| Název: Name: | Airbus Helicopters Puma HC.2 | Airbus Helicopters Puma HC.2 |
| Originální název: Original Name: | Airbus Helicopters Puma HC.2 | |
| Kategorie: Category: | víceúčelový vrtulník | utility helicopter |
| Výrobce: Producer: | DD.MM.2013-31.12.2013 Eurocopter France SA, Marignane 01.01.2014-DD.MM.201R Airbus Helicopters SAS, Marignane DD.MM.2013-31.12.2013 Eurocopter Romania SA, Ghimbav 01.01.2014-DD.MM.2015 Airbus Helicopters Romania SA, Ghimbav | |
| Období výroby: Production Period: | DD.MM.2013-DD.MM.2015 | |
| Vyrobeno kusů: Number of Produced: | 24 konverzí Puma HC.1 | |
| První vzlet: Maiden Flight: | DD.MM.RRRR | |
| Osádka: Crew: | 2 | |
| Základní charakteristika: Basic Characteristics: | ||
| Uspořádání rotorů: Rotor Configuration: | hlavní a vyrovnávací rotor | main and antitorque rotor |
| Podvozek: Undercarriage: | zatahovací | retractable |
| Přistávací zařízení: Landing Gear: | kola | wheels |
| Technické údaje: Technical Data: | ||
| Hmotnost prázdného vrtulníku: Empty Weight: | ? kg | ? lb |
| Vzletová hmotnost: Take-off Weight: | ? kg | ? lb |
| Maximální vzletová hmotnost: Maximum Take-off Weight: | ? kg | ? lb |
| Délka s otáčejícími se rotory: Length with Rotors Turning: | 18,20 m | 59ft 8,53in |
| Délka trupu: Fuselage Length: | 14,06 m | 46ft 1,53in |
| Šířka trupu: Fuselage Width: | 2,00 m | 6ft 6,73in |
| Celková výška: Overall Height: | 5,14 m | 16ft 10,36in |
| Průměr hlavního rotoru: Main Rotor Diameter: | 15,09 m | 49ft 6,09in |
| Průměr vyrovnávacího rotoru: Tail Rotor Diameter: | ? m | ? |
| Plocha disku hlavního rotoru: Main Rotor Disc Area: | 178,84 m2 | 1925.02 ft2 |
| Plocha disku vyrovnávacího rotoru: Tail Rotor Disc Area: | ? m2 | ? ft2 |
| Pohon: Propulsion: | ||
| Kategorie: Category: | turbohřídelový | turboshaft |
| Počet motorů: Number of engines: | 2 | |
| Typ: Type: | Turboméca Makila 1A1 o vzletovém výkonu 1357 kW/1845 k | Turboméca Makila 1A1, take-off power 1820 shp |
| Objem palivových nádrží: Fuel Tank Capacity: | ? | ? |
| Výkony: Performance: | ||
| Maximální rychlost: Maximum Speed: | 309 km/h v ? m | 192 mph in ? ft |
| Cestovní rychlost: Cruise Speed: | ? km/h v ? m | ? mph in ? ft |
| Rychlost stoupání: Climb Rate: | ? m/s | ? ft/min |
| Statický dostup: Static Ceiling: | ? m | ? ft |
| Dynamický dostup: Dynamic Ceiling: | 3993 m | 13100 ft |
| Dolet: Range: | ? km | ? mi |
| Maximální dolet: Maximum Range: | ? km | ? mi |
| Přepravní kapacita: Transport Capacity: | 16 vojáků nebo 6 ležících a 4 sedící zranění 2000 kg nákladu | 16 troops or 6 stretchers and 4 sitting wounded 4400 lb of cargo |
| Výzbroj a vybavení: Armament and Equipment: | ||
| Výzbroj: Armament: | 2x pohyblivý kulomet ráže 7,62 mm | 2x 7.62mm flexible machine gun |
| Vybavení: Equipment: | - | - |
| Uživatelské státy: User States: | | |
| Poznámka: Note: | - | - |
| Zdroje: Sources: | https://www.raf.mod.uk/aircraft/puma-hc2/ www.raf.mod.uk www.flightglobal.com https://www.helis.com/database/model/Puma-Mk2/ | |
Airbus Helicopters Puma HC.2
www.thinkdefence.co.uk].
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Reklama
Puma HC.2 abuts on a dirt landing area, exercise Agile Spear 15, the military training area Salisbury Plain, September 2015. Home base displayed the helicopter was RAF Benson, where operated all the services of the RAF-armed Puma helicopters HC.2: 28. squadron RAF, 33. squadron RAF and 230. squadron RAF..
© Crown Copyright
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© Crown Copyright
Puma HC.2 of the detachment 33. squadron RAF deleted decoys, operation Toral, Afghanistan, December 2015. Unit operated from the airport in Kabul from September 2015 to early 2016..
© Crown Copyright
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| Type | Airbus Helicopters Puma HC.2 |
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| Date (DD.MM.RRRR) | DD.MM.RRRR |
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| Published with authors permit | - |
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© Crown Copyright
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