| Název: Name: | Mil Mi-1MU | Mil Mi-1MU |
| Originální název: Original Name: | Миль Ми-1МУ | |
| Kategorie: Category: | bitevní vrtulník | attack helicopter |
| Výrobce: Producer: | DD.MM.1958-DD.MM.196R Moskevský vrtulníkový závod, Ljubercy | |
| Období výroby: Production Period: | DD.MM.1958-DD.MM.196R | |
| Vyrobeno kusů: Number of Produced: | 3 konverze | |
| První vzlet: Maiden Flight: | DD.MM.RRRR | |
| Osádka: Crew: | 2 | |
| Základní charakteristika: Basic Characteristics: | ||
| Uspořádání rotorů: Rotor Configuration: | hlavní a vyrovnávací rotor | main and antitorque rotor |
| Podvozek: Undercarriage: | pevný | fixed |
| Přistávací zařízení: Landing Gear: | kola | wheels |
| Technické údaje: Technical Data: | ||
| Hmotnost prázdného vrtulníku: Empty Weight: | 2092 kg | 4612 lb |
| Vzletová hmotnost: Take-off Weight: | 2550 kg | 5622 lb |
| Maximální vzletová hmotnost: Maximum Take-off Weight: | 2650 kg | 5842 lb |
| Délka s otáčejícími se rotory: Length with Rotors Turning: | 17,03 m | 55 ft 10 ½ in |
| Délka trupu: Fuselage Length: | 12,01 m | 39 ft 4 ⅞ in |
| Šířka trupu: Fuselage Width: | ? m | ? |
| Celková výška: Overall Height: | 3,30 m | 10 ft 9 ⅞ in |
| Průměr hlavního rotoru: Main Rotor Diameter: | 14,50 m | 47 ft 6 ⅞ in |
| Průměr vyrovnávacího rotoru: Tail Rotor Diameter: | 2,50 m | 8 ft 2 ⅜ in |
| Plocha disku hlavního rotoru: Main Rotor Disc Area: | 165,13 m2 | 1777.44 ft2 |
| Plocha disku vyrovnávacího rotoru: Tail Rotor Disc Area: | 4,91 m2 | 52.85 ft2 |
| Pohon: Propulsion: | ||
| Kategorie: Category: | pístový | piston |
| Počet motorů: Number of engines: | 1 | |
| Typ: Type: | Ivčenko AI-26V o výkonu 423 kW/575 k nebo Ivčenko AI-26VF o výkonu 452 kW/615 k | Ivchenko AI-26V, power 567 hp or Ivchenko AI-26VF, power 607 hp |
| Objem palivových nádrží: Fuel Tank Capacity: | 240 l | 52.8 Imp gal / 63.4 US gal |
| Výkony: Performance: | ||
| Maximální rychlost: Maximum Speed: | 160 km/h v 0 m | 99 mph in 0 ft |
| Cestovní rychlost: Cruise Speed: | 135 km/h v ? m | 84 mph in ? ft |
| Rychlost stoupání: Climb Rate: | ? m/s | ? ft/min |
| Statický dostup: Static Ceiling: | ? m | ? ft |
| Dynamický dostup: Dynamic Ceiling: | 3000 m | 9843 ft |
| Dolet: Range: | 165 km | 103 mi |
| Maximální dolet: Maximum Range: | ? km | ? mi |
| Přepravní kapacita: Transport Capacity: | - | - |
| Výzbroj a vybavení: Armament and Equipment: | ||
| Výzbroj: Armament: | 1.: 12x neřízená raketa TRS-132 2.: 3x protitanková raketa 3M11 Falanga 3.: 6x protitanková raketa 9K11 Maljutka | 1st: TRS-132 unguided rocket 2nd: 4x 3M11 Falanga (AT-2 Swatter) anti-tank rocket 3rd: 6x 9K11 Malyutka (AT-3 Sagger) anti-tank rocket |
| Vybavení: Equipment: | - | - |
| Uživatelské státy: User States: | - | - |
| Poznámka: Note: | - konverze Mi-1MU pro přímou palebnou podporu - přestože podoba se systémem Falanga byla doporučena pro přijetí do výzbroje, vedení armády o bitevní vrtulníky neprojevilo zájem - data platí pro druhý prototyp | - |
| Zdroje: Sources: | Михеев, В. Р. Московский вертолётный завод имени М. Л. Миля. Москва 2007. ISBN 5-98734-003-9. Хаустов, Андрей В. Большая карьера малечкого вертолета. Авиация и Время 1998/04. Soukup, Oldřich. Mil Mi-1, L+K 1981/16-17. ruslet.webnode.cz | |
Mil Mi-1MU (bitevní)
Mil Mi-1MU (attack)
Mil Mi-1MU (bitevný)
Миль Ми-1МУ (ударной)
http://www.aviastar.org/helicopters_eng/mi-1.php
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| Type | Mil Mi-1MU (bitevní) |
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| Date (DD.MM.RRRR) | DD.MM.RRRR |
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První prototyp, s raketami
TRS-132.
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| Type | Mil Mi-1MU (bitevní) |
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Kulomet RPK v kabině.
Reklama
http://www.aviastar.org/helicopters_eng/mi-1.php
topwar.ru
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| Producer | - |
| Type | Mil Mi-1MU (bitevní) |
| Camouflage | - |
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| Serial No. / Evidence No. | - |
| Tactical Marking / Imatriculation | - |
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| Date (DD.MM.RRRR) | DD.MM.RRRR |
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| Author Website | - |
Druhý prototyp, s raketami
Falanga.
| Period | - |
| Producer | - |
| Type | Mil Mi-1MU (bitevní) |
| Camouflage | - |
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| Tactical Marking / Imatriculation | - |
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| Date (DD.MM.RRRR) | DD.MM.RRRR |
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| Author Website | - |
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| Type | Mil Mi-1MU (bitevní) |
| Camouflage | - |
| Country | - |
| Pilot | - |
| Production No. | - |
| Serial No. / Evidence No. | - |
| Tactical Marking / Imatriculation | - |
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| Date (DD.MM.RRRR) | DD.MM.RRRR |
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| Author Website | - |
Odlišný způsob uchycení odpalovacích lišt.
www.aviastar.org
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| Period | - |
| Producer | - |
| Type | Mil Mi-1MU (bitevní) |
| Camouflage | - |
| Country | - |
| Pilot | - |
| Production No. | - |
| Serial No. / Evidence No. | - |
| Tactical Marking / Imatriculation | - |
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| Date (DD.MM.RRRR) | DD.MM.RRRR |
| Author | - |
| Print size / 300 DPI | - |
| Published with authors permit | - |
| Author Website | - |
Třetí prototyp, s raketami
Maljutka.
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