| Název: Name: | Kawasaki Ki-60.01 | Kawasaki Ki-60.01 |
| Originální název: Original Name: | キ60试作战斗机 | |
| Kategorie: Category: | stíhací letoun | fighter aeroplane |
| Výrobce: Producer: | DD.MM.1941-DD.03.1941 Kawasaki Aircraft, Ltd., Kakamigahara | |
| Období výroby: Production Period: | DD.MM.1941-DD.03.1941 | |
| Vyrobeno kusů: Number of Produced: | 1. z celkem 3 prototypů / first prototype of the three completed | |
| První vzlet: Maiden Flight: | DD.03.1941 | |
| 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: | 2290 kg | 5049 lb |
| Vzletová hmotnost: Take-off Weight: | 2890 kg | 6371 lb |
| Maximální vzletová hmotnost: Maximum Take-off Weight: | ? kg | ? lb |
| Rozpětí: Wingspan: | 9,780 m | 32ft 1,04in |
| Délka: Length: | 8,400 m | 27ft 6,7in |
| Výška: Height: | 2,750 m | 9ft 0,26in |
| Plocha křídla: Wing Area: | 15.90 m2 | 171.146 ft2 |
| Plošné zatížení: Wing Loading: | 181,76 kg/m2 | 37.23 lb/ft2 |
| Pohon: Propulsion: | ||
| Kategorie: Category: | pístový | piston |
| Počet motorů: Number of Engines: | 1 | |
| Typ: Type: | Daimler-Benz DB 601A o vzletovém výkonu 857 kW; v h= 4 000 m výkon 820 kW Vrtule: trojlistá stavitelná s konstantní rychlostí otáček o průměru 3 000 mm. | Daimler-Benz DB 601A rated 1,150 hp at take-off and 1,100 hp at 13,123 ft, driving a three-blade constant-speed metal propeller of 9 ft 10.11 in diameter. |
| Objem palivových nádrží: Fuel Tank Capacity: | 410 l | 90,2 UK gallons |
| Výkony: Performance: | ||
| Maximální rychlost: Maximum Speed: | 548 km/h v 4000 m | 340.5 mph in 13123 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: | 8,0 min do 5000 m | 8,0 min to 16404 ft |
| Operační dostup: Service Ceiling: | 9780 m | 32087 ft |
| Dolet: Range: | 980 km | 608.9 mi |
| Maximální dolet: Maximum Range: | ? km | ? mi |
| Výzbroj: Armament: | 2x pevný kulomet Ho-103 ráže 12,7 mm nad motorem a 2x pevný kanón Mauser MG 151/20 ráže 20 mm v křídlech | Two fixed forward-firing 0,50 in Ho-103 machine-guns in the fuselage and two fixed forward-firing 0,79 in Mauser MG 151/20 in the wings. |
| Uživatelské státy: User States: | - | - |
| Poznámka: Note: | TTD se vztahují k prvnímu prototypu. | The data are valid for the first prototype |
| Zdroje: Sources: | Rene J. Francillon Ph.D., Japanese Aircraft of the Pacific War, Naval Institute Press, Annapolis, Maryland, USA; rok 1995; ISBN-13: 978-0870213137 Rene J. Francillon, Profile Publications, Kawasaki Ki-61 Hein, Aircraft Profile No.118, 1969 Václav Němeček, Vojenská letadla 3. Naše vojsko, Praha rok 1992, 3. doplněné vydání, ISBN 80-206-0117-1 Famous Aircraft of the World. Army Experimental Fighters, Bunrin-Do., Japan, ISBN4-89319-021-0 Tadeusz Januszewski a Adam Jarski, Kawasaki Ki-61 Hien, Monografie Lotnicze 5. Gdańsk, Poland: AJ-Press, 1992. ISSN 0867-7867. http://www.airwar.ru/enc/fww2/ki60.html archiv autora | |
Kawasaki Ki 60.01
Kawasaki Ki-60.01 / 川崎 キ60・试作战斗机
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