C-160
사용국가
독일 공군 소유의 C-160
제원 (C-160)
Orthographic projection of a Transall C-160
The Transall C160NG, escardon Anjou, French Air Force
정보의 출처: Jane's All The World's Aircraft 1982-83
일반 특성
- 승무원: Three—two pilots, flight engineer
- 용량:
- 93 troops or
- 61–88 paratroops or
- 62 stretchers
- 화물탑재량: 16,000 kg (35,275 lb)
- 길이: 32.40 m (106 ft 3½ in)
- 날개폭: 40.00 m (131 ft 3 in)
- 높이: 11.65 m (38 ft 2¾ in)
- 날개면적: 160.0 m² (1,722 ft²)
- 공허중량: 29,000 kg (63,935 lb)
- 최대이륙중량: 51,000 kg (112,435 lb)
- 엔진: 2× Rolls-Royce Tyne Rty.20 Mk 22 turboprop, 4,549 kW (6,100 ehp) 각각
성능
- 초과금지속도: 593 km/h (320 knots, 368 mph)
- 최대속도: 513 km/h (277 knots, 319 mph) at 4,875 m (16,000 ft)
- 실속속도: 177 km/h (95 knots, 110 mph) flaps down
- 항속거리: 1,853 km (1,000 nmi, 1,151 mi) with 16,000 kg payload, 30 min reserves
- 최대항속거리: 8,858 km (4,780 nmi, 5,504 mi)
- 상승한도: 8,230 m (27,000 ft)
- 상승률: 6.6 m/s (1,300 ft/min)
- 날개하중: 319 kg/m² (65.3 lb/ft²)
- 출력대중량비: 0.18 kW/kg (0.11 hp/lb)
각주
- ↑ Hewson, R. The Vital Guide to Military Aircraft 2nd edition. Airlife Publishing Ltd., England 2001.
- ↑ Taylor 1982, pp. 119–120.