Soko J-22 Orao

· SOKO · 2 × Armstrong Siddeley Viper

Airplanes

Length

13.02 m

Flat Wing Span

9.3 m

Height

4.52 m

Flat Wing Area

26 m²

Flat Wing Aspect Ratio

3.33

Max Speed

1130 km/h

Max Ceiling

15000 m

Number of Engines

Aircraft Engine

First Flight

1974-10-31

Entry Into service

1978-01-01

Maximum Take-Off Weight

11.08 t (paragliders: kg)

Total Fuel Capacity

3120

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Total Fuel Capacity
Soko J-22 Orao	11.08	3120

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)
Hongdu JL-10		12.4	9.4	Compare
IAR-93 Vultur		14.9	9.3	Compare
Dassault Étendard II	Turbomeca Gabizo	12.89	8.74	Compare
AIDC F-CK-1 Ching-kuo		14.21	9	Compare
Yakovlev Yak-130		11.49	9.84	Compare
Mikoyan-Gurevich MiG-19		12.54	9	Compare

All data (27 fields)

Name: Soko J-22 Orao
Manufacturer: SOKO
Description: The Soko J-22 Orao () is a Yugoslavian and later Serbian twin-engined, subsonic ground-attack and aerial reconnaissance aircraft.
ICAO Code: YURO
First Flight: 1974-10-31
Entry Into service: 1978-01-01
Production End: 1992-01-01
Designer: VTI - Yugoslavia
Type: Attack aircraft, Reconnaissance aircraft
Length (m): 13.02
Height (m): 4.52
Cockpit Crew: 1
Max Speed (km/h): 1130
Min Speed (km/h): 185
Max Ceiling (m): 15000
Rate of Climb (m/s): 89.0016
Armament: 2× GSh-23L cannons in lower front fuselage, below engine air intakes, with 200 rounds per gun; 5 (4 underwing and 1 centreline)
Powerplant Description: 2 × Orao/Turbomecanica-built Rolls-Royce Viper Mk 633-47 turbojets, 17.79 kN thrust each
Primary Users: Serbian Air Force, Yugoslav Air Force (historical) , Bosnian Air Force (historical) , Republika Srpska Air Force (historical)
Status: Active
Wikipedia Article (URL): en.wikipedia.org/wiki/Soko_J-22_Orao
Flat Wing Span (m): 9.3
Flat Wing Area (m²): 26
Flat Wing Aspect Ratio: 3.33
Wake Category: M
Aircraft Engine: Armstrong Siddeley Viper
Number of Engines: 2