| Název: Name: | Hiro H4H1 | Hiro H4H1 (Navy Type 91 Flying-Boat) |
| Originální název: Original Name: | 九一式一号飛行艇（H4H1） | |
| Kategorie: Category: | průzkumný/pozorovací letoun | reconnaissance/scout aeroplane |
| Výrobce: Producer: | DD.MM.1931-DD.MM.1932 Hiro Naval Arsenal, Hiro | |
| Období výroby: Production Period: | DD.MM.1931-DD.MM.1932 | |
| Vyrobeno kusů: Number of Produced: | 2 | |
| První vzlet: Maiden Flight: | DD.MM.1931 | |
| Osádka: Crew: | 6 | |
| 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: | člunový trup | flying boat |
| Technické údaje: Technical Data: | ||
| Hmotnost prázdného letounu: Empty Weight: | 4304 kg | 9489 lb |
| Vzletová hmotnost: Take-off Weight: | 7500 kg | 16535 lb |
| Maximální vzletová hmotnost: Maximum Take-off Weight: | 8020 kg | 17681 lb |
| Rozpětí: Wingspan: | 23,550 m | 77ft 3in |
| Délka: Length: | 16,675 m | 54ft 8,5in |
| Výška: Height: | 5,810 m | 19ft 0,75in |
| Plocha křídla: Wing Area: | 82.70 m2 | 890.204 ft2 |
| Plošné zatížení: Wing Loading: | 79,27 kg/m2 | 16.24 lb/ft2 |
| Pohon: Propulsion: | ||
| Kategorie: Category: | pístový | piston |
| Počet motorů: Number of Engines: | 2 | |
| Typ: Type: | Hiro typ 91-2, kapalinou chlazený dvanáctiválec s válci do W o vzletovém výkonu 441 kW (600 k) a 382 kW (520 k) v h= 1 000 m. Vrtule čtyřlisté, dřevěné, vrtulové listy s pevným úhlem náběhu o průměru 3 600 mm | Hiro Type 91-2 twelve-cylinder water-cooled W-block (3 banks of 4 cylinders) engine, rated at 592 hp for take-off and 513 hp at 3,281 ft, driving a four-blade fixed-pitch wooden propellers of the diameter 11ft 9,75in. |
| Objem palivových nádrží: Fuel Tank Capacity: | ? | ? |
| Výkony: Performance: | ||
| Maximální rychlost: Maximum Speed: | 207.6 km/h v 0 m | 129 mph in 0 ft |
| Cestovní rychlost: Cruise Speed: | 157.7 km/h v 1000 m | 98 mph in 3281 ft |
| Rychlost stoupání: Climb Rate: | ? m/s | ? ft/min |
| Čas výstupu na výšku: Time to Climb to: | 18,0 min do 3000 m | 18,0 min to 9843 ft |
| Operační dostup: Service Ceiling: | 4970 m | 16306 ft |
| Dolet: Range: | 2000 km | 1243 mi |
| Maximální dolet: Maximum Range: | ? km | ? mi |
| Výzbroj: Armament: | 3x pohyblivý kulomet Type 89 Model 1 ráže 7,7 mm 1x v předním střelišti a 1x zdvojený kulomet ve střelišti na hřbetě trupu. Pumový náklad: do hmotnosti 500 kg (2x 250 kg). | One flexible 0.303 inch Type 89 Model 1 machine-gun in a bow-mounted and one twin flexible 0.303 inch Type 89 Model 1 machine-guns in dorsal position. Bomb load: Two 551 lb bombs. |
| Uživatelské státy: User States: | | |
| Poznámka: Note: | 九一式飛行艇 - Námořní hydroplán Hiro typ 91 model 1 První prototyp byl poháněn motory Hiro Type 91-1 o vzletovém výkonu 373 kW. | 九一式飛行艇 - Hiro Navy Type 91 Model 1 Flying Boat The first prototype was powered by engines Hiro Type 91-1 rated at 500 hp for take-off. |
| Zdroje: Sources: | Robert C. Mikesh and Shorzoe Abe, Japanese Aircraft 1910-1941, Naval Institute Press Annapolis, Maryland 21402, 1990, ISBN: 1-155750-563-2 Tadashi Nozawa, Encyclopedia of Japanese Aircraft 1900-1945, Vol.3. Kawanishi, Yokosuka Aircraft. Tokio, Shuppan Kyōdōsha (出版協同社), rok 1981 Tadeusz Januszewski a Kryzysztof Zalewski, Japońskie samoloty marynarski 1912-1945, tiel 2, Lampart, rok 2000, ISBN 83-86776-00-05 http://en.wikipedia.org/wiki/Hiro_H4H archiv autora | |
Hiro H4H1
Hiro H4H1 / 広廠 H4H1・九一式一号飛行艇
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