Top speed 250 km/h Length 7.3 m Manufacturer Yakovlev | Wingspan 10 m First flight September 7, 1944 | |
The Yakovlev Yak-5 (Russian: Яковлев Як-5) was an experimental trainer aircraft designed by Yakovlev OKB in the Soviet Union, and first flown in 1944. It was the first Yakovlev aircraft to be fitted with a variable-pitch propeller. It did not enter production.
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Development and design
In 1944, the Yakovlev UT-2 was the standard primary trainer of the Soviet Air Forces, but its simplicity caused problems when pilots moved on to more sophisticated aircraft, so the Yakovlev design bureau designed a more sophisticated derivative, the UT-2L, which featured an enclosed tandem cockpit, the addition of flaps and blind flying instruments.
At the same time, Yakovlev designed a single-seat aircraft based on the UT-2L, intended as a fighter-trainer. This aircraft, the Yak-5, was a low-wing monoplane of wooden construction, but unlike the UT-2, had the front cockpit removed and an enclosed sliding canopy placed over the rear cockpit. A retractable tailwheel undercarriage replaced the fixed landing gear of the UT-2. It was powered by a Shvetsov M-11D five-cylinder radial producing 115 hp (86 kW), which drove a two-bladed variable-pitch propeller. It could be fitted with a single synchronized ShKAS machine gun aimed by a reflector sight, while the aircraft was also fitted with a radio.
Operational history
The prototype Yak-5 first flew on 7 September 1944. The new fighter-trainer's handling proved popular with its test pilots, and the aircraft successfully passed official evaluation. In the end, neither the UT-2L or the Yak-5 entered production because the Soviet Air Force command believed wooden aircraft were becoming obsolete, which would result in production of the all-metal Yakovlev Yak-18 trainer in late 1945. The sole Yak-5 was destroyed when it suffered failure of the wooden wing during a snap roll and crashed.
Specifications (Yak-5)
Data from Yakovlev Aircraft since 1924
General characteristics
Performance