| General Information | ||
|---|---|---|
| Type | ITP (M-1) | ITP (M-2) |
| Function | Fighter prototype | |
| Year | 1942 | 1943 |
| Crew | 1 | 1 |
| Powerplant | ||
| Type |
VK-107P VK-107A |
AM-37 AM-39A |
| Takeoff Power | 1650hp | 1400hp 1700hp |
| Size | ||
| Length | 8.9m | 9.2m |
| Height | ?m | ?m |
| Wingspan | 10.0m | 10.0m |
| Wing area | 16.5m2 | 16.5m2 |
| Data below is for VK-107P and AM-39A variants | ||
| Weights and loads | ||
| Empty | 2960kg | 2910kg |
| Loaded | 3570kg | 3570kg |
| Wing Load (kg/m2) | 217 | 217 |
| Power load (kg/hp) | 2.1 | 2.1 |
| Speed | ||
| at 0m | 568km/h | 540km/h |
| at 6300m | 655km/h | n/a |
| at 2500m | n/a | 650km/h |
| Landing | 130km/h | 140km/h |
| Maneuverability | ||
| Turn time | ?sec | ?sec |
| Roll | ||
| Landing | 375m | 390m |
| Takeoff | 350m | 326m |
| Range | ||
| Practical | 1280km | 980km |
| Ceiling | ||
| Ceiling | 10400m | 11500m |
| Climb | ||
| 5000m | 5.9min | 6.0min |
| Payload | ||
| Fuel+Oil | 517+30kg | 440+50kg |
| Gun Type | Ammo (Position) | |
| 37mm Sh-37 | 1*40 (engine) | - |
| 20mm ShVAK | 2*200 (engine) | 3*? (engine) |
| Salvo (kg/sec) | 3.84 | |
| Bombs | 4*100kg | |
| or Rockets | 8*RS-82 | |
During the Great Patriotic War N.N.Polikarpov made an effort to design a fighter with performance even with best contemporary machines, but with superior firepower. He chose liquid-cooling engines of new design from both V.Ya.Klimov and A.A.Mikulin, promising high power output.
Airframe of the ITP was similar to I-185. Wooden monocoque fuselage made of multi-layer birch ply was combined with duralumin wing (main spar had steel shelves), controls - with fabric cover. Oil cooler located in 'chin' position. Water cooler - in the wing, with intakes on the leading edge. Heavy Sh-37 cannon fired through the propeller hub, pair of synchronized ShVAK cannons were also housed under the engine cowling.
Jean Alexander notices 'strange reminiscence' between the ITP and Mikoyan-Gurevich MiG-1/MiG-3. Actually this is not a surprise, because both designs are rooted in the N.N.Polikarpov 'Kh' (Cyrillic 'X') project of high-altitude interceptor.
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First variant (M-1) was assembled in October 1941 and was flown first time on February 23, 1942. In 1942 VK-107P engine was replaced with VK-107A.
Performance was promising, but toothing problems of both engines forced N.N.Polikarpov to abandon VK-107P/A and build another variant with different engine and armament.
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A.A.Mikulin AM-37 and AM-39A engines were fitted on the M-2 variant. Those engines had no provision for the hub-mounted guns, and weapon was reduced to three synchronized ShVAK cannons.
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Aircraft was built in late 1942, but flew first time only on November 23, 1943. Factory trials continued until June 1944. Abandoned after N.N.Polikarpov death, because A.S.Yakovlev had already adapted the Yak-9 to carry the 37mm cannon.
| Predecessors | Modifications | |
|---|---|---|
|
I-185 |
'Kh' (Cyrillic 'X') project | None |
| References | Links |
|---|---|
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| Created January 25, 1996 Modified May 2, 2000 |
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