Saab SAAB 105
Summary
Category | Training aircraft |
Origin country | πΈπͺ Sweden |
First flight | 29 June 1963 |
Year of introduction | 1967 |
Number produced | 192 units |
Description
The Saab 105 is a military aircraft developed by Saab, a Swedish aerospace company. It was primarily designed as a trainer and light attack aircraft, serving in various air forces around the world. The development of the Saab 105 started in the late 1960s, with the aircraft's first flight taking place in 1963. It features a twin-engine configuration and a streamlined design, allowing for efficient flight performance. Its versatile capabilities make it suitable for training purposes, reconnaissance missions, and limited attack roles. The Saab 105 has been deployed by several European countries, including Sweden, Austria, and Finland, successfully fulfilling its intended roles.
Technical specifications
Version: 105Γ | |
---|---|
Maximum speed | 970 km/h (603 mph) |
Wing area | 16.3 mΒ² (175.5 sqft) |
Wingspan | 9.5 m (31.2 ft) |
Height | 2.7 m (8.9 ft) |
Length | 10.8 m (35.4 ft) |
Empty weight | 2849 kg (6281 lbs) |
Max. takeoff weight | 4635 kg (10218 lbs) |
Powerplant | 2 Γ turbojets General Electric J85-GE-17B delivering 1293 kgp |
Current operating countries
Country | Units | ||
---|---|---|---|
Sweden | 46 |
Numbers in parentheses, e.g. '(+5)', indicate units ordered but not yet delivered.