Akula SB-3
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Akula SB-3 | |
---|---|
Role | Strategic bomber |
National origin | Tennai |
Manufacturer | Akula Industries |
First flight | 1980 |
Introduction | 1984 |
Status | In service |
Primary user | Royal Tennaiite Air Force |
The Akula SB-3 is a Tennaiite strategic bomber in service with the Royal Tennaiite Air Force.
Development
Design
Overview
Weapons
Upgrades
Operational History
Royal Tennaiite Air Force
Other nations
Variants
Operators
Specifications (SB-3C)
General characteristics
- Crew: 2
- Length: 26.82 m (88 ft 0 in)
- Wingspan: 21.34 m (70 ft 0 in)
- Lower wingspan: 13.72 m (45 ft 0 in) swept
- Height: 6.71 m (22 ft 0 in)
- Empty weight: 23,511 kg (51,833 lb)
- Max takeoff weight: 63,503 kg (140,000 lb)
- Fuel capacity: More than 29030 kg
- Powerplant: 2 × Gikrabanda F120 afterburning turbofan, 105 kN (24,000 lbf) thrust each dry, 156 kN (35,000 lbf) with afterburner
Performance
- Maximum speed: 1,852 km/h (1,151 mph; 1,000 kn)
- Range: 9,300 km (5,779 mi; 5,022 nmi)
- Combat range: 5,400 km (3,355 mi; 2,916 nmi)
- Ferry range: 15,000 km (9,321 mi; 8,099 nmi)
- Service ceiling: 45,000 m (148,000 ft)
- Rate of climb: 30 m/s (5,900 ft/min)
Armament
- Hardpoints: 10 total;4 × rotating under-wing pylons, 6× conformal stations, internal weapons bay with a capacity of up to 11,500 kg (25,400 lb) of stores on external stations and up to 17,000 kg (37,000 lb) for a total maximum capacity of 28,500 kg (62,800 lb),
- Rockets:
- Missiles:
- Bombs:
Avionics
- ML/M-2032 pulse doppler radar