Military Wiki
Im>Chesipiero
 
m (→‎Design and development: Remove some templates, interwiki links, delink non military terms, cleanup and move Wikipedia link above categories)
 
(16 intermediate revisions by 2 users not shown)
Line 1: Line 1:
 
{|{{Infobox aircraft begin
<!-- This article is a part of [[Wikipedia:WikiProject Aircraft]]. Please see [[Wikipedia:WikiProject Aircraft/page content]] for recommended layout. -->
 
{|{{Infobox Aircraft Begin
 
 
|name =Gloster E.1/44
 
|name =Gloster E.1/44
 
|image = Gloster E1-44 2.jpg
 
|image = Gloster E1-44 2.jpg
 
|caption = TX148, the third prototype on a test flight, c. 1949
 
|caption = TX148, the third prototype on a test flight, c. 1949
 
}}
}}{{Infobox Aircraft Type
+
{{Infobox aircraft type
 
|type =Fighter
 
|type =Fighter
|manufacturer =[[Gloster Aircraft Company]]
+
|manufacturer =Gloster Aircraft Company
 
|designer =[[George Carter (engineer)|George Carter]]
 
|designer =[[George Carter (engineer)|George Carter]]
 
|first flight =9 March 1948
 
|first flight =9 March 1948
Line 24: Line 24:
   
 
==Design and development==
 
==Design and development==
The success of the first British jet aircraft the [[Gloster E.28/39]] led to the design of the twin-engined [[Gloster Meteor]] jet fighter from 1940 onwards. However in 1942 [[Rover Company|Rover]], who were contracted to produce the [[Frank Whittle|Whittle]] W2 jet engine, were having production problems so the [[Air Ministry]] issued a Specification, [[List of Air Ministry Specifications|E.5/42]], asking for a design which would use only one engine rather than the two. Gloster produced a design for a low-winged [[monoplane]] with a highly tapered wing and a [[T-tail]], to be fitted with a [[conventional landing gear|tailwheel undercarriage]]. It was to be powered by a single [[de Havilland Goblin|Halford H.1]] or [[Rolls-Royce Nene]] engine fed by intakes in the wing roots. Construction began of two GA.1 prototypes began late in 1943.<ref name="Goulding p146">Goulding 1986, p. 146.</ref><ref name="James p306-7">James 1971, pp. 306–307.</ref> In the end [[Rolls-Royce Limited]] traded jet engine production (the W2 would become known as the [[Rolls-Royce Welland|Welland]]) for [[Rolls-Royce Meteor|Meteor tank engine]] production with Rover; the supply problem was resolved and the single-engined design was not required. Gloster continued with their design work privately intending to use a Halford H.1 engine instead of the W2/Welland.
+
The success of the first British jet aircraft the [[Gloster E.28/39]] led to the design of the twin-engined [[Gloster Meteor]] jet fighter from 1940 onwards. However in 1942 [[Rover Company|Rover]], who were contracted to produce the [[Frank Whittle|Whittle]] W2 jet engine, were having production problems so the [[Air Ministry]] issued a Specification, [[List of Air Ministry Specifications|E.5/42]], asking for a design which would use only one engine rather than the two. Gloster produced a design for a low-winged monoplane with a highly tapered wing and a T-tail, to be fitted with a tailwheel undercarriage. It was to be powered by a single [[de Havilland Goblin|Halford H.1]] or [[Rolls-Royce Nene]] engine fed by intakes in the wing roots. Construction began of two GA.1 prototypes began late in 1943.<ref name="Goulding p146">Goulding 1986, p. 146.</ref><ref name="James p306-7">James 1971, pp. 306–307.</ref> In the end Rolls-Royce Limited traded jet engine production (the W2 would become known as the [[Rolls-Royce Welland|Welland]]) for [[Rolls-Royce Meteor|Meteor tank engine]] production with Rover; the supply problem was resolved and the single-engined design was not required. Gloster continued with their design work privately intending to use a Halford H.1 engine instead of the W2/Welland.
   
 
In 1944 the Ministry issued a Specification, [[List of Air Ministry Specifications|E.1/44]], for an experimental jet aircraft using the new Rolls-Royce Nene engine. Gloster's design to meet this specification was a new design (GA.2), not based on the E.5/42, being significantly larger.<ref name="Goulding p151">Goulding 1986, p.151.</ref> Gloster received a contract to build a single prototype, in 1944, with orders for a further three aircraft following in late 1945.<ref name="Mason fighter p356-7">Mason 1992, pp. 356–357.</ref>
 
In 1944 the Ministry issued a Specification, [[List of Air Ministry Specifications|E.1/44]], for an experimental jet aircraft using the new Rolls-Royce Nene engine. Gloster's design to meet this specification was a new design (GA.2), not based on the E.5/42, being significantly larger.<ref name="Goulding p151">Goulding 1986, p.151.</ref> Gloster received a contract to build a single prototype, in 1944, with orders for a further three aircraft following in late 1945.<ref name="Mason fighter p356-7">Mason 1992, pp. 356–357.</ref>
[[Image:E1-44.jpg|thumb|right|Gloster E.1/44 SM809 with original tail unit c. 1944]]
+
[[File:E1-44.jpg|thumb|right|Gloster E.1/44 SM809 with original tail unit c. 1944]]
[[Image:Gloster E1-44.jpg|thumb|right|Gloster E.1/44 TX145 with modified tail unit]]
+
[[File:Gloster E1-44.jpg|thumb|right|Gloster E.1/44 TX145 with modified tail unit]]
   
The new design was a [[stressed-skin]] [[mid-wing]]ed monoplane with, unlike the E5/42, a [[tricycle landing gear]]. The [[tailplane]] was mounted midway up the rear fuselage, behind the single [[Vertical stabilizer|fin]] and rudder. The engine was fed from semi-circular intakes ahead of the wing roots, while the wings were, unusually, skinned in difficult to work [[stainless-steel]].<ref name="Goulding p151-2">Goulding 1986, pp. 151–152.</ref><ref name="James p307-8">James 1971, pp. 307–308.</ref>
+
The new design was a [[stressed-skin]] [[mid-wing]]ed monoplane with, unlike the E5/42, a [[tricycle landing gear]]. The tailplane was mounted midway up the rear fuselage, behind the single fin and rudder. The engine was fed from semi-circular intakes ahead of the wing roots, while the wings were, unusually, skinned in difficult to work [[stainless-steel]].<ref name="Goulding p151-2">Goulding 1986, pp. 151–152.</ref><ref name="James p307-8">James 1971, pp. 307–308.</ref>
   
 
==Operational history==
 
==Operational history==
 
Progress on the new fighter was slow, with Gloster concentrating on development of the Meteor. The first prototype was not completed until July 1947, and was destroyed in a road accident when being taken to [[MoD Boscombe Down|Boscombe Down]] for flight testing.<ref name="Goulding p152">Goulding 1986, p. 152.</ref>
 
 
The first E.1/44 to fly (the second prototype) did so on 9 March 1948 at Boscombe Down flown by Gloster Chief Test Pilot [[Bill Waterton]] who was not impressed with its lack of power or poor flying characteristics, dubbing it the "Gormless". The unofficial name never stuck and the prototype did not have an official name, although "Ace" was proposed.<ref>Waterton 1956, p. 12.</ref>
 
 
Handling was initially poor, with a new tail unit, with a high mounted tailplane being fitted. While this solved the handling problems, performance was still little better than that of the Meteor, and the programme was stopped in 1949 as the aircraft did not have the development potential of the Meteor, with the fourth prototype (TX150) not completed.<ref name="James p309-0">James 1971, pp. 309–310.</ref> The revised E.1/44 tail design was, however, carried over to the Meteor, and employed on the Meteor F 8 and later models.<ref name="Goulding p155">Goulding 1986, p. 155.</ref> The only two aircraft to fly were used as testbeds for a while before being scrapped, one remaining in use until at least 1951.<ref name="James p310">James 1971, p. 310.</ref>
Progress on the new fighter was slow, with Gloster concentrating on development of the Meteor. The first prototype was not completed until July 1947, and was destroyed in a road accident when being taken to [[MoD Boscombe Down|Boscombe Down]] for flight testing.<ref name="Goulding p152">Goulding 1986, p. 152.</ref>
 
 
The first E.1/44 to fly (the second prototype) did so on 9 March 1948 at Boscombe Down flown by Gloster Chief Test Pilot [[Bill Waterton]] who was not impressed with its lack of power or poor flying characteristics, dubbing it the "Gormless". The unofficial name never stuck and the prototype did not have an official name, although "Ace" was proposed.<ref>Waterton 1956, p. 12.</ref>
 
 
Handling was initially poor, with a new tail unit, with a high mounted tailplane being fitted. While this solved the handling problems, performance was still little better than that of the Meteor, and the programme was stopped in 1949 as the aircraft did not have the development potential of the Meteor, with the fourth prototype (TX150) not completed.<ref name="James p309-0">James 1971, pp. 309–310.</ref> The revised E.1/44 tail design was, however, carried over to the Meteor, and employed on the Meteor F 8 and later models.<ref name="Goulding p155">Goulding 1986, p. 155.</ref> The only two aircraft to fly were used as testbeds for a while before being scrapped, one remaining in use until at least 1951.<ref name="James p310">James 1971, p. 310.</ref>
 
   
 
==Variants==
 
==Variants==
Line 51: Line 47:
 
:Forty early production aircraft were ordered in two batches in April and July 1946, cancelled and not built.
 
:Forty early production aircraft were ordered in two batches in April and July 1946, cancelled and not built.
   
==Specifications (E.1/44) ==
+
==Specifications (E.1/44)==
 
{{aircraft specifications
 
{{aircraft specifications
<!-- if you do not understand how to use this template, please ask at [[Wikipedia talk:WikiProject Aircraft]] -->
 
<!-- please answer the following questions -->
 
 
|plane or copter?=plane<!-- options: plane/copter -->
 
|plane or copter?=plane<!-- options: plane/copter -->
 
|jet or prop?=jet<!-- options: jet/prop/both/neither -->
 
|jet or prop?=jet<!-- options: jet/prop/both/neither -->
|ref=The British Fighter since 1912 <ref name="Mason fighterp357">Mason 1992, p. 357.</ref>
+
|ref=The British Fighter since 1912 <ref name="Mason fighterp357">Mason 1992, p. 357.</ref>
<!-- Now, fill out the specs. Please include units where appropriate (main comes first, alt in parentheses). If an item doesn't apply, like capacity, leave it blank. For instructions on using |more general=, |more performance=, |power original=, and |thrust original= see [[Template talk:Aircraft specifications]]. To add a new line, end the old one with a right parenthesis ")", and start a new fully formatted line beginning with * -->
 
 
|crew=
 
|crew=
 
|capacity=
 
|capacity=
Line 119: Line 112:
   
 
==See also==
 
==See also==
 
*[[Supermarine Attacker]]
{{aircontent|
 
|similar aircraft=*[[Supermarine Attacker]]
 
 
*[[Hawker Sea Hawk]]
 
*[[Hawker Sea Hawk]]
|lists=
 
 
}}
 
   
 
==References==
 
==References==
Line 144: Line 133:
   
 
==External links==
 
==External links==
{{commonscat|Gloster E.1/44}}
+
{{Commons|Gloster E.1/44}}
 
*[http://tanks45.tripod.com/Jets45/Histories/Gloster-E1-44/Gloster-E1-44.htm E.1/44]
 
*[http://tanks45.tripod.com/Jets45/Histories/Gloster-E1-44/Gloster-E1-44.htm E.1/44]
 
*[http://www.flightglobal.com/pdfarchive/view/1948/1948%20-%200521.html "Meteor's Stable-mate"] a 1948 ''Flight'' article
 
*[http://www.flightglobal.com/pdfarchive/view/1948/1948%20-%200521.html "Meteor's Stable-mate"] a 1948 ''Flight'' article
  +
{{Wikipedia|Gloster E.1/44}}
 
{{Gloster aircraft}}
 
{{aviation lists}}
 
   
 
{{DEFAULTSORT:Gloster E.1 44}}
 
{{DEFAULTSORT:Gloster E.1 44}}

Latest revision as of 09:58, 6 January 2019

Gloster E.1/44
Gloster E1-44 2
TX148, the third prototype on a test flight, c. 1949
Role Fighter
Manufacturer Gloster Aircraft Company
Designer George Carter
First flight 9 March 1948
Retired Cancelled
Primary user Royal Air Force (intended)
Number built 3 (4th prototype not completed)

The Gloster E.1/44 was a British single-engined jet fighter design of the Second World War which came about because of low availability of jet engines but was not completed in prototype form until after the war and never entered production.

Design and development

The success of the first British jet aircraft the Gloster E.28/39 led to the design of the twin-engined Gloster Meteor jet fighter from 1940 onwards. However in 1942 Rover, who were contracted to produce the Whittle W2 jet engine, were having production problems so the Air Ministry issued a Specification, E.5/42, asking for a design which would use only one engine rather than the two. Gloster produced a design for a low-winged monoplane with a highly tapered wing and a T-tail, to be fitted with a tailwheel undercarriage. It was to be powered by a single Halford H.1 or Rolls-Royce Nene engine fed by intakes in the wing roots. Construction began of two GA.1 prototypes began late in 1943.[1][2] In the end Rolls-Royce Limited traded jet engine production (the W2 would become known as the Welland) for Meteor tank engine production with Rover; the supply problem was resolved and the single-engined design was not required. Gloster continued with their design work privately intending to use a Halford H.1 engine instead of the W2/Welland.

In 1944 the Ministry issued a Specification, E.1/44, for an experimental jet aircraft using the new Rolls-Royce Nene engine. Gloster's design to meet this specification was a new design (GA.2), not based on the E.5/42, being significantly larger.[3] Gloster received a contract to build a single prototype, in 1944, with orders for a further three aircraft following in late 1945.[4]

E1-44

Gloster E.1/44 SM809 with original tail unit c. 1944

File:Gloster E1-44.jpg

Gloster E.1/44 TX145 with modified tail unit

The new design was a stressed-skin mid-winged monoplane with, unlike the E5/42, a tricycle landing gear. The tailplane was mounted midway up the rear fuselage, behind the single fin and rudder. The engine was fed from semi-circular intakes ahead of the wing roots, while the wings were, unusually, skinned in difficult to work stainless-steel.[5][6]

Operational history

Progress on the new fighter was slow, with Gloster concentrating on development of the Meteor. The first prototype was not completed until July 1947, and was destroyed in a road accident when being taken to Boscombe Down for flight testing.[7] The first E.1/44 to fly (the second prototype) did so on 9 March 1948 at Boscombe Down flown by Gloster Chief Test Pilot Bill Waterton who was not impressed with its lack of power or poor flying characteristics, dubbing it the "Gormless". The unofficial name never stuck and the prototype did not have an official name, although "Ace" was proposed.[8] Handling was initially poor, with a new tail unit, with a high mounted tailplane being fitted. While this solved the handling problems, performance was still little better than that of the Meteor, and the programme was stopped in 1949 as the aircraft did not have the development potential of the Meteor, with the fourth prototype (TX150) not completed.[9] The revised E.1/44 tail design was, however, carried over to the Meteor, and employed on the Meteor F 8 and later models.[10] The only two aircraft to fly were used as testbeds for a while before being scrapped, one remaining in use until at least 1951.[11]

Variants

GA.1
Single-engined version of the design to meet Air Ministry Specification E.5/42 - two aircraft serial numbers SM801 and SM805, construction abandoned.
GA.2 Ace
Improved variant to meet E.1/44, three built, SM809 was destroyed during transit to Boscombe Down by road and never flew. TX145 was first to fly on 9 March 1948. TX148 with a modified tail first flew in 1949, the tail design was later used on the Gloster Meteor F.8.
GA.3
Pre-production aircraft, serial number TX150, not built.
GA.4
Forty early production aircraft were ordered in two batches in April and July 1946, cancelled and not built.

Specifications (E.1/44)

Data from The British Fighter since 1912 [12]

General characteristics

  • Length: 38 ft 0 in (11.59 m)
  • Wingspan: 36 ft 0 in (10.98 m)
  • Height: 11 ft 8 in (3.56 m)
  • Wing area: 254 ft² (23.6 m²)
  • Empty weight: 8,260 lb (3,755 kg)
  • Loaded weight: 11,470 lb (5,214 kg)
  • Powerplant: 1 × Rolls-Royce Nene II centrifugal flow turbojet, 5,000 lbf (22.3 kN)

Performance

  • Maximum speed: 539 knots (620 mph, 998 km/h)
  • Range: 357 nm (410 mi, 660 km)
  • Service ceiling: 44,000 ft (13,400 m)
  • Climb to 40,000 ft (12,200 m): 12 min 30 sec

Armament

See also

References

Notes
  1. Goulding 1986, p. 146.
  2. James 1971, pp. 306–307.
  3. Goulding 1986, p.151.
  4. Mason 1992, pp. 356–357.
  5. Goulding 1986, pp. 151–152.
  6. James 1971, pp. 307–308.
  7. Goulding 1986, p. 152.
  8. Waterton 1956, p. 12.
  9. James 1971, pp. 309–310.
  10. Goulding 1986, p. 155.
  11. James 1971, p. 310.
  12. Mason 1992, p. 357.
Bibliography
  • Ashley, Glenn. Meteor in Action. Carrollton, Texas: Squadron/Signal Publications Inc., 1995. ISBN 0-89747-332-9.
  • Bowyer, Chaz. Gloster Meteor. London: Ian Allan Ltd., 1985. ISBN 0-7110-1477-9.
  • Buttler, Tony. Gloster Meteor (Warpaint Series No.22). Milton Keynes, Buckinghamshire, United Kingdom: Hall Park Books Ltd., 2001. ISBN 1-85780-230-6.
  • Caruana, Richard J. and Richard A. Franks. The Gloster & AW Meteor. Kingsway, Bedford, United Kingdom: SAM Publications, 2004. ISBN 0-9533465-8-7.
  • Goulding, James. Interceptor: RAF Single-Seat Multi-Gun Fighters. London: Ian Allan, 1986. ISBN 0-7110-1583-X.
  • Green, William and Gordon Swanborough. The Great Book of Fighters. St. Paul, Minnesota: MBI Publishing, 2001. ISBN 0-7603-1194-3.
  • James, Derek N. Gloster Aircraft since 1917. London: Putnam, 1971. ISBN 0-370-00084-6.
  • Jones, Barry. Gloster Meteor. Ramsbury, Marlborough, Wiltshire, United Kingdom: The Crowood Press Ltd., 1998. ISBN 1-86126-162-4.
  • Mason, Francis K. The British Fighter since 1912. Annapolis, Maryland: Naval Institute Press, 1992. ISBN 1-55750-082-7.
  • Waterton, W.A. The Quick and the Dead: The Story of a Chief Test Pilot. London: Muller, 1956.

External links

All or a portion of this article consists of text from Wikipedia, and is therefore Creative Commons Licensed under GFDL.
The original article can be found at Gloster E.1/44 and the edit history here.