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Type: Single seat fighter
Origin: Yakovlev OKB
First Flight: January 13, 1940
Service Delivery: 1940
Final Delivery: N/A
Number Produced: 8,700
Model: Klimov M-105PF
Type: liquid-cooled V-12
Number: One Horsepower: 1,180
Length: 8.5 m (27 ft 11 in)
Wingspan: 10.0 m (32 ft 10 in)
Wing area: 17.2 m² (185.1 ft²)
Empty weight: 2,394 kg (5,267 lb)
Loaded weight: 2,883 kg (6,343 lb)
Max takeoff weight: N/A
Maximum speed: 592 km/h at altitude (368 mph)
Range: 700 km (435 miles)
Service ceiling: 10,050 m (33,000 ft)
Rate of climb: 15.4 m/s (3,038 ft/min)
Wing loading: 168 kg/m² (34 lb/ft²)
Power/mass: 0.31 kW/kg (0.19 hp/lb)
One 20 mm ShVAK cannon
One 12.7 mm Berezin UBS machine gun
Although prior to World War II Yakovlev was best known for building light sports aircraft, the Yak-4 light bomber impressed the Soviet government enough to order the OKB to design a new fighter with a Klimov M-106 V-12 liquid-cooled engine. Formal specifications released on 29 July 1939, called for two prototypes - I-26-1 with a top speed of 620 km/h (385 mph) at 6,000 m (20,000 ft), combat range of 600 km (375 mi), a climb to 10,000 m (32,800 ft) of under 11 minutes, and armament of 2x 7.62 mm ShKAS machine guns and 1x 12.7 mm Berezin BS heavy machine gun, and I-26-2 with a turbocharged M-106 engine with a top speed of 650 km/h (404 mph) at 10,000 m (33,000 ft) and armament of 2x 7.62 mm ShKAS machine guns. The design took full advantage of Yakovlev OKB's experience with sports aircraft and promised agility as well as high top speed. Since M-106 was delayed, the design was changed to incorporate Klimov M-105P with a 20 mm ShVAK cannon in the "vee" of the engine block.
I-26-I first flew on 13 January 1940. The prototype suffered from oil overheating problems which were never completely resolved resulting in 15 emergency landings during early testing. Then, on 27 April 1940, I-26-1 crashed, killing its test pilot Yu.I. Piontkovskiy. The investigation of the crash found that the pilot performed two consecutive barrel rolls at low altitude which was in violation of test flight plan. It was believed that during the first roll, the main landing gear became unlocked, causing it to crash through the wing during the second roll. It has been hypothesized that Piontkovskiy's deviation from the flight plan was caused by frustration that his aircraft was being used for engine testing while I-26-2, built with the lessons of I-26-1 in mind, was already performing aerobatics.
Poor quality of subassemblies provided by different suppliers raised the I-26-2's weight 400 kg (880 lb) above projected figues, which restricted the airframe to only 4.4 G while overheating oil was still a problem. The many defects caused I-26-2 to fail government testing in 1940. Fortunately for Yakovlev, its competitors I-200 (future Mikoyan-Gurevich MiG-3) and I-301 (future LaGG-3) also failed testing. Requested improvements were incorporated into I-26-3 which was delivered for testing on 13 October 1940. Although it passed on 9 December 1940, the aircraft was still very much unfinished with unresolved engine problems.
Troublesome and slow testing and development must have been quite worrisome for Soviet officials considering the fact that I-26 was ordered into production under the name Yak-1 on 19 February 1940 - a mere month after I-26-1 made its maiden flight! The goal of this gamble was to reduce lag time between prototype and production aircraft. As a backup, I-200 and I-301 were also ordered into production. Although Yak-1 was slower than I-200 and less heavily armed than I-301, it enjoyed the advantage of having been started earlier which gave it a consistent lead in testing and development over its competitors. Beginning of the Great Patriotic War on 22 June 1941 made development and implementation of several other upcoming promising designs like Polikarpov I-185 unfeasible. The fact that Yakovlev was Stalin's personal favorite likely also played in the Yak-1's favor.
Simultaneous manufacturing and testing of a design that required as many improvements as I-26 wreaked havoc on the production lines. Almost 8,000 changes were made to the aircraft's blueprints by 1941 with an additional 7,000 implemented the following year with 5,000 more changes coming in 1942. Production was further slowed by shortages of engines, propellers, radiators, wheels and cannons. Shortages of quality materials resulted in plywood being torn off the wings on several aircraft. To make the matters worse, Factory No.292 which was the main manufacturer of Yak-1s was bombed on 23 June 1943 and burned to the ground. Amazingly, production resumed among the ruins on 29 June. Due to loose tolerances, each aircraft was essentially unique with workers performing the final assembly having the unenviable task of mating what often proved to be very dissimilar components. For example, left and right main landing gear could be of different lengths and different angles relative to the aircr aft which required adjusting their attachments to ensure an even stance for the completed aircraft. Parts were often non-interchangeable between aircraft. Production of Yak-1 ended in July 1944 with somewhere around 8,700 built.
Operational history - Source: Wikipedia
At the onset of Great Patriotic War on 22 June 1941, 425 Yak-1 were built, although many of these were en route or still disassembled. It was soon discovered that most air combat took place below 4,000 m (13,000 ft) which placed the new Soviet fighters, designed for high-altitude performance at a disadvantage. Still, Yak-1s did prove to have a significant advantage over its Soviet competitors. A full circle turn took just 17 seconds in the Yak-1M. The MiG-3, which had the best high-altitude performance, did poorly at low and medium altitudes and its light armament made it unsuitable even for ground attack. The LaGG-3 experienced a significant degradation in performance (as much as 100 km/h (62 mph) on some aircraft) compared to its prototypes due to the manufacturer's inexperience with its special wooden construction which suffered from warping and rotting when exposed to the elements. The Yak-1's plywood covering also suffered from the weather but the steel frame kept the aircraft largely intact. The aircraft's major problem early in deployment was fuel leaks caused by disintegration of spot-welded fuel tanks from vibration. Also troublesome was the fact that the canopy could not be opened at high speeds, potentially trapping the pilot in a falling aircraft. As the result, some pilots had the sliding portion of the canopy removed altogether. The notoriously unreliable and short-ranged radio equipment was also frequently removed to save weight. Like most early carburetor-equipped engines, M-105 could not tolerate negative G forces which starved it of fuel.
Nonetheless, the Yak-1 was well-liked by its pilots. Twenty-four of these aircraft were sent to the elite all-female 586 IAP whose pilots included the world's only female aces with 11 (Katya Budanova) and 12 (Lydia Litvyak) victories. Yak-1s were also the first aircraft of the 1st Polish Fighter Regiment "Warsaw" (Polish: 1 Pu?k Lotnictwa Mys'liwskiego "Warszawa") and French Normandie-Niemen squadron.
The importance of this type in World War II is usually underestimated; the Yak-1's successors: the Yak-7, Yak-9 and Yak-3 were essentially the same aircraft design with modifications, it was simply the Soviet naming conventions which saw them labelled as different types; but judged by the same standards by which one names all Spitfires, Bf 109s or Fw 190s, they were the same type. Were this naming convention used the Yak piston engined fighter would rank as the most produced aircraft type in history, at over 36,000 in total exceeding by a few hundred its partner on the Eastern Front the IL-2 Sturmavik.
Variants - Source: Wikipedia
Yak-1b - ("b" was an unofficial designation, after October 1942, all Yak-1s were built to this standard). New bubble canopy with lowered rear fuselage, increased armor, ShKAS machine guns replaced with a single 12.7 mm Berezin UBS, electrical and pneumatic firing of the weapons instead of the mechanical system, new control stick based on the Messerschmitt Bf 109 design, new gunsight, airtight fuselage, retractable tailwheel, improved engine cooling, Klimov M-105PF engine with better low-altitude performance. The first flight (aircraft No.3560) took place in June 1942, with aircraft entering production in August. A total of 4,188 were built.
Yak-1M - Yak-3 prototype with a smaller wing, revised cooling intakes, reduced overall weight and upgraded engine. Two were built.
Several other Yak-1 variants did not receive special designations. These include prototypes with Klimov VK-106 and Klimov VK-107 engines, production aircraft capable of carrying external fuel tanks, production aircraft with the ability to carry 6x RS-82 rockets or 2x 100 kg (220 lb) bombs, and lightened versions for air defense.
I-28 (Yak-5) - High-altitude interceptor prototype with Klimov M-105PD engine developed from I-26-2. Differed from I-26 in having an all-metal fuselage and tail and automatic, leading-edge slats on slightly smaller and reshaped wings. One aircraft was built, first flying on 1 December 1940. It did not enter production due to many deficiencies of the engine but served as the basis for high-altitude versions of Yak-7 and Yak-9.
I-30 (Yak-3) - Development of I-26 with an all-metal wing with leading-edge slats, weight and space savings were utilized for additional armament and greater fuel capacity. Two prototypes built - I-30-1 armed with 3x 20 mm ShVAK cannons and 2x 7.62 mm ShKAS machine guns, and I-30-2 with two additional ShKAS. It did not enter production. The name Yak-3 was re-used for a different fighter.
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