Boeing

Boeing CH-47 Chinook

Transport

Boeing CH-47 Chinook
  • First flight1961
  • Introduction1962
  • StatusIn service
  • Number built1,179+

History

Design and development

CH-47 carries a howitzer, 1970

Initial development

During late 1956, the U.S. Department of the Army announced its intention to replace the Sikorsky CH-37 Mojave, which was powered by piston engines, with a new, gas turbine-powered helicopter.[2] Turbine engines were also a key design feature of the smaller UH-1 “Huey” utility helicopter. Following a design competition, in September 1958, a joint Army–Air Force source selection board recommended that the Army procure the Vertol-built medium-transport helicopter. Funding for full-scale development was not then available, though, and the Army vacillated on its design requirements. Some officials in Army Aviation thought that the new helicopter should be operated as a light tactical transport aimed at taking over the missions of the old piston-engined Piasecki H-21 and Sikorsky H-34 helicopters, and be consequently capable of carrying about 15 troops (one squad). Another faction in Army Aviation thought that the new helicopter should be much larger, enabling it to airlift large artillery pieces and possess enough internal space to carry the new MGM-31 “Pershing” missile system.[2]

HC-1B during in-flight evaluation

During 1957, Vertol commenced work upon a new tandem-rotor helicopter, designated as the Vertol Model 107 or V-107.[3][4] During June 1958, the U.S. Army awarded a contract to Vertol for the acquisition of a small number of the rotorcraft, giving it the YHC-1A designation.[5] As ordered, the YHC-1A possessed the capacity to carry a maximum of 20 troops.[2] Three underwent testing by the Army for deriving engineering and operational data. However, the YHC-1A was considered by many figures within the Army users to be too heavy for the assault role, while too light for the more general transport role.[2] Accordingly, a decision was made to procure a heavier transport helicopter, and at the same time, upgrade the UH-1 “Huey” to serve as the needed tactical troop transport. The YHC-1A would be improved and adopted by the Marines as the CH-46 Sea Knight in 1962.[6] As a result, the Army issued a new order to Vertol for an enlarged derivative of the V-107, known by internal company designation as the Model 114, which it gave the designation of HC-1B.[7] On 21 September 1961, the preproduction Boeing Vertol YHC-1B made its initial hovering flight. During 1962, the HC-1B was redesignated the CH-47A under the 1962 United States Tri-Service aircraft designation system; it was also named “Chinook” after the Chinook people of the Pacific Northwest

Technical data

Specifications

01

Crew & dimensions

Crew
3 (pilot, copilot, flight engineer or loadmaster)
Length
98 ft 10.7 in
Height
18 ft 7.8 in
02

Performance

Maximum speed
170 kn
Range
400 nmi
Service ceiling
20,000 ft
03

Powerplant

Powerplant
2 × Lycoming T55-GA-714A turboshaft engines (4,733 shp)
04

Armament

Armament
Up to 3 pintle-mounted medium machine guns (1 on loading ramp and 2 at shoulder windows), generally 7.62 mm (0.300 in) M240/FN MAG machine guns, and can be armed with the 7.62 mm M134 Minigun rotary machine gun
Technical drawing

Silhouette

Side viewATN-02201
Silhouette of the Boeing CH-47 Chinook — side view
Aircraft
Boeing CH-47 Chinook
First flight
1961
Role
Transport
Length
98 ft 10.7 in
Height
18 ft 7.8 in
Drawing
Aircrafttotal · Side view

Helicopter 1

BC 1961 American helicopters Boeing CH-47 Chinook In production for more than 60 years Boeing · United States→