Venture Aeronautics Project D700
27.8k TheFlightGuySP
2.2 years ago
Overview: the D700 is the first blended flying-wing aircraft to be developed by Venture Aeronautics. The aircraft was designed to test the flight characteristics, safety, practicality, and design features of blended flying-wing aircraft. The aircraft is powered by two Venture Aeronautics JE-11 experimental turbofan engines, which were designed to be very efficient and less noisy compared to other turbine engines.
FLIGHT CHARACTERISTICS
Maximum Airspeed (TAS): 350mph, 563kph, 304knots.
Maximum Altitude: 30,000ft, 9,144m.
Takeoff Airspeed (IAS)(75% Power): ~165mph, ~266kph, ~143knots.
Landing Airspeed (IAS): ~100mph, ~161kph, ~87knots.
Controls:
- Activate1/2: Start Up/Shut Down Engine 1/2.
- Trim: Trim.
NOTES
- The difference in the aircraft's takeoff and landing airspeed is largely due to the engine and landing gear placement.
- If one of the engines is shut down mid-flight, the aircraft will go into an uncontrollable roll-over spin.
- Yawing the aircraft will cause the aircraft to roll. However, non-commanded oscillations will be counteracted by the fly-by-wire yaw system.
Specifications
Spotlights
- WINGSIRONAVIATION 2.2 years ago
General Characteristics
- Created On Windows
- Wingspan 77.9ft (23.8m)
- Length 51.3ft (15.6m)
- Height 19.2ft (5.8m)
- Empty Weight N/A
- Loaded Weight 24,698lbs (11,203kg)
Performance
- Power/Weight Ratio 0.545
- Wing Loading 22.5lbs/ft2 (110.0kg/m2)
- Wing Area 1,096.0ft2 (101.8m2)
- Drag Points 4633
Parts
- Number of Parts 112
- Control Surfaces 0
- Performance Cost 713
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