| Název: Name: | Micubiši 3MT10 7-Ši | Mitsubishi 3MT10 7-Shi |
| Originální název: Original Name: | 海軍七試艦上攻撃機 [3MT10] / 九5 | |
| Kategorie: Category: | bombardovací letoun | bomber aeroplane |
| Výrobce: Producer: | DD.MM.1932-DD.MM.1932 Mitsubishi Internal Combustion Engine Manufacturing Co., Ltd., Nagoya | |
| Období výroby: Production Period: | DD.MM.1932-DD.MM.1932 | |
| Vyrobeno kusů: Number of Produced: | 1 | |
| První vzlet: Maiden Flight: | DD.10.1932 | |
| 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: | dvouplošník | biplane |
| 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: | 2600 kg | 5732 lb |
| Vzletová hmotnost: Take-off Weight: | 4400 kg | 9700 lb |
| Maximální vzletová hmotnost: Maximum Take-off Weight: | ? kg | ? lb |
| Rozpětí: Wingspan: | 14,723 m | 48ft 3,64in |
| Délka: Length: | 10,079 m | 33ft 0,81in |
| Výška: Height: | 3,885 m | 12ft 8,94in |
| Plocha křídla: Wing Area: | 57,00 m2 | 613.54 ft2 |
| Plošné zatížení: Wing Loading: | 79,19 kg/m2 | 16.22 lb/ft2 |
| Pohon: Propulsion: | ||
| Kategorie: Category: | pístový | piston |
| Počet motorů: Number of engines: | 1 | |
| Typ: Type: | Rolls-Royce Buzzard II MS kapalinou chlazený vidlicový dvanáctiválec o výkonu 615 kW Vrtule: dřevěná, dvoulistá, nestavitelná o průměru 4 000 mm | Rolls-Royce Buzzard II MS twelve cylinder water-cooled Vee engine rated at 825 hp, driving a two-blade fixed-pitch wooden propellers of diameter 13ft 1.48ft |
| Objem palivových nádrží: Fuel Tank Capacity: | 930 l | 204.5 UK gallons |
| Výkony: Performance: | ||
| Maximální rychlost: Maximum Speed: | 213 km/h v 1000 m | 132.4 mph in 3281 ft |
| Cestovní rychlost: Cruise Speed: | 160 km/h v 1000 m | 99.4 mph in 3281 ft |
| Rychlost stoupání: Climb Rate: | ? m/s | ? ft/min |
| Čas výstupu na výšku: Time to Climb to: | 12,0 min do 3050 m | 12,0 min to 10007 ft |
| Operační dostup: Service Ceiling: | ? m | ? ft |
| Dolet: Range: | ? km | ? mi |
| Maximální dolet: Maximum Range: | ? km | ? mi |
| Výzbroj: Armament: | 1x pevný kulomet typ 87 ráže 7,7 mm v trupu 2x pohyblivý kulomet Type 87 ráže 7,7 mm - na konci kabiny a ve výstřelné štěrbině pod trupem 800 kg pum nebo 1x torpédo Type 91 o hmotnosti 785 kg | One forward-firing 0.303in Type 87 machine-gun Two flexible rear-firing 0.303in Type 87 machine-guns Bomb-load: one 800 kg torpedo or 800 kg of bombs carried externally under the fuselage. |
| Uživatelské státy: User States: | - | - |
| Poznámka: Note: | palubní torpédový bombardér Letová vytrvalost: 12,0 h Ka-5 – tovární označení | Carrier Attack or Torpedo Bomber Aircraft Endurance: 12,0 hours |
| Zdroje: Sources: | René J. Francillon Ph.D., Japanese Aircraft of the Pacific War, Naval Institute Press, Annapolis, Maryland, Peprinted, rok 1990, ISBN: 0-87021-313-X Robert C. Mikesh and Shorzoe Abe, Japanese Aircraft 1910-1941, Putnam Aeronautical Books, rok 1990, ISBN 1557505632 Tadeusz Januszewski a Kryzysztof Zalewski, Japońskie samoloty marynarski 1912-1945, Lampart, rok 2000, ISBN 83-86776-00-05 www.modelbud.pl - obrázek archiv autora | |
Micubiši 3MT10 7-Ši
Mitsubishi 3MT10 7-Shi / 海軍七試艦上攻撃機 [3MT10]
Mitsubishi 3MT10
Aircraft history:
In 1932, the Japanese Naval Air Command - Kaigun Koku Hombu wrote out the technical specifications of the 7-Shi for a deck torpedo aircraft of purely Japanese design. The Nakajima Hikoki K.K., Mitsubishi Jukogyo K.K. factories were approached, the Aichi Tokei Denki factory participated on its own initiative with an aircraft that was factory designated AB-8, the Naval Air Arsenal in Yokosuka also entered its aircraft and this machine eventually won. At the Mitsubishi Jukogyo K.K. factory, the design work was undertaken by Ing. Hajime Matsuhara, who, however, remained under the influence of the B2M torpedo bomber design, was himself involved in the design of this bomber, having already been in the construction of the prototype 3MT4 at Blackburn. He used a powerful Rolls-Royce Buzzard twelve-cylinder engine for propulsion. During factory trials at Kasumigahara base, the aircraft crashed after the engine lost revs, thus eliminating the aircraft from competition.
Other aircraft that participated in the 7-Shi program were Aichi AB-8; Nakajima B3N1 and Yokosuka B3Y[/b
Aircraft history:
In 1932, the Japanese Naval Air Command - Kaigun Koku Hombu wrote out the technical specifications of the 7-Shi for a deck torpedo aircraft of purely Japanese design. The Nakajima Hikoki K.K., Mitsubishi Jukogyo K.K. factories were approached, the Aichi Tokei Denki factory participated on its own initiative with an aircraft that was factory designated AB-8, the Naval Air Arsenal in Yokosuka also entered its aircraft and this machine eventually won. At the Mitsubishi Jukogyo K.K. factory, the design work was undertaken by Ing. Hajime Matsuhara, who, however, remained under the influence of the B2M torpedo bomber design, was himself involved in the design of this bomber, having already been in the construction of the prototype 3MT4 at Blackburn. He used a powerful Rolls-Royce Buzzard twelve-cylinder engine for propulsion. During factory trials at Kasumigahara base, the aircraft crashed after the engine lost revs, thus eliminating the aircraft from competition.
Other aircraft that participated in the 7-Shi program were Aichi AB-8; Nakajima B3N1 and Yokosuka B3Y[/b
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Shigeru Nohara: The Xplanes of Imperial Japanese Army & Navy 1924-45, Illustrated Warplane History, ISBN4-7663-3292-X
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