History
With the success of the Sukhoi Su-17 "Fitter" as a rotor product, it was only natural that the Soviet authorities allowed it to be sold to allies around the world, and this effort set the stage for the Su-20 "Fitter-C" export brand - Primarily based on the Su-17M (S-32MK variant), the Su-20 is equipped with a ranging radar system, an improved navigation suite and a modern attack system, while powered by the AL-21F - 3 24,800 lb thrust engine aircraft also with limited The export number appears as a reconnaissance variant called "Su-20R" - which is based on the Su-17R reconnaissance model. The Su-17 was later developed into a greatly improved export version known as the "Su-22".
Weapons include 2 x 30mm Nudelman-Rikhter NR-30 series internal cannons for close range work. The fuselage also contains about ten brackets for carrying a variety of air-to-air and air-to-surface munitions.
Its crew was one person, and the export model retained much of the form and function of the Soviet line. Operational use of the Su-20 fell to Egypt, Poland and Syria, where they served fighter-bomber and ground attack missions.
Specification
Basic
Production
Roles
- Fighter
- Intercept
- Ground Attack
- Reconnaissance (RECCE)
- Education
Dimensions
18.75m
45.28 ft (13.8 m)
16. 40 feet (5 m)
Weight
19,500 kg
Performance
Performance
1,379 mph (2,220 km/h; 1,199 knots)
49,869 ft (15,200 m; 9.44 mi)
419 miles (675 km; 364 nmi)
Armor
Default:
2 x 30mm Nudelman-Rikhter NR-30 Cannons
10 hardpoints for various air-to-air or air-to-ground munitions.
Austin A. F. T. 3 (Osprey) History
Heading into 1918 during World War 1, there was already work being done to find a viable successor to the classic Sopwith Camel biplane fighter. The Camel appeared in June of 1917 and, by wartime standards, it lived a healthily long service life amidst changing technologies and tactics concerning the air war.
The Austin Osprey, a single-seat triplane fighter - was developed with the hopes that it could follow the veteran design but it eventually lost out to the Sopwith Snipe - of which nearly 500 were produced from 1918 onward. For the Osprey, only a single prototype was ever made by the Austin Motor Company and the design quickly forgotten.
The original requirement was made by British authorities in 1917 (Specification A. 1. A) calling for a single-seat, twin-gunned mount to succeed the venerable Camel. At this point in the war, the Austen Motor Company, like other concerns in British industry, were already helping in the war effort by producing other company's aircraft designs to meet demand. When the specification came down, Austen decided to try its hand in the design and development of a suitable fighter.
The result was the A. F. T. 3 "Osprey" of which three prototypes were ordered. Interestingly, engineers elected for a triple-wing arrangement over the standard two wings common to many fighters of the period.
On the whole, the Osprey utilized proven construction internally and out as well as traditional design techniques which did little to set it apart from the competition. Dimensions included a length of 17. 6 feet, a wingspan of 23 feet and a height of 18. 7 feet. Empty weight was 500 kilograms to a loaded weight of 860 kilograms.
Power was served from a Bentley BR2 series rotary engine of 230 horsepower fitted to the nose and driving a two-bladed wooden propeller. Performance specs included a maximum speed of 119 miles per hour, a service ceiling of 19,000 feet and endurance up to three hours in the air.
The triple-wing arrangement was all equal-span with a forward cant and parallel strut works.
Armament was the usual pairing of 2 x . 303 Vickers machine guns in fixed, forward firing positions over the nose and synchronized to fire through the spinning propeller blades. Another interesting quality of the Osprey was the placement of a third machine gun, this being a Lewis Gun, set upon the center section of the middle wing assembly.
Additionally this installation was trainable to an extent but its flexibility added little.
A first-flight of a prototype Osprey was had during February of 1918 as the war raged and testing followed into the coming weeks. As it stood, the Osprey simply could not compete, performance-wise, with the speedy, two-winged Snipe (fitting the same engine). Its three-winged arrangement created drag despite offering increased agility, this during a time when speed for fighter aircraft was the rule of the day.
As such, the Osprey never advanced beyond the prototype stage and its two remaining prototypes were never built.
Austin A. F. T. 3 (Osprey) Specification
BASICS
MANUFACTURING
ROLES
- Fighter
- X-Plane / Developmental
DIMENSIONS
17. 55 ft (5. 35 m)
22. 97 ft (7 m)
10. 66 ft (3. 25 m)
WEIGHTS
1,102 lb (500 kg)
1,896 lb (860 kg)
POWER
PERFORMANCE
118 mph (190 kph; 103 kts)
19,029 feet (5,800 m; 3. 6 miles)
354 miles (570 km; 308 nm)
980 ft/min (299 m/min)
ARMAMENT
STANDARD:
2 x . 303 Vickers machine guns in fixed, forward-firing positions over the nose and synchronized to fire through the spinning propeller blades.
Su-17M3 / S-52 (Fitter-H) - additional fuel and avionics; based on two-seater trainer without second cockpit; improved range; internal Doppler radar system; AA-2 installed and the launch track of the AA-8 rocket; production from 1976 to 1981.
Su-22M / S-52K (Fitter-J) - Export model designation of Su-17M3; equipped with Tumansky R-29 series engines; downgraded avionics.
Su-22M3 / S-52MK (Fitter-J) - Export model designation of the Su-17M3 with existing Soviet Su-17M3 avionics.
Su-17UM3 / S-52UM3 (Fitter-G) - Improved two-seat trainer; Su-17M3 avionics; produced from 1978 to 1982.
Su-22UM3 (Fitter-G) - Export model designation of the Su-17UM3 trainer; equipped with Tumansky R-29 engines.
Su-22UM3K (Fitter-G) - Export model designation of Su-17UM3 trainer; equipped with Lyulka AL-21 engine.
Su-17M4 - upgraded avionics suite; improved laser rangefinder; radar alert receiver Sirena; torso and back air intakes for improved engine cooling; solid shock cone; compatible with TV-controlled ammunition; from 1981 Year to 1988 production.
Su-22M4/S-54K - Export model designation for production models of the Su-17M4; production from 1983 to 1990.
Su-22M5 - Modern assembler with French/Russian equipment and systems; hot air; glass cockpit; upgraded avionics suite; Phazotron/Thomson CSF radar system; no laser rangefinder.





