosene, commercial grade JP-4 or JP-5, their military equivalents, or special high-temperature blends such as those used in the SR-71. More...
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