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Yakovlev Yak-17


Single-Seat, Single-Engine Jet-Powered Fighter Aircraft


The Yakovlev Yak-17 is a direct development of the jet-powered Yak-15 type.
Authored By: Staff Writer | Last Edited: 1/21/2019
The Yak-17 was a solid operator in service with the Soviet Union. As a post-World War Two design, the system had its roots in the Yak-3 piston-engine fighter which spawned the jet-powered Yak-15 - of which the Yak-17 was a direct development of. The Yak-17 appeared in twice the numbers as did the Yak-15, featuring a host of improvements over its predecessor.

The Yak-17 was fitted with a larger and more powerful engine in the form of the Klimov RD-10A turbojet engine. Still retaining the fuselage characteristics of a piston-engine aircraft, the Yak-17 did in fact feature a tricycle retractable undercarriage with no tail wheel - something found on the Yak-15. Wings were of a straight-wing design and elevators were mounted close to the single rudder - an arrangement still stemming from piston-engine aircraft development.

The base cockpit seated one pilot and a pilot and trainer in the two seat conversion model. Vision was reportedly good from the front and to the sides with decent peripheral vision at rear. Outwardly, provisions for drop tanks increased the combat radius and loitering time the system - a pivotal consideration for the early fuel-hungry turbojets and standard armament consisted of just 2 x 23mm fixed-forward cannons mounted in the nose.

The Yak-17 served along with Soviet-controlled countries up until the middle of the 1950s where the system would soon give in to the ever-advancing aircraft in the development pipeline.






Specifications



Year:
1947
Status
Retired, Out-of-Service
Crew
1
[ 430 Units ] :
Yakovlev OKB - Soviet Union
National flag of Czechoslovakia National flag of Poland National flag of Soviet Union Czechoslovakia; Poland; Soviet Union
- Fighter
Length:
28.81 ft (8.78 m)
Width/Span:
30.18 ft (9.2 m)
Height:
6.89 ft (2.1 m)
(Showcased structural dimension values pertain to the Yakovlev Yak-17 production model)
Empty Weight:
5,357 lb (2,430 kg)
MTOW:
7,326 lb (3,323 kg)
(Diff: +1,969lb)
(Showcased weight values pertain to the Yakovlev Yak-17 production model)
1 x Klimov RD-10A turbojet engine developing 2,205 lb of thrust.
(Showcased powerplant information pertains to the Yakovlev Yak-17 production model)
Maximum Speed:
466 mph (750 kph; 405 kts)
Service Ceiling:
41,831 feet (12,750 m; 7.92 miles)
Maximum Range:
446 miles (717 km; 387 nm)
Rate-of-Climb:
2,828 ft/min (862 m/min)
(Showcased performance values pertain to the Yakovlev Yak-17 production model; Compare this aircraft entry against any other in our database)
2 x 23mm automatic cannons.
(Showcased armament details pertain to the Yakovlev Yak-17 production model)
Yak-17 - Single Seat Production Model
Yak-17UTI - Two-Seat Conversion Trainer

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