| Název: Name: | Mikojan-Gurevič Je-152A | Mikoyan-Gurevich Ye-152A |
| Originální název: Original Name: | Микоян-Гуревич Е-152А | |
| Kategorie: Category: | stíhací letoun | fighter aeroplane |
| Výrobce: Producer: | DD.MM.1959-DD.MM.1959 Moskevský letecký závod č. 155, Moskva | |
| Období výroby: Production Period: | DD.MM.1959-DD.MM.1959 | |
| Vyrobeno kusů: Number of Produced: | 1 | |
| První vzlet: Maiden Flight: | 10.07.1959 | |
| 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: | 8740 kg | 19268 lb |
| Vzletová hmotnost: Take-off Weight: | 12500 kg | 27558 lb |
| Maximální vzletová hmotnost: Maximum Take-off Weight: | 13960 kg | 30777 lb |
| Rozpětí: Wingspan: | 8,49 m | 27ft 10,25in |
| Délka: Length: | 19,00 m | 62ft 4,02in |
| Výška: Height: | ? m | ? |
| Plocha křídla: Wing Area: | 34,02 m2 | 366.19 ft2 |
| Plošné zatížení: Wing Loading: | ? kg/m2 | ? lb/ft2 |
| Pohon: Propulsion: | ||
| Kategorie: Category: | jednoproudový | turbojet |
| Počet motorů: Number of Engines: | 2 | |
| Typ: Type: | Tumanskij R-11F-300 o tahu 37,27 kN / 56,29 kN s přídavným spalováním | Tumansky R-11F-300, thrust 8378 lb / 12655 lb with afterburner |
| Objem palivových nádrží: Fuel Tank Capacity: | 4400 l 1x 600 l nebo 1500 l přídavná nádrž | 968 Imp gal / 1162 US gal 1x 132 or 330 Imp gal / (159 or 396 US gal) drop tank |
| Výkony: Performance: | ||
| Maximální rychlost: Maximum Speed: | 2135 km/h v 13700 m | 1326.6 mph in 44948 ft |
| Cestovní rychlost: Cruise Speed: | ? km/h v ? m | ? mph in ? ft |
| Rychlost stoupání: Climb Rate: | ? m/s | ? ft/min |
| Čas výstupu na výšku: Time to Climb to: | 7,64 min do 20000 m | 7,64 min to 65617 ft |
| Operační dostup: Service Ceiling: | 19800 m | 64961 ft |
| Dolet: Range: | ? km | ? mi |
| Maximální dolet: Maximum Range: | ? km | ? mi |
| Výzbroj: Armament: | 2x K-9 | 2x K-9 |
| Uživatelské státy: User States: | - | - |
| Poznámka: Note: | - | - |
| Zdroje: Sources: | Якубович, Николай. Боевые самолеты Микояна: Есть только МИГ... Яуза, Москва 2009. ISBN 978-5-699-34100-9. Gordon, Yefim; Guston, Bill. Soviet X-Planes. Midland Publishing, Leicester 2000. ISBN 1-85780-099-0. Guston, Bill; Gordon, Yefim. MiG Aircraft since 1937. Putnam Aeronautical Books, London 1998. ISBN 0-85177-884-4. ruslet.webnode.cz | |
Mikojan-Gurevič Je-152A [kód NATO: Flipper]
Mikoyan-Gurevich Ye-152A
Микоян-Гуревич Е-152А
http://www.airwar.ru/enc/xplane/e152a.html
.![Mikojan-Gurevič Je-152A [kód NATO: Flipper] -](/attachments/217/e152a-2.jpg)
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| Type | Mikojan-Gurevič Je-152A [kód NATO: Flipper] |
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![Mikojan-Gurevič Je-152A [kód NATO: Flipper] -](/attachments/217/e152a-3.jpg)
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| Type | Mikojan-Gurevič Je-152A [kód NATO: Flipper] |
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![Mikojan-Gurevič Je-152A [kód NATO: Flipper] -](/attachments/217/e152a-1.jpg)
| Period | - |
| Producer | - |
| Type | Mikojan-Gurevič Je-152A [kód NATO: Flipper] |
| Camouflage | - |
| Country | - |
| Pilot | - |
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| Date (DD.MM.RRRR) | DD.MM.RRRR |
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| Published with authors permit | - |
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Reklama
The heavy fighter Je-152A Flipper was first seen by the West in Tushin in 1961, based on the Je-150, which was a heavy fighter based on the MiG-21. The Je-152A had two Tumanskii R-11F jet engines, in addition to being equipped with K-9 missiles under the wings. The installation of the R-11F engines was merely a failsafe in case of problems with the R-15 engines powering the Je-150 and Je-152. The top speed was Mach 2.51. It remained only in prototype form, apparently mainly due to the development of the more promising Je-155P, the later MiG-25.
Source:
www.aviation.ru
Source:
www.aviation.ru
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