| Název: Name: | Rikugun Ki-93-Ia | Rikugun Ki-93-Ia |
| Originální název: Original Name: | 陆军航空工厂 キ93-I甲试作输送机 | |
| Kategorie: Category: | stíhací letoun | fighter aeroplane |
| Výrobce: Producer: | DD.MM.1945-DD.MM.1945 1st Army Aviation Workshop, Tachikawa | |
| Období výroby: Production Period: | DD.05.1944-DD.08.1945 | |
| Vyrobeno kusů: Number of Produced: | 1 (některé prameny píší o stavbě 12 prototypů) | |
| První vzlet: Maiden Flight: | 08.05.1945 | |
| 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: | 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: | 7686 kg | 16945 lb |
| Vzletová hmotnost: Take-off Weight: | 10525 kg | 23204 lb |
| Maximální vzletová hmotnost: Maximum Take-off Weight: | 11380 kg | 25089 lb |
| Rozpětí: Wingspan: | 19,000 m | 62ft 4,02in |
| Délka: Length: | 14,220 m | 46ft 7,84in |
| Výška: Height: | 4,850 m | 15ft 10,93in |
| Plocha křídla: Wing Area: | 54,75 m2 | 589.322 ft2 |
| Plošné zatížení: Wing Loading: | 192,24 kg/m2 | 39.37 lb/ft2 |
| Pohon: Propulsion: | ||
| Kategorie: Category: | pístový | piston |
| Počet motorů: Number of Engines: | 2 | |
| Typ: Type: | Micubiši Ha-214, vzduchem chlazený dvouhvězdicový osmnáctiválec o vzletovém výkonu 1 765 kW (2 400 k), 1 449 kW (1 970 k) v h= 1 500 m a 1 272 kW (1 730 k) v h= 8 300 m. Vrtule šestilistá kovová VDM s konstantní rychlostí otáček o průměru 3 800 mm. | Mitsubishi Ha-214, eighteen-cylinder air-cooled two-row radial engine rated at 2,367 hp for take-off, 1,943 hp for 4,920 ft and 1,706 hp at 27,230 ft, driving a six-blade VDM metal constant-speed propeller of the diameter 12ft 6in. |
| Objem palivových nádrží: Fuel Tank Capacity: | 2 480 l | 545.5 UK gallons |
| Výkony: Performance: | ||
| Maximální rychlost: Maximum Speed: | 624 km/h v 8300 m | 387.7 mph in 27231 ft |
| Cestovní rychlost: Cruise Speed: | 475 km/h v 6000 m | 217.5 mph in 19685 ft |
| Rychlost stoupání: Climb Rate: | 11,4 m/s | 2244.1 ft/min |
| Čas výstupu na výšku: Time to Climb to: | 9,05 min do 6000 m | 9,05 min to 19685 ft |
| Operační dostup: Service Ceiling: | 12050 m | 39534 ft |
| Dolet: Range: | 2000 km | 1242.7 mi |
| Maximální dolet: Maximum Range: | 3000 km | 1864.1 mi |
| Výzbroj: Armament: | 1x pevný kanón Ho-401 ráže 57 mm v gondole pod trupem, 20 granátů 2x pevný kanón Ho-5 ráže 20,0 mm v kořenech křídel s 200 granáty pro každý a 1x pohyblivý kulomet Ho-103 ráže 12,7 mm v zadní části kabiny se 400 náboji. Pumový náklad: 2x 250 kg nebo přídavné nádrže paliva. | One fixed forward-firing 2.24 inchs Ho-401 cannon in ventral gondola with 20 rounds, two fixed forward-firing 0.79 inch Ho-5 cannons wing roots 200 rpg and one flexible rear-firing 0.5 inch Ho-103 machine-gun mounting in rear cockpit. Bomb load: Up to 1,102 lbs bombs or drop tanks. |
| Uživatelské státy: User States: | - | - |
| Poznámka: Note: | - Výkony jsou pouze vypočtené, letoun nalétal pouze 20 minut. | Japanese Heavy fighter. The performances are only calculated, aircraft flew only 20 minutes. |
| Zdroje: Sources: | René J. Francillon Ph.D., Japanese Aircraft of the Pacific War, Naval Institute Press, Annapolis Maryland, Reprinted 1990, ISBN-0-87021-313-X Famous Airplanes of the World, Army Experimental Fighters, No.24, Bunrin-Do Co. Ltd., Nakano Koku, Japan, ISBN4-89319-021-0 L+K 13/1977, Václav Němeček, Letadla 1939 – 45, Rikugun Ki-93 http://www.samoloty.ow.pl/str089.htm archiv autora | |
Rikugun Ki 93-Ia
Rikugun Ki-93-Ia / 陆军航空工厂 キ93-I甲试作输送机
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