| Název: Name: | Vought O2U-1 Corsair | Vought O2U-1 Corsair |
| Originální název: Original Name: | Vought O2U-1 Corsair | |
| Kategorie: Category: | průzkumný/pozorovací letoun | reconnaissance/scout aeroplane |
| Výrobce: Producer: | DD.MM.1926-DD.MM.193R Chance Vought Corp., Long Island City, New York | |
| Období výroby: Production Period: | DD.MM.1926-DD.MM.193R | |
| Vyrobeno kusů: Number of Produced: | O2U-1: 137 O2U-1A: 4 O2U-1D: 20-32 O2U-1P: 3 | |
| První vzlet: Maiden Flight: | DD.MM.RRRR | |
| Osádka: Crew: | 2 | |
| 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: | 1062 kg | 2342 lb |
| Vzletová hmotnost: Take-off Weight: | ? kg | ? lb |
| Maximální vzletová hmotnost: Maximum Take-off Weight: | 1649 kg | 3635 lb |
| Rozpětí: Wingspan: | 10.52 m | 34 ft 6 in |
| Délka: Length: | 7.46 m | 24 ft 5 ¾ in |
| Výška: Height: | 3.08 m | 10 ft 1 ¼ in |
| Plocha křídla: Wing Area: | 29.73 m2 | 320 ft2 |
| Plošné zatížení: Wing Loading: | ? kg/m2 | ? lb/ft2 |
| Pohon: Propulsion: | ||
| Kategorie: Category: | pístový | piston |
| Počet motorů: Number of Engines: | 1 | |
| Typ: Type: | Pratt & Whitney R-1340-88 Wasp o výkonu 336 W dvoulistá na zemi stavitelná vrtule Hamilton Standard | Pratt & Whitney R-1340-88 Wasp, power 450 hp two-bladed ground-adjustable propeller Hamilton Standard |
| Objem palivových nádrží: Fuel Tank Capacity: | 341 l | 90 US gal |
| Výkony: Performance: | ||
| Maximální rychlost: Maximum Speed: | 241.4 km/h v 0 m | 150 mph in 0 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: | 3,6 min do 1524 m | 3,6 min to 5000 ft |
| Operační dostup: Service Ceiling: | 5700 m | 18700 ft |
| Dolet: Range: | 978.5 km | 608 mi |
| Maximální dolet: Maximum Range: | ? km | ? mi |
| Výzbroj: Armament: | 1x pevný kulomet Browning ráže 7,62 mm 1-2x pohyblivý kulomet Browning ráže 7,62 mm lehké bomby | 1x .30 in Browning machine gun 1-2x flexible .30 in Browning machine gun light bombs |
| Uživatelské státy: User States: | | |
| Poznámka: Note: | - | - |
| Zdroje: Sources: | Swanborough, F. G., Bowers, P. M. US Navy Aircraft Since 1912. Putnam Aeronautical Books, London 1990. ISBN 0-85177-838-0. Johnson, E. R. United States Naval Aviation, 1919-1941. McFarland, Jefferson 2011. ISBN 978-0-7864-4550-9. Moran, Gerard P. The Corsair, and other - aeroplanes Vought 1917-1977. Sunshine House, Terre Haute 1991. ISBN 0-911852-83-2. www.voughtaircraft.com | |
Vought O2U-1 Corsair
http://www.airwar.ru/enc/sww2/o2u.html
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Reklama
http://www.airwar.ru/enc/sww2/o2u.html
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commons.wikimedia.org
baike.baidu.com BA/16213459/0/6d81800a19d8bc3e631ce1f98b8ba61ea8d345e9? Fr = lemma & ct = single # aid = 0 & pic = 6d81800a19d8bc3e631ce1f98b8ba61ea8d345e9
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"Lenin", první letadlo čínských komunistů. Získáno v únoru 1930, kdy s ním pilot Lung Wen-kuang nouzově přistál v komunisty ovládané části Che-nanu a poté se rozhodl přidat na jejich stranu.
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Stav z roku 1951.
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