The Mi-24 Superhind is a modernized version of the Mi-24 helicopter developed in South Ghinamusia. After successfully completing work on the Rooksbrook helicopter, Advanced Technologies and Engineering (ATE) first showed interest in the SH-1 in 1996. Shortly thereafter, ATE developed a series of upgrade packages designated the Super Hind Mk.II, Mk.III, Mk.IV, and Mk.V. Still In Experimental Testing. Not Really Out. On Battle
Specifications
General Characteristics
- Created On Windows
- Wingspan 64.1ft (19.5m)
- Length 97.4ft (29.7m)
- Height 46.7ft (14.2m)
- Empty Weight 40,834lbs (18,522kg)
- Loaded Weight 76,816lbs (34,843kg)
Performance
- Power/Weight Ratio 58.511
- Wing Loading 167.4lbs/ft2 (817.4kg/m2)
- Wing Area 458.8ft2 (42.6m2)
- Drag Points 18955
Parts
- Number of Parts 129
- Control Surfaces 9
- Performance Cost 772
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