The second prototype of the Ramirux corp (now Onicorp) ''STAR PROJECT'' the XR-1B don't have the AMWS system, but have a geometry variable wing, with this system the aircraft can fly at very high speeds with the fold wings. and solve the wings vibration problem at mach1+ speeds, maintaining the high manuevability at low speeds, when the XR-1A prototype crashes, the STAR PROJECT competition has done, with this, the XR-1B it's named IF-15 Nebula
Specifications
General Characteristics
- Created On Windows
- Wingspan 90.8ft (27.7m)
- Length 125.9ft (38.4m)
- Height 24.5ft (7.5m)
- Empty Weight 32,999lbs (14,968kg)
- Loaded Weight 139,999lbs (63,502kg)
Performance
- Power/Weight Ratio 0.481
- Wing Loading 39.9lbs/ft2 (195.0kg/m2)
- Wing Area 3,505.0ft2 (325.6m2)
- Drag Points 9529
Parts
- Number of Parts 116
- Control Surfaces 16
- Performance Cost 1,109
