Mikoyan-Gurevich MiG-1
| MiG-1 | |
|---|---|
 |
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| Role | Fighter |
| Manufacturer | Mikoyan-Gurevich |
| First flight | 5 April 1940 |
| Primary user | VVS |
| Produced | 1940 |
| Number built | 100 + 3 prototypes |
| Variants | MiG-3 |
The Mikoyan-Gurevich MiG-1 (Микоян-Гуревич МиГ-1) was a Soviet fighter aircraft of World War II. Although difficult to handle, it formed the basis for the MiG-3, which proved to be a capable high-altitude interceptor aircraft and established a reputation for its designers.
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Design
The MiG-1 was designed in response to a requirement for a high-altitude fighter with an inline engine issued by the VVS in January 1939. Initially the aircraft, designated I-200, was designed in the Polikarpov construction bureau. Work started in June 1939, under the direction of Nikolai Polikarpov and his assistant M. Tetivikin. Polikarpov himself preferred radial engines and promoted his I-180 design at that time, but when the powerful Mikulin AM-37 inline engine became available, he decided to use it in a fighter. The approach that he selected was to build the smallest possible aircraft around the intended powerplant, thereby minimising weight and drag — the philosophy of the light fighter. As specified, the aircraft was to be capable of reaching 670 km/h (417 mph). In August 1939, Polikarpov fell out of favour with Stalin and as a result, when Polikarpov went in November 1939 to tour Germany's aviation works, the Soviet authorities decided to scatter his construction team and create a new Experimental Construction Section (OKO), headed by Artem Mikoyan and Mikhail Gurevich, which remained formally subordinated to Polikarpov bureau until June 1940. Further work upon the I-200 design was assigned to Mikoyan and Gurevich, who later became recognized — not with full justice — as its designers.[1]
Development
The MiG-1 was a low-wing monoplane with a tail-dragging undercarriage of mixed construction. Due to shortages of light alloys the rear fuselage was made from wood, but the front fuselage, from the propeller to the rear of the cockpit was a welded steel tube truss covered by duralumin. The bulk of the wing was wooden, but the center section was all-metal with a steel I-section main spar. The wing used a Clark YH profile. It was evenly tapered with rounded tips and the outer wing panels had 5° of dihedral. All three landing gear wheels retracted hydraulically; the main units inwards into the wing center section. The cockpit was situated well aft, which seriously limited forward vision when landing and taxiing. The AM-37 engine was not yet available and the less powerful V-12 Mikulin AM-35A had to be substituted. It had six exhaust ejectors, one for each pair of cylinders, that provided some additional thrust. It drove a VISh-22Ye controllable pitch propeller 3 metres (9.8 ft) in diameter. The air intakes for the supercharger were in the wing roots and the oil cooler was on the port side of the engine cowling. The radiator was underneath the cockpit. Armament included two fuselage-mounted 7.62 mm (0.300 in) ShKAS machine guns and one 12.7 mm (0.50 in) UBS machine gun.[2]
The result was a highly conventional aircraft that first flew on schedule on 5 April 1940 at the Khodynka Airport in Moscow with chief test pilot Arkadij Ekatov at the controls. On 24 May the first prototype attained a speed of 648.5 km/h (402.9 mph) at 6,900 m (22,638 ft). It could not, however, attain the speed originally specified by the Air Force with this engine. The second prototype took to the air on 9 May, but the third aircraft, the first to be armed, was forced to wait until 6 June, as problems with its interrupter gear prolonged the ground firing tests. On 5 August 651 km/h (405 mph) was reached at 7,000 m (23,000 ft) using maximum boost. Time to altitude figures were 5.1 minutes to 5,000 m (16,000 ft) and 7.2 minutes to 7,000 m (23,000 ft) and speeds at lower altitudes were 579 km/h (360 mph) at 2,200 m (7,200 ft) and 605 km/h (376 mph) at 3,630 m (11,910 ft).[2]
The I-200 was ordered into production almost immediately, on 31 May 1940.[3] In contrast to the other competing designs, the I-26 (Yak-1) and I-301 (LaGG-3), the I-200 successfully completed the state trials in August on its first attempt, demonstrating 651 km/h at 7000 meters altitude. Time to climb to 5000 meters was 5.3 minutes. But the trials revealed a number of serious defects, including inadequate visibility when taxiing, poor-quality plexiglas in the canopy obscuring the pilot's view, heavy controls, poor longitudinal stability, difficulty in opening canopy, an excessively hot cockpit and a "dangerous propensity to flick from a simple stall into a spin from which it was almost impossible to recover".[4]
A number of improvements were ordered to be made to the aircraft as a result of the deficiencies discovered during the trials, but only a few of them were able to be implemented before production began as the VVS was very anxious to get modern fighters into service. These included an additional oil cooler air intake on the starboard side of the nose, rubber sheaths around the fuel tanks to make them self-sealing, two underwing bomb racks each capable of carrying a 100 kg (220 lb) FAB-100 bomb, a PBP-1 gunsight and each ShKAS was given 375 rounds and the UBS 300 rounds. From the ninth aircraft onwards the side-opening canopy was replaced by a rear-sliding canopy that could be jettisoned in flight. On 9 December 1940 the first 100 I-200s were designated as the MiG-1 (after the initials of Mikoyan and Gurevich).[5]
The improvement process continued throughout the production run, but they weren't immediately implemented on the production line, but were instead incorporated in a fourth prototype for evaluation. This aircraft first flew on 29 October 1940 and was a significant improvement over the I-200s then in production. It passed its State acceptance trials and its improvements were incorporated on the production line from the 101st I-200. These were designated as the MiG-3 on 9 December, although the first production MiG-3 was not completed until 20 December 1940.[6]
Other testing
The I-200 prototypes were used to evaluate a number of proposals. For example the second prototype was fitted with a prototype of the AM-37 engine and first flew with that engine on 6 January 1941. It experienced severe vibration problems and, despite efforts to cure the problems, failed during a flight on 7 May, and was destroyed in the ensuing crash. The third prototype was generally used for armament trials, experimenting with 82 mm (3.2 in) RS-82 rockets among other weapons. For another trial it was equipped with the experimental 23 mm (0.91 in) MP-3 autocannon carried underneath the wings in external pods and redesignated as the IP-201. The 12.7 mm UBS gun was removed for the these tests and the space freed up was used to install an extra fuel tank. Initially the cannon had the low rate of fire of only 300 rounds per minute, but this was soon doubled and the gun was renamed as the MP-6. Installation of the guns was difficult, despite the aircraft's metal outer wing panels, and the wings deformed when the cannon were first mounted. It made its first, and only, flight on 1 December 1940 carrying two MP-6s and two 12.7 mm AP-12.7 machine guns, but a blocked fuel line caused a forced landing before the guns could be fired. But testing on a variety of other aircraft revealed very unsatisfactory performance by the guns and their development was canceled. The designers were arrested on 15 May 1941 and executed on 28 October 1941.[7]
Operational history
On 3 December 1940 the VVS ordered that the 41st Fighter Regiment (isbrebitel'nyy aviatsionnyy polk), based at the Crimean town of Kacha, was to conduct the operational trials for the I-200 and that they were to be transferred to the 146th Fighter Regiment at Yevpatoria, also in the Crimea, for pilot training after the conclusion of the trials. By 22 February 1941 89 had been issued to regular fighter units, notably the 89th Fighter Regiment at Kaunas, Lithuania and the 41st Fighter Regiment at Białystok, Poland, both places under Soviet occupation since 1939–40.[5] On 1 June 1941 they were spread out a bit more, with 31 in the Baltic Military District, 37 in the Western Special Military District, one in the Kiev Military District and eight in the Odessa Military District for a total of 77 on hand, of these only 55 were operational. Furthermore an additional eight were assigned to the Soviet Navy.[8]
Little is known of the performance of the MiG-1 in combat as most were likely destroyed during the opening days of Operation Barbarossa. However, one was still in the inventory of the VVS as late as 1944 when it was recorded as withdrawn that year.[5]
Variants
- Izdeliye-61 : This was the internal OKB designation of the I-200 prototype.
- I-200 : MiG-1 prototype, 3 made.
- MiG-1 : Single-seat interceptor fighter aircraft for the Soviet Air Force.
Operators
Specifications (Mikoyan-Gurevich MiG-1)
General characteristics
- Crew: One
- Length: 8.16 m (26 ft 9 in)
- Wingspan: 10.20 m (33 ft 5 in)
- Height: 2.62 m (8 ft 7 in)
- Wing area: 17.5 m² (188 ft²)
- Airfoil: Clark YH
- Empty weight: 2,602 kg (5,736 lb)
- Loaded weight: 3,099 kg (6,832 lb)
- Max takeoff weight: 3,319 kg (7,317 lb)
- Powerplant: 1× Mikulin AM-35A liquid-cooled V-12, 1,007 kW (1,350 hp)
Performance
- Maximum speed: 657 km/h (410 mph)
- Range: 580 km (362 mi)
- Service ceiling: 12,000 m (39,370 ft)
- Rate of climb: 16.8 m/s (3,306 ft/min)
- Wing loading: 177 kg/m² (36 lb/ft²)
- Power/mass: 0.32 kW/kg (0.20 hp/lb)
Armament
- 1 × 12.7 mm BS machine gun
- 2 × 7.62 mm ShKAS machine guns
- up to 200 kg (440 lb) of bombs
See also
Related development
Comparable aircraft
Related lists List of military aircraft of the Soviet Union and the CIS - List of fighter aircraft
References
Notes
- ↑ Gordon (2008), pp. 95–96
- ↑ 2.0 2.1 Gordon (2008), pp. 96–97
- ↑ Gordon (2008), p. 96
- ↑ Gordon (2008), p. 97
- ↑ 5.0 5.1 5.2 Gordon (2008), p. 98
- ↑ Gordon (2008), pp. 98, 100
- ↑ Gordon (2008), p. 99
- ↑ "Airforce_41.xls". http://www.rkkaww2.armchairgeneral.com/weapons/Airforce_41.xls. Retrieved 2009-09-07.
Bibliography
- Gordon, Yefim and Komissarov, Dmitry. OKB Mikoyan: A History of the Design Bureau and its Aircraft. Hinckley, England: Midland Publishing, 2009. ISBN 1-85780-307-5.
- Gordon, Yefim. Mikoyan's Piston-Engined Fighters (Red Star Volume 13). Earl Shilton, Leicester, UK: Midland Publishing, 2003. ISBN 1-85780-160-1.
- Gordon, Yefim. Soviet Airpower in World War 2. Hinckley, England: Midland Publishing, 2008. ISBN 978-1-85780-304-4.
- Gordon, Yefim and Khazanov, Dmitri. Soviet Combat Aircraft of the Second World War, Volume One: Single-Engined Fighters. Earl Shilton, Leicester, UK: Midland Publishing, 1998. ISBN 1-85780-083-4.
- Green, William. War Planes of the Second World War, Volume Three: Fighters. London: Macdonald & Co., 1961. ISBN 0-356-01447-9.
- Green, William and Swanborough, Gordon. WW2 Aircraft Fact Files: Soviet Air Force Fighters, Part 1. London: Macdonald and Jane's Publishers, 1977. ISBN 0-354-01026-3.
- Gunston, Bill. The Osprey Encyclopaedia of Russian Aircraft 1875–1995. London, Osprey, 1995. ISBN 1-85532-405-9.
- Stapfer, Hans-Heiri. Early MiG Fighters in Action (Aircraft number 204). Carrollton, TX: Squadron/Signal Publications, 2006. ISBN 0-89747-507-0.
- Tessitori, Massimo. Mikoyan Gurevich MiG-1/MiG-3. Sandomierz, Poland/Redbourn, UK: Mushroom Model Publications, 2006. ISBN 83-8945-026-7.
External links
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