S-76C++
Press1 for turn on nav lights, nice flying!
Design:
The S-76 is of conventional configuration, with a four-bladed fully articulated main rotor and a four-bladed anti-torque rotor on the port side of the tailboom. Two turboshaft engines are located above the passenger cabin. In the prototypes and initial production aircraft, these engines were Allison 250-C30s, a new version of the popular Allison 250 engine developed specially for the S-76, with a single-stage centrifugal com mpressor instead of the multi-stage axial/centrifugal compressor of earlier models of the engine, rated at 650 shp (480 kW) for takeoff. These engines are connected to the main rotor by the main gearbox, a three-stage unit with a bull gear as its final stage rather than the planetary gear used by previous generations of Sikorsky helicopters. This arrangement has 30% fewer parts and lower costs than a more conventional design.
Specifications
Spotlights
- Bori0 7.4 years ago
General Characteristics
- Created On Windows
- Wingspan 42.8ft (13.0m)
- Length 47.1ft (14.4m)
- Height 14.1ft (4.3m)
- Empty Weight N/A
- Loaded Weight 16,145lbs (7,323kg)
Performance
- Horse Power/Weight Ratio 0.216
- Wing Loading 118.6lbs/ft2 (579.1kg/m2)
- Wing Area 136.1ft2 (12.6m2)
- Drag Points 5787
Parts
- Number of Parts 141
- Control Surfaces 2
- Performance Cost 570
The last comment is a lie !!! 😂😂😂😂
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