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TU-134 Tupolev Design Bureau is the former Soviet Union developed the twin-engine narrow-body aircraft. Figure shape layout -134 to -124 outline diagram is based on two engines under the wing of the movement to the end, use a T-shaped tail. Changes completed in 1963, July 29, 1963 a successful maiden flight.
Specifications
General Characteristics
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- Wingspan 106.4ft (32.4m)
- Length 110.8ft (33.8m)
- Height 24.6ft (7.5m)
- Empty Weight 19,411lbs (8,804kg)
- Loaded Weight 134,719lbs (61,108kg)
Performance
- Power/Weight Ratio 1
- Wing Loading 72.6lbs/ft2 (354.7kg/m2)
- Wing Area 1,854.6ft2 (172.3m2)
- Drag Points 7818
Parts
- Number of Parts 112
- Control Surfaces 9
- Performance Cost 843
