T-32 Spéirling
Jump to navigation
Jump to search
T-32 Spéirling | |
---|---|
Role | Multirole fighter |
National origin | Ossoria |
Manufacturer | Tionscail Ríoga Aeraspáis |
First flight | September 1984 |
Introduction | April 1988 |
Status | In service |
Primary user | Royal Ossorian Air Force |
Produced | 1986–present |
Number built | 890+ |
The T-32 Spéirling (English: hurricane) is a fourth-generation light single-engine multirole fighter aircraft manufactured by the Ossorian aerospace defense company Tionscail Ríoga Aeraspáis (TRA). The Spéirling uses a canard and delta wing configuration as well as a relaxed stability design and fly-by-wire technology for increased maneuverability. It is designed to make use of CSN-standard weapons and perform a wide array of missions, including air supremacy, interdiction, aerial reconnaissance, ground support, and anti-ship strike.
Design and development
Operational service
Royal Ossorian Air Force T-32s fought in the 2018 Arzell Crisis, successfully shooting down several ISAF aircraft for minimal losses.
Variants
- T-32A: initial production version that entered service with the Royal Ossorian Air Force in 1995
- T-32B: two-seat version of the T-32A, with an extended fuselage and the internal cannon removed to make room for the second crewman
- T-32C: upgraded version with improved armament and electronics
- T-32D: two-seat version of the T-32C with similar modifications as the T-32B
- T-32E: upgraded version with a more powerful engine, ASEA radar, expanded payload capacity, and various other improvements
- T-32F: two-seat version of the T-32E with similar modifications as the T-32D
- EF-168: variant built by Aestrup SLS for the Acrean Air Force
Operators
Specifications (T-32E/F)
General characteristics
- Crew: 1/2 (E/F)
- Length: 15.2 m (49 ft 10 in) (E)/15.9 m (52 ft) (F)
- Wingspan: 8.6 m (28 ft 3 in)
- Height: 4.5 m (14 ft 9 in)
- Wing area: 30 m2 (320 sq ft)
- Empty weight: 8,000 kg (17,637 lb)
- Max takeoff weight: 16,500 kg (36,376 lb)
- Fuel capacity: 3400 kg
- Powerplant: 1 × ISA119 afterburning turbofan, 98 kN (22,000 lbf) thrust with afterburner
Performance
- Maximum speed: 2,460 km/h (1,529 mph; 1,328 kn) +
- Maximum speed: Mach 2+
- Cruise speed: 1,470 km/h (913 mph; 794 kn) +
- Combat range: 1,500 km (932 mi; 810 nmi) +
- Ferry range: 4,000 km (2,485 mi; 2,160 nmi) +
- Service ceiling: 16,000 m (52,000 ft)
- g limits: +9 -3
- Time to altitude: 6,000 m (19,685 ft) in 4 minutes
- Wing loading: 283 kg/m2 (58 lb/sq ft)
- Takeoff distance: 500 m (1,640 ft)
- Landing distance: 600 m (1,969 ft)
Armament
- Guns: 1 × 25 mm revolver cannon with 120 rounds
- Hardpoints: 9 (three hardpoints under the fuselage, two under and one on the tip of each wing) with a capacity of 5,300 kg,with provisions to carry combinations of:
Avionics
- AESA radar
- IRST system
- FLIR/LD/Reconnaissance pod hardpoint
- TDL system
- Helmet-mounted display