First Flight: Spring 1943
Service Delivery: July 1943
Final Delivery: N/A
Number Produced: N/A
Model: Klimov VK-105PF
Type: V12 Liquid cooled
Number: One Horsepower: 1,225 hp
Wing span: 30 ft. 2.25 in. (9.20m)
Length: 27 ft. 10.25 in. (8.50m)
Height: 7 ft. 10 in. (2.39m)
Wing Surface Area: 159.53 sq. ft. (14.83 m²)
Empty: 4,960 lbs. (2250 kg)
Max. Take-Off: 5,864 lbs. (2660 kg)
Maximum Speed: 404 mph (650 km/h)
Initial climb: 4,265 ft./min. (1300 m/min)
Service Ceiling: 35,450 ft. (10,800m)
Range: 506 Miles (815 km)
One 20mm ShVAK cannon firing through spinner
Ammunition: 120 Rounds
Two 12.7mm machine guns above engine
Ammunition: 250 Rounds per gun
Design and development - Source: Wikipedia|
The origins of the Yak-3 went back to 1941 when the 1-30 prototype was offered along with the I-26 as an alternate design to the Yak-1. The I-30, powered by a Klimov M-105P engine, was of all-metal construction, using a wing with dihedral on the outer panels. Like the early Yak-1, it had a ShVAK 20 millimeter cannon firing through the prop spinner and twin ShKAS 7.62 millimeter machine guns in the nose, but was also fitted with a ShVAK cannon in each wing. The first of two prototypes was fitted with a slatted wing to improve handling and short-field performance while the second prototype had a wooden wing without slats, in order to simplify production. The second prototype crashed during flight tests and was written off. Although there were plans to put the Yak-3 into production, the scarcity of aviation aluminum and the pressure of the Nazi invasion led to abandoning work on the first Yak-3 in the late fall of 1941.
In 1943, Yakovlev designed the Yak-1M which was a smaller and lighter version of the Yak-1. A second Yak-1M prototype was constructed later that year, differing from the first aircraft in plywood instead of fabric covering of the rear fuselage, mastless radio antenna, reflector gunsight and improved armor and engine cooling. The chief test pilot for the project Piotr Mikhailovich Stefanovskiy was so impressed with the new aircraft that he recommended that it should completely replace Yak-1 and Yak-7 with only the Yak-9 retained in production for further work with the Klimov VK-107 engine. The new fighter, designated theYak-3 entered service in 1944, later than the Yak-9 in spite of the lower designation number. A total of 4,848 aircraft were produced.
The designation Yak-3 was also used for other Yakovlev projects - a proposed but never built, heavy twin-engine fighter and the Yakovlev Yak-7A.
Operational history - Source: Wikipedia
Variants - Source: Wikipedia
Yak-3 (VK-107A) - Klimov VK-107A engine with 1,230 kW (1,650 hp) and 2x 20 mm Berezin B-20 cannons with 120 rounds of ammunition each. After several mixed-construction prototypes, 48 all-metal production aircraft were built in 1945-1946. In spite of excellent performance (720 km/h (447 mph) at 5,750 m (18,860 ft)), VK-107 was prone to overheating and it was decided to leave the engine for the better-suited Yak-9.
Yak-3 (VK-108) - Yak-3 (VK-107A) modified with VK-108 engine with 1,380 kW (1,850 hp), and armed a single 23 mm Nudelman-Suranov NS-23 cannon with 60 rounds of ammunition. The aircraft reached 745 km/h (463 mph) at 6,290 m (20,630 ft) in testing but suffered from significant engine overheating. Another Yak-3 with 2x 20 mm Berezin B-20 cannons was also fitted with the engine with similar results.
Yak-3K - tank destroyer with a 45 mm Nudelman-Suranov NS-45 cannon, only a few built because Yak-9K was a better match for the weapon
Yak-3P - produced from April 1945 until mid-1946, armed with 3x 20 mm Berezin B-20 cannons with 120 rounds for the middle cannon and 130 rounds for each of the side weapons. The three-cannon armament with full ammunition load was actually 11 kg (24 lb) lighter than that of a standard Yak-3, and the one-second burst mass of 3.52 kg (7.74 lb) was greater than that of most contemporary fighters. Starting in August 1945, all Yak-3 were produced in the Yak-3P configuration with a total of 596 built.
Yak-3PD - high-altitude interceptor with Klimov VK-105PD engine and a single 23 mm Nudelman-Suranov NS-23 cannon with 60 rounds of ammunition, reached 13,300 m (43,625 ft) in testing but did not enter production due to unreliability of the engine.
Yak-3RD (Yak-3D) - experimental aircraft with an auxiliary Glushko RD-1 liquid-fuel rocket engine with 2,9 kN (650 lbf) of thrust in the modified tail, armed with a single 23 mm Nudelman-Suranov NS-23 cannon with 60 rounds of ammunition. On May 11, 1945, the aircraft reached 782 km/h (485 mph) at 7,800 m (25,585 ft). During the August 16 test flight, the aircraft crashed for unknown reasons, killing the test pilot V.L. Rastorguev. Like all mixed powerplant aircraft of the time, the project was abandoned in favor of turbojet engines.
Yak-3T - tank destroyer version armed with 1x 37 mm Nudelman N-37 cannon with 25 rounds and 2x 20 mm Berezin B-20S cannons with 100 rounds each. Cockpit was moved 0.4 m (1 ft 4 in) back to compensate for the heavier nose. Engine modifications required to accept the weapons resulted in serious overheating problems which were never fixed and the aircraft did not advance beyond the prototype stage.
Yak-3T-57 - single Yak-3T with a 57 mm OKB-16-57 cannon
Yak-3TK - powered by a VK-107A engine, and fitted with an exhaust turbocharger.
Yak-3U - Yak-3 fitted with Shvetsov ASh-82FN radial engine with 1,380 kW (1,850 hp) in an attempt to increase performance while avoiding the overheating problems of VK-107 and VK-108. Wingspan increased by 20 cm (8 in), wings moved 22 cm (9 in) forward, cockpit raised by 8 cm (3 in). Armament of 2x 20 mm Berezin B-20 cannons with 120 rounds per gun. The prototype reached 682 km/h (424 mph) at 6,000 m (19,680 ft) and while successful did not enter production because it was completed after the war.
Yak-3UTI - two-seat conversion trainer based on Yak-3U powered by Shvetsov ASh-21 radial piston engine. The aircraft became the prototype for the Yak-11.