Haynes Publishing Group HYNH5401 – Kniha RAF CHINOOK MANUAL HAYNES ( RAF Official Licensed Product )

499 

Skladem

Katalogové číslo: HYNH5401 Kategorie: , , ,
Výrobce: Haynes Publishing Group

Popis

-kniha   RAF CHINOOK MANUAL HAYNES  ( RAF  Official Licensed Product )
               jazyk:  Angličtina
               vazba: Pevná
               počet stran: 160
               nakladatelství: Haynes Publishing Group

                   Boeing CH-47 Chinook

Boeing CH-47 Chinook je americký střední transportní vrtulník s tandemovým uspořádáním dvou nosných rotorů. Je přímým pokračovatelem známého typu CH-46D Sea Knight. První prototyp vzlétl 21. září roku 1961 a první sériově vyráběné vrtulníky byly dodány koncem roku 1965.

The Boeing CH-47 Chinook is an American twin-engined, tandem rotor, heavy-lift helicopter developed by American rotorcraft company Vertol and manufactured by Boeing Vertol (later known as Boeing Rotorcraft Systems). The CH-47 is among the heaviest lifting Western helicopters. Its name, Chinook, is from the Native American Chinook people of modern-day Washington state.

Role Transport helicopter
National origin United States
Manufacturer Boeing Rotorcraft Systems
First flight 21 September 1961
Introduction 1962
Status In service
Primary users United States Army
Japan Ground Self-Defense Force
Royal Netherlands Air Force
See CH-47 operators for others
Produced 1962–present
Number built Over 1,200 as of 2012
Unit cost
US$38.55 million (CH-47F, FY13)
Developed from Vertol Model 107
Variants Boeing Chinook HC (UK variants)

General characteristics

  • Crew: 3 three (pilot, copilot, flight engineer or loadmaster)
  • Capacity:
    • 33–55 troops or
    • 24 litters and 3 attendants or
  • Payload: 24,000 lb (10,886 kg)
  • Length: 98 ft 10 in (30.1 m)
  • Fuselage length: 52 ft (15.85 m)
  • Fuselage width: 12 ft 5 in (3.78 m)
  • Rotor diameter: 60 ft  (18.3 m)
  • Height: 18 ft 11 in (5.7 m)
  • Disc area: 5,600 ft2 (520 m2)
  • Empty weight: 24,578 lb (11,148 kg)
  • Max. takeoff weight: 50,000 lb (22,680 kg)
  • Powerplant: 2 × Lycoming T55-GA-714A turboshaft, 4,733 shp (3,529 kW) each

Performance

  • Maximum speed: 170 knots (196 mph, 315 km/h)
  • Cruise speed: 160 kt (184 mph, 296 km/h)
  • Range: 400 nmi (450 mi, 741 km)
  • Combat radius: 200 nmi (230 mi, 370 km)
  • Ferry range: 1,216 nmi (1,400 mi, 2,252 km)
  • Service ceiling: 20,000 ft (6100 m)
  • Rate of climb: 1,522 ft/min (7.73 m/s)
  • Disc loading: 9.5 lb/ft2 (47 kg/m2)
  • Power/mass: 0.28 hp/lb (460 W/kg)

Armament

  • Up to 3 pintle-mounted medium machine guns (1 on loading ramp and 2 at shoulder windows), generally 7.62 mm (0.308 in) M240/FN MAG machine guns, and can be armed with the 7.62 mm M134 rotary machine gun

Avionics

  • Rockwell Collins Common Avionics Architecture System (CAAS) (MH-47G/CH-47F)

Další informace

Výrobce

Dostupnost

Skladem

Mohlo by se Vám líbit…