БО-105 ПАГ

MBB Bo 105

КраїніЗахідна Німеччина
РольЛегкий комунальний вертоліт
Перший політ6 лютого 1967 р.
Побудований1500+

У 201 Messerschmitt-Bölkow-Blohm bo 105 is a light, twin-engine, multi-purpose helicopter developed by Bölkow of Ottobrunn, West Germany. It was the first light twin-engine helicopter in the world, and the first rotorcraft that could perform aerobatic maneuvers such as inverted loops. The Bo 105 features a revolutionary hingeless rotor system, a pioneering innovation in helicopters when it was introduced into service in 1970. Production of the Bo 105 began at the then-recently merged Messerschmitt-Bölkow-Blohm (MBB). The main production facilities for producing the Bo 105 were located in Germany and Canada; due to the level of export sales encountered, additional manufacturing lines were set up in Spain, Indonesia, and the Philippines. MBB became a part of Eurocopter in 1991, who continued production of the type until 2001. The Bo 105 was formally replaced in Eurocopter’s product range by the newer Eurocopter EC135.

Джерело: MBB Bo 105 у Вікіпедії

BO-105 PAH Walk Around
ФотографівНезнай
ЛокалізацієюНезнай
Фото25
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Літак Amodel 72322-1/72 MBB Bo-105 GSH, масштабний пластиковий модельний набір - Amazon

BO-105 PAH 1A1 Walk Around
ФотографівНезнай
ЛокалізацієюНезнай
Фото20
Зачекайте, шукаючи MBB Bo 105 для вас...
BO-105 PAH 1A1 Walk Around
ФотографівУльріх Веде
ЛокалізацієюНезнай
Фото17

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General Characteristics

The MBB Bo 105 (later Eurocopter, now Airbus Helicopters) is a light, twin-engine utility helicopter developed in West Germany. It is famous for being the first light helicopter in the world to feature the innovative rigid main rotor system.

Property Value (Bo 105 CBS Variant)
Роль Light Utility, Search and Rescue (SAR), Air Ambulance, Anti-Tank
Виробник Bolkow / Messerschmitt-Bölkow-Blohm (MBB)
First Flight February 16, 1967
команда 1 or 2 pilots
Passenger Capacity 4 passengers (5 total occupants)
Maximum Take-Off Weight 2,500 kg (5,511 lb)

Design and Powerplant

  • Powerplant: Two Allison 250-C20B turboshaft engines (Rolls-Royce).
  • Power Output: Approximately 313 kW (420 shp) each (for C20B model).
  • Rotor System: Four-blade rigid main rotor made of fiberglass, featuring a unique hingeless design. This system provides exceptionally responsive control and improved negative G maneuverability.
  • Transmission: Dual hydraulic system and transmission designed to run dry for an extended period, enhancing safety.
  • Fuselage: Semi-monocoque aluminum alloy construction.

Performance and Armament

  • Maximum Speed (VNE): 242 km/h (150 mph / 131 knots).
  • Cruise Speed: 232 km/h (144 mph).
  • Operational Range: Up to 575 km (357 miles).
  • Service Ceiling: 5,180 m (17,000 ft).
  • Anti-Tank Role: The military variant (e.g., Bo 105 PAH-1) was equipped with up to six HOT anti-tank missiles for the German Army.
  • Notable Feature: Its rigid rotor system allows the Bo 105 to perform certain aggressive aerobatic maneuvers (loops and rolls) not typically possible for helicopters of its size and configuration.

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