Mikojan-Gurevič MiG-1 AM-37

Mikoyan-Gurevich MiG-1 AM-37
Микоян-Гуревич МиГ-1 АМ-37
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Název:
Name: 		Mikojan-Gurevič MiG-1 (motor AM-37) Mikoyan-Gurevich MiG-1 (with engine AM-37)
Originální název:
Original Name: 		Микоян-Гуревич МиГ-1 (c моторoм АМ-37)
Kategorie:
Category: 		stíhací letoun fighter aeroplane
Výrobce:
Producer:		 DD.MM.1940-08.12.1940 Moskevský letecký závod č. 1 Aviachimu, Moskva /
Období výroby:
Production Period: 		DD.09.1940-08.12.1940
Vyrobeno kusů:
Number of Produced: 		1 konverze
První vzlet:
Maiden Flight: 		06.01.1941
Osádka:
Crew: 		1
Základní charakteristika:
Basic Characteristics:		 
Vzlet a přistání:
Take-off and Landing: 		CTOL - konvenční vzlet a přistání CTOL - conventional take-off and landing
Uspořádání křídla:
Arrangement of Wing: 		jednoplošník monoplane
Uspořádání letounu:
Aircraft Concept: 		klasické conventional
Podvozek:
Undercarriage:		 zatahovací retractable
Přistávací zařízení:
Landing Gear:		 kola wheels
Technické údaje:
Technical Data: 		 
Hmotnost prázdného letounu:
Empty Weight: 		2398 kg 5287 lb
Vzletová hmotnost:
Take-off Weight: 		3300 kg 7275 lb
Maximální vzletová hmotnost:
Maximum Take-off Weight: 		? kg ? lb
Rozpětí:
Wingspan: 		10,200 m 33ft 5,56in
Délka:
Length: 		8,155 m 26ft 9,06in
Výška:
Height: 		3,325 m 10ft 10,9in
Plocha křídla:
Wing Area: 		17,44 m2 187.72 ft2
Plošné zatížení:
Wing Loading: 		189,202 kg/m2 38.75 lb/ft2
Pohon:
Propulsion:		 
Kategorie:
Category:		 pístový piston
Počet motorů:
Number of Engines:		 1
Typ:
Type:		 Mikulin AM-37 kapalinou chlazený přeplňovaný vidlicový dvanáctiválec o vzletovém výkonu 1 030 kW (1 400 k) a 1 030 kW (1 400 k) v h= 5 800 m.
Vrtule trojlistá kovová VIŠ-61AP s nastavitelným úhlem náběhu o průměru 3 000 m.		 Mikulin AM-37 twelve-cylinder liquid-cooled supercharged Vee engine rated at 1,381 hp at 2,050 rpm for také-off and 1,381 hp at 19,030 ft,
driving a three-blade VISh-61AP metal variable-pitch propeller of the diameter 9ft 10in.
Objem palivových nádrží:
Fuel Tank Capacity: 		360 l 79.2 UK gallons (92.1 US gallons)
Výkony:
Performance: 		 
Maximální rychlost:
Maximum Speed: 		660 km/h v 5800 m 410.1 mph in 19029 ft
Cestovní rychlost:
Cruise Speed: 		580 km/h v ? m 360.4 mph in ? ft
Rychlost stoupání:
Climb Rate: 		? m/s ? ft/min
Čas výstupu na výšku:
Time to Climb to: 		? min do ? m ? min to ? ft
Operační dostup:
Service Ceiling: 		12000 m 39370 ft
Dolet:
Range: 		? km ? mi
Maximální dolet:
Maximum Range: 		? km ? mi
Výzbroj:
Armament: 		1x pevný kulomet UBK ráže 12,7 mm střílející osou vrtule s 300 náboji a
2x pevný kulomet ŠKAS ráže 7,62 mm v trupu, 375 nábojů pro každý.
Pumový náklad: ?		 One fixed forward-firing 0.5 inch UBK machine-gun mounted in through the shaft and
Two fixed forward-firing 0.3 inch ShKAS machine-guns mounted in the fuselage.
Bomb load: ?
Uživatelské státy:
User States:
Poznámka:
Note: 		- -
Zdroje:
Sources: 		Yefim Gordon and Dmitri Khazanov, 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.
Yefim Gordon and Dmitry Komissarov, OKB Mikoyan, A History of the Design Bureau and its Aircraft, Hinckley, England: Midland Publishing, 2009, ISBN 978-1-85780-307-5.
www.topedge.com
http://www.airwar.ru/enc/fww2/mig1am37.html
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Mikojan-Gurevič MiG-1 AM-37 -


URL : https://www.valka.cz/Mikojan-Gurevic-MiG-1-AM-37-t141258#458063 Version : 0

the MiG-1 with the engine Mikulin AM-37[/heading]

The end of the year has been declared the engine Mikulin AM-37 as eligible for installation in a verification types of aircraft. This engine promised higher performance and single stage and single speed compressor eased off on the výškovosti engine. OKB 155 Mikojana and Gereviče got instructed to the engine zastavěla to your the Mig-1. For installation was selected second prototype (-200.02), the area was not too complex, in addition to the new engine were installed more efficient radiator coolant and engine oil. The entire reconstruction was completed 8. December 1940. The aircraft also received the new propeller you KNOW-61AP.
The first takeoff was performed 6. January of the following year. During the first flight was zještěno that the engine will run rough and at a height of more than 4 000 m experiencing a very strong vibration. The prototype was sent to the motorcycle factory no. 24, which was also the moscow, here motoráři remove the deficiencies, but the tests the aircraft has not been completed, because 7. may the aircraft crashed for an engine failure, the aircraft was destroyed and the work completed. Engine development was terminated after making several dozen engines, because there was the need of engines AM-38.

sources:
Yefim Gordon and Dmitry Komissarov, OKB Mikoyan, And the History of the Design Bureau and its Aircraft, Hinckley, England: Midland Publishing, 2009, ISBN 978-1-85780-307-5.
http://www.airwar.ru/enc/fww2/mig1am37.html
author archive.

URL : https://www.valka.cz/Mikojan-Gurevic-MiG-1-AM-37-t141258#458070 Version : 0
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