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| Název: Name: | IMAM Ro.43 | IMAM Ro.43 |
| Originální název: Original Name: | IMAM Ro.43 | |
| Kategorie: Category: | průzkumný/pozorovací letoun | reconnaissance/scout aeroplane |
| Výrobce: Producer: | DD.11.1934-DD.09.1941 SA Industrie Aeronautiche Romeo, Napoli DD.07.1936-DD.09.1937 SA Costruzioni Meccaniche Aeronautiche, Pisa | |
| Období výroby: Production Period: | DD.MM.1934-DD.MM.1941 | |
| Vyrobeno kusů: Number of Produced: | 194: 149 Romeo 45 CMASA | |
| První vzlet: Maiden Flight: | 19.11.1934 (MM.224) | |
| Osádka: Crew: | 1-2 | |
| 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: | plováky | floats |
| Technické údaje: Technical Data: | ||
| Hmotnost prázdného letounu: Empty Weight: | 1760 kg | 3880 lb |
| Vzletová hmotnost: Take-off Weight: | 2400 kg | 5291 lb |
| Maximální vzletová hmotnost: Maximum Take-off Weight: | ? kg | ? lb |
| Rozpětí: Wingspan: | 11,580 m | 37ft 11,91in |
| Délka: Length: | 9,720 m | 31ft 10,68in |
| Výška: Height: | 3,500 m | 11ft 5,8in |
| Plocha křídla: Wing Area: | 33,36 m2 | 359.08 ft2 |
| Plošné zatížení: Wing Loading: | 71,94 kg/m2 | 14.73 lb/ft2 |
| Pohon: Propulsion: | ||
| Kategorie: Category: | pístový | piston |
| Počet motorů: Number of Engines: | 1 | |
| Typ: Type: | Piaggio P.IX RC.35, vzduchem chlazený hvězdicový devítiválec o výkonu 522 kW (700 k). Vrtule trojlistá kovová. | Piaggio P.IX RC.35, nine-cylinder, air-cooled, radial engine rated 672 hp, driving three blade metal propeller. |
| Objem palivových nádrží: Fuel Tank Capacity: | ? | ? |
| Výkony: Performance: | ||
| Maximální rychlost: Maximum Speed: | 300 km/h v 2000 m | 186.4 mph in 6562 ft |
| Cestovní rychlost: Cruise Speed: | 245 km/h v 1000 m | 152.2 mph in 3281 ft |
| Rychlost stoupání: Climb Rate: | 11.1 m/s | 2178.501 ft/min |
| Čas výstupu na výšku: Time to Climb to: | 11,0 min do 4000 m | 11,0 min to 13123 ft |
| Operační dostup: Service Ceiling: | 6600 m | 21654 ft |
| Dolet: Range: | 800 km | 497.1 mi |
| Maximální dolet: Maximum Range: | 1500 km | 932.1 mi |
| Výzbroj: Armament: | 2x pevný kulomet Breda-SAFAT ráže 7,7 mm nad motorem s 500 náboji pro každý | One fixed forward firing 0.303 Breda-SAFAT machine guns mouted in the nose, 500 rpg |
| Uživatelské státy: User States: | | |
| Poznámka: Note: | Plovákový letoun Ro.43 úzce vycházel průzkumného letoun IMAM Ro.37 a byl dílem i stejného konstruktéra. Byl navržen pro službu na katapultech bitovních lodí a křižníků italského námořnictva (Regia Marina). | Derived from the Ro.37 Lince reconnaissance aircraft, with the same designer. The Ro.43 was designed to meet a requirement of the Regia Marina, for a catapult launched reconnaissance aircraft to equip the Maritime Reconnaissance Squadrons operating from its cruisers and battleships. |
| Zdroje: Sources: | Wiesław Bączkowski, Włoskie samoloty wojskowe 1936 - 1945, Warszawa, 1999, ISBN 83-86776-49-8 L+K 25/1995, Letadla 1939-45 http://it.wikipedia.org/wiki/IMAM_Ro.43 http://www.airwar.ru/enc/sww2/ro43.html www.wwiivehicles.com archiv autora | |
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