| Název: Name: | Micubiši Ki 1-II / typ 93-2 | Mitsubishi Ki-1-II / Type 93-2 |
| Originální název: Original Name: | キ1九三式重爆击机 | |
| Kategorie: Category: | bombardovací letoun | bomber aeroplane |
| Výrobce: Producer: | DD.MM.1935-DD.MM.1936 Mitsubishi Heavy Industries, Ltd., Nagoya | |
| Období výroby: Production Period: | DD.MM.1935-DD.MM.1936 | |
| Vyrobeno kusů: Number of Produced: | 48 | |
| První vzlet: Maiden Flight: | DD.MM.RRRR | |
| Osádka: Crew: | 4 | |
| 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: | pevný | fixed |
| Přistávací zařízení: Landing Gear: | kola | wheels |
| Technické údaje: Technical Data: | ||
| Hmotnost prázdného letounu: Empty Weight: | 4840 kg | 10670 lb |
| Vzletová hmotnost: Take-off Weight: | 8050 kg | 17747 lb |
| Maximální vzletová hmotnost: Maximum Take-off Weight: | ? kg | ? lb |
| Rozpětí: Wingspan: | 26,500 m | 86ft 11,25in |
| Délka: Length: | 14,800 m | 48ft 6,5in |
| Výška: Height: | 4.920 m | 16ft 1,68in |
| Plocha křídla: Wing Area: | 90,74 m2 | 976.72 ft2 |
| Plošné zatížení: Wing Loading: | 88,72 kg/m2 | 18.17 lb/ft2 |
| Pohon: Propulsion: | ||
| Kategorie: Category: | pístový | piston |
| Počet motorů: Number of engines: | 2 | |
| Typ: Type: | Mitsubishi Ha-2-3 o výkonu 723 kW (970 k) Vrtule: dřevěné dvoulisté | Mitsubishi Ha-2-3 power 957 hp at take-off Two-blade wooden propeller |
| Objem palivových nádrží: Fuel Tank Capacity: | ? | ? |
| Výkony: Performance: | ||
| Maximální rychlost: Maximum Speed: | 230 km/h v ? m | 142.9 mph in ? ft |
| Cestovní rychlost: Cruise Speed: | 195 km/h v 1500 m | 121.2 mph in 4921 ft |
| Rychlost stoupání: Climb Rate: | ? m/s | ? ft/min |
| Čas výstupu na výšku: Time to Climb to: | 14,0 min do 3000 m | 14,0 min to 9843 ft |
| Operační dostup: Service Ceiling: | 8500 m | 27887 ft |
| Dolet: Range: | 1100 km | 683.5 mi |
| Maximální dolet: Maximum Range: | ? km | ? mi |
| Výzbroj: Armament: | 3x pohyblivý kulomet Type 89 ráže 7,7 mm Pumy: 1 000-1 500 kg | 3x 0.303 in machine guns Bomb-load: 3,307 lb maximum |
| Uživatelské státy: User States: | Japonsko (armádní letectvo) | Japan (Imperial Japanese Army Air Service) |
| Poznámka: Note: | Armádní bombardér typ 93-2 | Modified version of Junkers K-37 bomber Army Type 93-2 Heavy Bomber |
| Zdroje: Sources: | Japanese Aircraft 1910-1941 by Robert C. Robert C. Mikesh a Shorzoe Abe, Japanese Aircraft 1910-1941, Naval Institute Press, Annapolis, rok 1990, ISBN: 1557505632 Václav Němeček, Vojenská letadla 2 díl, Naše Vojsko, Praha 1987; ISBN 80-206-0117-1 http://www.airwar.ru/enc/bww1/ki1.html http://www.cofe.ru/avia/M/M-144.htm archiv autora | |
Micubiši Ki 1-II
Mitsubishi Ki-1-II / キ1 九三式重爆击机
Mitsubishi Ki-1-II
キ1九三式重爆击机
Development:
Heavy bomber Mitsubishi Ki-1-I was at the flying personnel popular and so the designers tried to improve its flight characteristics. 71-made aircraft was modified into the form of a new version marked with Ki-1-II, or also the "army heavy bomber Type 92 - 2". Version type the type of the engine have now been used japanese engines Ha-2-II the performance of the engine was lower, but on the other hand managed to slightly improve aerodynamics, leading edges of the wings was used to smooth duralumin sheet (before corrugated) and before the bomb bay doors were installed aerodynamic covers. The main distinguishing feature was a faired landing gear. The performance then was slightly better, but the popularity has remained small..
キ1九三式重爆击机
Development:
Heavy bomber Mitsubishi Ki-1-I was at the flying personnel popular and so the designers tried to improve its flight characteristics. 71-made aircraft was modified into the form of a new version marked with Ki-1-II, or also the "army heavy bomber Type 92 - 2". Version type the type of the engine have now been used japanese engines Ha-2-II the performance of the engine was lower, but on the other hand managed to slightly improve aerodynamics, leading edges of the wings was used to smooth duralumin sheet (before corrugated) and before the bomb bay doors were installed aerodynamic covers. The main distinguishing feature was a faired landing gear. The performance then was slightly better, but the popularity has remained small..
Reklama
http://www.airwar.ru/enc/bww1/ki1.html
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| Type | Micubiši Ki 1-II |
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| Date (DD.MM.RRRR) | DD.MM.RRRR |
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