Top
about
element
General Info

Boeing CH-46E
Seaknight "Phrog"

 
General information
Type Transport helicopter
National origin United States
Manufacturer
Status In limited service
Primary users United States Marine Corps (historical)
Number built H-46: 524
History
Manufactured 1962–1971
Introduction date 1964
First flight 22 April 1958 (V-107)
Retired
  • 2004 (US Navy)
  • 2015 (US Marine Corps)
Developed into

.

History Boeing 
BoeingCH-46E Seaknight
Manufactured 1962–1971 Introduction date 1964
First flight 22 April 1958 (V-107)



Development of the Sea Knight, which was originally designated by the firm as the Vertol Model 107, commenced during 1956. It was envisioned as a successor to the first generation of rotorcraft, such as the H-21 "Flying Banana", that had been powered by piston engines; in its place, the V-107 made use of the emergent turboshaft engine. On 22 April 1958, the V-107 prototype performed its maiden flight. During June 1958, the US Army awarded a contract for the construction of ten production-standard aircraft, designated as the YHC-1A, based on the V-107; this initial order was later cut down to three YHC-1As. During 1961, the US Marine Corps (USMC), which had been studying its requirements for a medium-lift, twin-turbine cargo/troop assault helicopter, selected Boeing Vertol's Model 107M as the basis from which to manufacture a suitable rotorcraft to meet their needs. Known colloquially as the "Phrog" and formally as the "Sea Knight", it was operated across all US Marine Corps' operational environments between its introduction during the Vietnam War and its frontline retirement during 2014.

Development

Origins

During the 1940s and 1950s, American rotorcraft manufacturer Piasecki Helicopter emerged as a pioneering developer of tandem-rotor helicopters; perhaps the most famous of these being the piston-powered H-21 "Flying Banana", an early utility and transport helicopter. During 1955, Piasecki was officially renamed as Vertol Corporation (standing for vertical take-off and landing); it was around this time that work commenced on the development of a new generation of tandem rotor helicopter. During 1956, the new design received the internal company designation of Vertol Model 107, or simply V-107; this rotorcraft differed from its predecessors by harnessing the newly developed turboshaft engine instead of piston-based counterparts. During that year, construction of a prototype, powered by a pair of Lycoming T53 turboshaft engines, each one being capable of producing 877 shp (640 kW), commenced.

V-107 prototype in 1961
On 22 April 1958, the V-107 prototype performed its maiden flight. In order to garner publicity for the newly developed rotorcraft, it was decided to use the prototype to conduct a series of publicised flight demonstrations during a tour across the United States and several overseas nations. During June 1958, it was announced that the U.S. Army had awarded a contract to Vertol for the construction of ten production-standard aircraft based on the V-107, which were designated YHC-1A.[4] However, this order was later decreased to three helicopters; according to aviation author Jay P. Spenser, the cutback had been enacted in order that the U.S. Army would be able to divert funds for the development of the rival V-114 helicopter, which was also a turbine-powered tandem rotor design but substantially larger than the V-107. All of the U.S. Army's three YHC-1As were powered by pairs of GE-T-58 engines. During August 1959, the first YHC-1A-model rotorcraft conducted its first flight; independently, it was shortly followed by the maiden flight of an improved model intended for the commercial and export markets, designated 107-II..[.

0

Km

Ceiling

0

Km

MAX RANGE

0

Km/H

Aircraft Speed

0

Max Crew

element
element
Boeing Vertol helicopters

BoeingCH-46E Seaknight
Manufactured 1962–1971 Introduction date 1964 First flight 22 April 1958 (V-107)

1

General characteristics

  • Crew: 5: two pilots, one crew chief, one aerial gunner/observer, one tail gunner
  • Capacity:
    • 24 troops or
    • 15 stretchers and two attendants
    • 7,000 lb (3,200 kg)
  • Length: 44 ft 10 in (13.67 m) (fuselage)
  • 83 ft 4 in (25.40 m) (rotors turning)
    • Height: 16 ft 9 in (5.11 m) to top of rear rotor head
2

Powerplant

plane
3

Specifications

  • Maximum speed: 144 kn (166 mph, 267 km/h) at sea level
  • Cruise speed: 143 kn (165 mph, 265 km/h) maximum at sea level
  • Range:  1,020 km) with (1,100 kg) payload
  • Ferry range:  1,100 km)
  • Service ceiling: (5,200 m)
  • Hover ceiling IGE: (2,900 m)
  • Hover ceiling OGE: (1,750 m)
4

Armament

Special Links Boeing/Hughes CH-46E SEaknight

Links to Youtube & Others

Beginning in April 2011 the Navy's Fleet Readiness Center East began refurbishing retired USMC CH-46Es for service with the United States Department of State Air Wing.. A number of CH-46s from HMX-1 were transferred to the Air Wing in late 2014

Boeing CH-46E Seaknight "Phrog"

The Royal Canadian Air Force procured six CH-113 Labrador helicopters for the SAR role

interior

Youtube Link

In 1963, Sweden procured ten UH-46Bs from the US as a transport and anti-submarine helicopter for the Swedish Armed Forces, designated Hkp 4A.

interior
Aircrafttotal : Helicopters

Read more in Helicopters

brand
brand
brand
brand
brand