| Název: Name: | Iljušin Il-54 | Ilyushin Il-54 |
| Originální název: Original Name: | Ильюшин Ил-54 | |
| Kategorie: Category: | bombardovací letoun | bomber aeroplane |
| Výrobce: Producer: | DD.MM.1954-DD.MM.1956 Moskevský letecký závod č. 240, Moskva | |
| Období výroby: Production Period: | DD.MM.1954-DD.MM.1956 | |
| Vyrobeno kusů: Number of Produced: | 2 | |
| První vzlet: Maiden Flight: | 03.04.1954 | |
| Osádka: Crew: | 3 | |
| 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: | 26505 kg | 58434 lb |
| Vzletová hmotnost: Take-off Weight: | 40400 kg | 89067 lb |
| Maximální vzletová hmotnost: Maximum Take-off Weight: | 41600 kg | 91712 lb |
| Rozpětí: Wingspan: | 17,65 m | 57ft 10,87in |
| Délka: Length: | 28,96 m | 95ft 0,16in |
| Výška: Height: | 7,90 m | 25ft 11,01in |
| Plocha křídla: Wing Area: | 84,60 m2 | 910.63 ft2 |
| Plošné zatížení: Wing Loading: | ? kg/m2 | ? lb/ft2 |
| Pohon: Propulsion: | ||
| Kategorie: Category: | jednoproudový | turbojet |
| Počet motorů: Number of Engines: | 2 | |
| Typ: Type: | 1. prototyp: Ljulka AL-7 o maximálním tahu 75,51 kN 2. prototyp: Ljulka AL-7F o maximálním tahu 98,07 kN | 1st prototype: Lyulka AL-7, maximum thrust 16976 lb 2nd prototype: Lyulka AL-7F, maximum thrust 22046 lb |
| Objem palivových nádrží: Fuel Tank Capacity: | ? | ? |
| Výkony: Performance: | ||
| Maximální rychlost: Maximum Speed: | 11501) km/h v 5000 m | 714.6 1) mph in 16404 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: | 4 min do 5000 m | 4 min to 16404 ft |
| Operační dostup: Service Ceiling: | 13600 m | 44619 ft |
| Dolet: Range: | 2057 km | 1278.2 mi |
| Maximální dolet: Maximum Range: | 2312 km | 1436.6 mi |
| Výzbroj: Armament: | 1x kanon AM-23 ráže 23 mm v přídi 2x kanon AM-23 ráže 23 mm v ocasním střelišti DK-35 3000-5000 kg pum | 1x 23 mm AM-23 cannon in the nose 2x 23 mm AM-23 cannon in the DK-35 tail turret 6614-11023 lb of bombs |
| Uživatelské státy: User States: | - | - |
| Poznámka: Note: | 1) 1250 kmh druhý prototyp | 1) second prototype 776.7 mph |
| Zdroje: Sources: | Gordon, Y.; Komissarov, D.; Komissarov, S. OKB Ilyushin: A History of the Design Bureau and its Aircraft. Midland Publishing, Hinckley 2004. ISBN 1-85780-187-3. Егоров, Ю. А. Самолеты ОКБ С.В.Ильюшина. Русавиа, Москва 2003. ISBN 5-900078-20-5. Якубович, Николай. Самолеты Ильюшина: Лучшие из лучших. ЯУЗА, Москва 2009. ISBN 987-5-699-33921-1. V.Němeček, Vojenská letadla 1 - 5, Naše vojsko 1990, ISBN 80-206-0114-7 (soubor) V.Němeček, Sovětská letadla, Naše vojsko 1969, 28-082-68 encyklopedie.seznam.cz http://www.aviastar.org/air/russia/il-54.php http://www.airwar.ru/enc/bomber/il54.html | |
Iljušin Il-54 [kód NATO: Blowlamp]
Ilyushin Il-54
Ильюшин Ил-54
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(Фронтовой бомбардировщик)
Zdroj : http://www.aviastar.org/pictures/russia/il-54.gif
![Iljušin Il-54 [kód NATO: Blowlamp] -](/attachments/11501/01_Il_54_01.JPG)
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Reklama
This post has not been translated to English yet. Please use the TRANSLATE button above to see machine translation of this post.
(Фронтовой бомбардировщик)
![Iljušin Il-54 [kód NATO: Blowlamp] -](/files/ilju_in_il-54_118.jpg)
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http://aviadejavu.ru/Site/Crafts/Craft30900.htm
.![Iljušin Il-54 [kód NATO: Blowlamp] -](/attachments/217/1463508401_18-1.jpg)
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