Název: Name: | Micubiši Ki 2-I | Mitsubishi Ki-2-I |
Originální název: Original Name: | キ2-I 一型九三式双发轻爆击机 | |
Kategorie: Category: | bombardovací letoun | bomber aeroplane |
Výrobce: Producer: | DD.MM.1933-DD.06.1934 Mitsubishi Internal Combustion Engine Manufacturing Co., Ltd., Nagoya DD.06.1934-DD.MM.1936 Mitsubishi Heavy Industries, Ltd., Nagoya DD.11.1934-DD.08.1935 Kawasaki Shipyard, Ltd., Kakamigahara | |
Období výroby: Production Period: | DD.MM.1933-DD.MM.1936 | |
Vyrobeno kusů: Number of Produced: | Mitsubishi 113 Kawasaki 13 total 126 | |
První vzlet: Maiden Flight: | DD.05.1933 | |
Osádka: Crew: | 3 | |
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: | 2760 kg | 6085 lb |
Vzletová hmotnost: Take-off Weight: | 4420 kg | 9744 lb |
Maximální vzletová hmotnost: Maximum Take-off Weight: | 4650 kg | 10251 lb |
Rozpětí: Wingspan: | 19,952 m | 65ft 5,5in |
Délka: Length: | 12,600 m | 41ft 4in |
Výška: Height: | 4,636 m | 15ft 2,5in |
Plocha křídla: Wing Area: | 56,20 m2 | 604.93 ft2 |
Plošné zatížení: Wing Loading: | 78,65 kg/m2 | 16.11 lb/ft2 |
Pohon: Propulsion: | ||
Kategorie: Category: | pístový | piston |
Počet motorů: Number of Engines: | 2 | |
Typ: Type: | Nakadžima Jupiter vzduchem chlazený hvězdicový devítiválec o výkonu 335,5 kW. Vrtule dvoulistá dřevěná. | Nakajima Jupiter nine-cylinder air-cooled radial engine, rated at 450 hp for take-off, driving a two-blade wooden propeller. |
Objem palivových nádrží: Fuel Tank Capacity: | ? | ? |
Výkony: Performance: | ||
Maximální rychlost: Maximum Speed: | 255 km/h v 3000 m | 158.4 mph in 9843 ft |
Cestovní rychlost: Cruise Speed: | 150 km/h v 3000 m | 93.2 mph in 9843 ft |
Rychlost stoupání: Climb Rate: | ? m/s | ? ft/min |
Čas výstupu na výšku: Time to Climb to: | 10,5 min do 3000 m | 10,5 min to 9843 ft |
Operační dostup: Service Ceiling: | 7000 m | 22966 ft |
Dolet: Range: | 900 km | 559.2 mi |
Maximální dolet: Maximum Range: | 1630 km | 1012.8 mi |
Výzbroj: Armament: | 1x pohyblivý kulomet typ 89 model 1 ráže 7,7 mm v polozakratý střelecké věži v přídi a 1x pohyblivý kulomet typ 89 model 1 ráže 7,7 mm ve hřbetním střelišti. Pumový náklad: 300 - 500 kg | One flexible 0.303 inch Type 89 Model 1 machine-gun mounted in a semi-enclosed nose gun turret and one flexible 0.303 inch Type 89 Model 1 machine-gun dorsal position. Bomb load: 661 lb to 1,102 lb of bombs. |
Uživatelské státy: User States: | | |
Poznámka: Note: | キ2-I 一型九三式双发轻爆击机 - Iči gata Kju san-šiki sokei bakugekiki - Armádní lehký dvoumotorový bombardér Typ 93-I (Ki-2-I) Spojenecké kódové jméno: Luise | キ2-I 一型九三式双发轻爆击机 - Ichi gata Kyu san-shiki sokei bakugekiki - Army Type 93-1 Twin-engined Light Bomber (Ki-2-I) Allied Code Name: "Luise" In February 1931, a Swedish-built Junkers K 37 aircraft had been purchased by private funds and donated to the Army in early 1932 as Aikuko (patriotic gift) No.1, this being the first of many such privately donated Aikuko machines. This machine subsequently seeing combat service in Manchuria. In close association with the Army Type 93 Heavy Bomber, the Army was interested in devloping a twin-engined light bomber that was also based upon the qualities observed in the imported Swedish-built Junkers K 37. During the K 37's participation in combat in Manchuria in support of ground troops, its performance proved superior to that of the Mitsubishi Type 87 and the Kawasaki Type 88 Light Bombers. To replace these older aircraft, in September 1932 the Army asked Mitsubishi to redesign the K 37 to meet specific requirements for a new three-seat bomber that would become the Ki-2 in the new Kitai numbering system. The design team remained that of the Ki-1 project, Nobushiro Nakata as chief designer, assisted by Kiro Honjo, HIsanojo Ozawa, and Jiro Tanaka. Capt. Komabayishi continued his liaison role for the Army. This new light bomber was to have a crew of three or four and be very manoeuvrable, especially in making tight turns. With one engine inoperative, it was to be able to maintain straight and level flight. Ease of handling in night landings and take-offs as well as daylight operations would be a strong consideration. Maximum speed should be 161 mph at 9,842 ft. Fuel capacity should allow for a 4 1/2 hr flight at 149 mph 9,842 ft with a 661 to 1,102 lb bomb load, or 6 hr at the same speed without a bomb load. Normal operating altitude would be from 6,561 ft to 9,842 ft, with a service ceiling of 22,965 ft. The engines were to be 450 hp Nakajima-built Jupiters. Two prototypes of the new bomber were asked for, the first to be completed by July 1933. |
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 Robert C. Mikesh and Shorzoe Abe, Japanese Aircraft 1910-1941, Naval Institute Press Annapolis, Maryland 21402, 1990, ISBN: 1-155750-563-2 www.aviastar.org archiv autora |