| Název: Name: | Suchoj Su-15 | Sukhoi Su-15 |
| Originální název: Original Name: | Сухой Су-15 | |
| Kategorie: Category: | stíhací letoun | fighter aeroplane |
| Výrobce: Producer: | DD.MM.1948-DD.MM.1948 Moskevský letecký závod č. 134, Moskva | |
| Období výroby: Production Period: | DD.MM.1948-DD.MM.1948 | |
| Vyrobeno kusů: Number of Produced: | 2 | |
| První vzlet: Maiden Flight: | 11.01.1949 | |
| 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: | 7409 kg | 16334 lb |
| Vzletová hmotnost: Take-off Weight: | ? kg | ? lb |
| Maximální vzletová hmotnost: Maximum Take-off Weight: | 10437 kg | 23010 lb |
| Rozpětí: Wingspan: | 12,87 m | 42ft 2,68in |
| Délka: Length: | 15,44 m | 50ft 7,87in |
| Výška: Height: | ? m | ? |
| Plocha křídla: Wing Area: | 36,00 m2 | 387.5 ft2 |
| Plošné zatížení: Wing Loading: | 59,40 kg/m2 | 12.17 lb/ft2 |
| Pohon: Propulsion: | ||
| Kategorie: Category: | jednoproudový | turbojet |
| Počet motorů: Number of Engines: | 2 | |
| Typ: Type: | Klimov RD-45F o tahu 22,26 kN | Klimov RD-45F, thrust 5005 lb |
| Objem palivových nádrží: Fuel Tank Capacity: | 2875 l | 632 Imp gal / 759 US gal |
| Výkony: Performance: | ||
| Maximální rychlost: Maximum Speed: | 1045 km/h v 5000 m | 649.3 mph in 16404 ft |
| Cestovní rychlost: Cruise Speed: | ? km/h v ? m | ? mph in ? ft |
| Rychlost stoupání: Climb Rate: | 33,3 m/s | 6555.1 ft/min |
| Čas výstupu na výšku: Time to Climb to: | 2,5 min do 5000 m | 2,5 min to 16404 ft |
| Operační dostup: Service Ceiling: | 15000 m | 49213 ft |
| Dolet: Range: | ? km | ? mi |
| Maximální dolet: Maximum Range: | 1208 km | 750.6 mi |
| Výzbroj: Armament: | 2x kanon N-37 ráže 37 mm, 110 nábojů každý | 2x 37 mm N-37 cannon, 110 rounds each |
| Uživatelské státy: User States: | - | - |
| Poznámka: Note: | - havárie letového prototypu Su-15 3. 6. 1949 byla důvodem ke zrušení Suchojovy OKB | - |
| Zdroje: Sources: | Antonov, Vladimir; Gordon, Yefim et al. OKB Sukhoi: A History of the Design Bureau and its Aircraft. Midland Publishing, Hinckley 1996. ISBN 1-85780-012-5. Якубович, Николай. Все авиашедевры Сухого – от Су-2 до Су-27 и Т-50. Яуза, Москва 2015. ISBN 978-5-699-78965-8. ruslet.webnode.cz | |
Suchoj Su-15 (1948)
Sukhoi Su-15 / Сухой Су-15
http://www.airwar.ru/enc/fighter/su15_1.html
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| Date (DD.MM.RRRR) | DD.MM.RRRR |
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