| Název: Name: | Tupolev ANT-5 | Tupolev ANT-5 |
| Originální název: Original Name: | Туполев АНТ-5 | |
| Kategorie: Category: | stíhací letoun | fighter aeroplane |
| Výrobce: Producer: | DD.MM.1927-DD.MM.1927 Ústřední aerohydrodynamický institut, Moskva | |
| Období výroby: Production Period: | DD.MM.1927-DD.MM.1927 | |
| Vyrobeno kusů: Number of Produced: | 1 | |
| První vzlet: Maiden Flight: | 10.08.1927 | |
| 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: | dvouplošník | biplane |
| Uspořádání letounu: Aircraft Concept: | klasické | conventional |
| Podvozek: Undercarriage: | pevný | fixed |
| Přistávací zařízení: Landing Gear: | kola | wheels |
| Technické údaje: Technical Data: | ||
| Hmotnost prázdného letounu: Empty Weight: | 921 kg | 2030 lb |
| Vzletová hmotnost: Take-off Weight: | ? kg | ? lb |
| Maximální vzletová hmotnost: Maximum Take-off Weight: | 1343 kg | 2961 lb |
| Rozpětí: Wingspan: | 11,40 m | 37ft 4,81in |
| Délka: Length: | 7,23 m | 23ft 8,64in |
| Výška: Height: | 3,35 m | 10ft 11,88in |
| Plocha křídla: Wing Area: | 23,80 m2 | 256.18 ft2 |
| Plošné zatížení: Wing Loading: | ? kg/m2 | ? lb/ft2 |
| Pohon: Propulsion: | ||
| Kategorie: Category: | pístový | piston |
| Počet motorů: Number of Engines: | 1 | |
| Typ: Type: | Gnome-Rhône Jupiter 9Ad o výkonu 309 kW/420 k dvoulistá dřevěná vrtule | Gnome-Rhône Jupiter 9Ad, power 414 hp two-bladed wooden propeller |
| Objem palivových nádrží: Fuel Tank Capacity: | ? | ? |
| Výkony: Performance: | ||
| Maximální rychlost: Maximum Speed: | 250 km/h v 3500 m | 155.3 mph in 11483 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: | 11,4 min do 5000 m | 11,4 min to 16404 ft |
| Operační dostup: Service Ceiling: | 7200 m | 23622 ft |
| Dolet: Range: | ? km | ? mi |
| Maximální dolet: Maximum Range: | ? km | ? mi |
| Výzbroj: Armament: | 2x kulomet Vickers ráže 7,7 mm | 2x .300 in Vickers machine gun |
| Uživatelské státy: User States: | | |
| Poznámka: Note: | - prototyp I-4 | - |
| Zdroje: Sources: | Gordon, Yefim; Rigmant, Vladimir. OKB Tupolev: A History of the Design Bureau and its Aircraft. Midland Publishing, Hinckley 2005. ISBN 1-85780-214-4. Gunston, Bill. Tupolev Aircrat since 1922. Naval Institute Press, Annapolis 1995. ISBN 1-55750-882-8. Duffy, Paul; Kandalov, Andrej. Tupolev: muž a jeho letadla. Jan Vašut, Praha 1999. ISBN 80-7236-051-5. Andersson, Lennart. Soviet Aircraft and Aviation 1917-1941. Putnam Aeronautical Books, London 1997. ISBN 0-85177-859-3. Green, W.; Swanborough, G. Encyklopedie stíhacích letounů. Svojtka & Co., Praha 2002. ISBN 80-7237-341-2. http://www.tupolev.ru/ant-5-(i-4) | |
Tupolev ANT-5
Туполев АНТ-5
commons.wikimedia.org
http://www.airwar.ru/enc/fww1/i4.html
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