This is our dream project after Concorde landed. Concorde landed due to High Operating Cost, Sonic Boom (Not able to fly over the land at Supersonic Speed ), High Fuel Consumption, Low Passenger capacity, Low Range. Several companies are involving design supersonic business jets. NASA has developed various technology to minimize sonic boom by various design. Today’s concept on the second-generation commercial supersonic flight is to design the flight that can fly at supersonic speed over the sea and can fly at subsonic speed over the land. But our flight will be able to fly at supersonic speed over the sea and land with our efficient structure. Our efficient nose cone will reduce the sonic boom level to very lower level and the efficient wing will increase the L/D ratio, range. The efficient High and Low Bypass ratio Gimbal Thrust Turbofan engine will reduce the fuel consumption at all speed.
Specifications*
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R – 9X9 SST
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Capacity |
320 (Single Class) 270 (Two Class) |
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Crew |
2 |
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Cruise Speed |
Mach 3 |
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Range |
13, 000 km |
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Propulsion |
4, RYAN High & Low Bypass Ratio Gimbal Thrust Turbofan Engine |
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Service Ceiling |
75, 000 ft |
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Overall Length |
320 ft 8 in |
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Fuselage Width |
13 ft 7 in |
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Wingspan |
180 ft 5 in |
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Tail Height |
42 ft |
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Max. Takeoff Weight |
3 15 000 Kg |
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Max. Landing Weight |
2 10 000 Kg |
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Max. Zero Fuel Weight |
1 50 000 Kg |
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Max. Usable Fuel |
1 75 000 Lit |
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Takeoff Runway Length |
6 000 ft |
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Landing Runway Length |
7, 000 ft |
* Specifications are based on preliminary design. The specification will change after detail design???????