HAL HT-2
Indian two-seat primary trainer
- 1 min read
- 2 chapters
Related on Lably
Operators
Military operators
- Ghana Air Force (retired)
- 12 HAL HT-2s were delivered and used between 1959 and 1974.
- India
- Indian Air Force (retired)
- Indian Navy (retired)
Civilian operators
- Indian Flying schools
Sign in to keep reading
One more chapter is free with a Lably account.
Specifications (HT-2)
Data from Jane's All The World's Aircraft 1953–54
General characteristics
- Crew: 2
- Length: 7.53 m (24 ft 8 in)
- Wingspan: 10.72 m (35 ft 2 in)
- Height: 2.74 m (9 ft 0 in)
- Wing area: 16.0 m2 (172 sq ft)
- Aspect ratio: 7.13:1
- Airfoil: NACA 23012
- Empty weight: 699 kg (1,540 lb)
- Gross weight: 1,016 kg (2,240 lb)
- Fuel capacity: 117 L (26 imp gal; 31 US gal)
- Powerplant: 1 × Cirrus Major III air-cooled four-cylinder inverted inline engine, 116 kW (155 hp)
Performance
- Maximum speed: 210 km/h (130 mph, 110 kn)
- Cruise speed: 185 km/h (115 mph, 100 kn)
- Stall speed: 84 km/h (52 mph, 45 kn)
- Range: 560 km (350 mi, 300 nmi)
- Endurance: 3 hr 30 min
- Service ceiling: 4,400 m (14,500 ft)
- Rate of climb: 4.1 m/s (800 ft/min)