Jump to content

Curtiss XP-62: Difference between revisions

From Wikipedia, the free encyclopedia
Browse history interactively
← Previous edit
Content deleted Content added
VisualWikitext
m Disambiguating links to Fighter (link changed to Fighter aircraft) using DisamAssist.
m infobox cleanup
 
(8 intermediate revisions by 8 users not shown)
Line 1: Line 1:
{{short description|Prototype fighter aircraft}}
{{Inline citations|date=August 2024}}{{short description|Prototype fighter aircraft}}
<!-- This article is a part of [[Wikipedia:WikiProject Aircraft]]. Please see [[Wikipedia:WikiProject Aircraft/page content]] for recommended layout. -->
<!-- This article is a part of [[Wikipedia:WikiProject Aircraft]]. Please see [[Wikipedia:WikiProject Aircraft/page content]] for recommended layout. -->
{|{{Infobox Aircraft Begin
{{Infobox aircraft
| name = XP-62
| name = XP-62
| image = XP-62_-_Ray_Wagner_Collection_Image_(28023153805).jpg
| image = XP-62 - Ray Wagner Collection Image (28023153805).jpg
| caption = A Curtiss-XP-62 on the tarmac
| caption = A Curtiss XP-62 on the tarmac
| type = [[Fighter aircraft|Fighter]] [[Interceptor aircraft|interceptor]]
}}{{Infobox Aircraft Type
| type = [[Fighter aircraft|Fighter]] [[interceptor]]
| manufacturer = [[Curtiss-Wright]]
| manufacturer = [[Curtiss-Wright]]
| designer =
| designer =
| first flight = 21 July 1943
| first_flight = 21 July 1943
| introduced =
| introduction =
| retired =
| retired =
| status = Cancelled 21 September 1943
| status = Cancelled 21 September 1943
| primary user = [[United States Army Air Forces]]
| primary_user = [[United States Army Air Forces]]
| more users =
| more_users =
| produced = 1943
| produced = 1943
| number built = 1
| number_built = 1
| unit cost =
| unit cost =
| variants with their own articles =
| variants =
}}
}}
|}


The '''Curtiss XP-62''' was a [[prototype]] single-engine [[interceptor aircraft]], that was built at the request of the [[United States Army Air Forces]], by the [[Curtiss-Wright Corporation]]. It first flew in 1943.
The '''Curtiss XP-62''' was a [[prototype]] single-engine [[interceptor aircraft]], that was built for the [[United States Army Air Forces]], by the [[Curtiss-Wright Corporation]]. It first flew in 1943.


Relatively unusual objectives of the design, for its time, included superior high-altitude performance, which was to be assisted by a [[pressurized cabin|pressurized cockpit]], heavier armament than contemporary USAAF fighter aircraft, in the form of four 20&nbsp;mm [[autocannon]]s, and higher speeds, at all altitudes, than other contemporary fighters. A key physical feature of the XP-62, in terms of the above objectives, was its relatively large and powerful engine, an 18-cylinder [[Wright R-3350 Duplex-Cyclone]].
The design sought to have an improved high-altitude performance and higher speeds, at all altitudes, which was to be assisted by the 18-cylinder [[Wright R-3350 Duplex-Cyclone]] engine.<ref name=":0" /> It was to be armed with four {{cvt|20|mm}} [[autocannon]]s, a heavier armament than contemporary USAAF fighter aircraft, and was fitted with a [[pressurized cabin|pressurized cockpit]].


==Design and development==
==Design and development==
The terms of the contract, in accordance with a proposal of 29 April 1941, called for the first flight within fifteen months of the award.
The terms of the contract proposal of 29 April 1941 called for the first flight within fifteen months of the award and meet the following objectives.
#Maximum level flight speed at {{cvt|27000|ft}} had to exceed {{cvt|468|mph}}.
#It was to feature an [[Air conditioning|air-conditioned]] [[Cabin pressurization|pressurized]] [[cockpit]].
#Armament to be either eight {{cvt|20|mm}} cannons or twelve {{cvt|0.50|in|1}} machine guns, mounted in the wings.


Two [[prototype]]s were ordered; the first designated '''XP-62''' and the second designated '''XP-62A'''.
The maximum level flight speed at 27,000&nbsp;ft (8,230&nbsp;m) had to be at least 468&nbsp;mph (753&nbsp;km/h).


On 2 August 1941, the specifications were amended for the XP-62, reducing the maximum speed to {{cvt|448|mph}} with eight {{cvt|20|mm}} cannons, and increasing the loaded weight by {{cvt|1537|lb}}.
The aircraft was to feature an [[Air conditioning|air-conditioned]], [[Cabin pressurization|pressurized]] [[cockpit]].


During a project review of 1 January 1942, the specification was again revised, with the loaded weight reduced by eliminating four cannons and removing the [[propeller (aircraft)|propeller]] [[de-icing]] equipment.
Proposed armament was either eight 20&nbsp;mm (.79&nbsp;in) cannons or twelve 0.50&nbsp;in (12.7&nbsp;mm) machine guns, mounted in the wings.


On 25 May 1942 a contract for 100 P-62 fighters was awarded. However, on 27 July 1942, before production could begin, the contract for the P-62 was terminated by the USAAF because of the effect on deliveries of Curtiss-built [[Republic P-47 Thunderbolt|Republic P-47G-CU Thunderbolt]]s.<ref name=":0">{{Cite web |date=2009 |title=Curtiss XP-62 |url=http://www.nationalmuseum.af.mil/factsheets/factsheet.asp?id=2266 |archive-url=https://web.archive.org/web/20121010042055/http://www.nationalmuseum.af.mil/factsheets/factsheet.asp?id=2266 |archive-date=10 October 2012 |access-date=2 September 2024 |website=National Museum of the U.S. Air Force}}</ref>
Two [[prototype]]s were ordered; the first designated '''XP-62''' and the second designated '''XP-62A'''.


While work on the XP-62A continued, it progressed slowly, owing to its low priority. Delays in delivery of the pressure-cabin supercharger and engine modifications delayed the first flight until 21 July 1943. Only a limited amount of flight testing was carried out before the XP-62A was canceled on 21 September 1943 and full performance characteristics were not obtained. The prototype was scrapped in early 1944.
On 2 August 1941, the specifications were submitted for the XP-62 reducing the maximum speed to 448&nbsp;mph (721&nbsp;km/h) with eight 20&nbsp;mm (.79&nbsp;in) cannon armament and increasing the loaded weight by 1,537&nbsp;lb (697&nbsp;kg).


== Variants ==
During a project review of 1 January 1942, the contract specification was again revised: the loaded weight would be reduced by eliminating four cannons and removing the [[propeller (aircraft)|propeller]] [[de-icing]] equipment.
;XP-62

:Prototype, 8 x 20 mm cannons
On 25 May 1942 a contract for 100 P-62 fighters was awarded. However, on 27 July 1942, before production could begin, the contract for the P-62 was terminated (although not, apparently, the XP-62A). The reason given was the effect on deliveries of Curtiss-built [[Republic P-47 Thunderbolt|P-47 Thunderbolt]]s.
;P-62A

:Planned initial production version, 100-aircraft contract cancelled
While work on the XP-62A continued, it progressed slowly, owing to its low priority; delays in delivery of the unique pressure-cabin supercharger and engine modifications delayed the first flight until 21 July 1943. Only a limited amount of flight testing was carried out before the XP-62A was canceled on 21 September 1943 and full performance characteristics were not obtained. In early 1944, the XP-62A prototype was scrapped.


==Specifications (XP-62)==
==Specifications (XP-62)==
Line 49: Line 50:
|ref=Curtiss Aircraft 1907–1947<ref name=Bowers>{{cite book |last1=Bowers |first1=Peter M. |title=Curtiss aircraft, 1907-1947 |date=1979 |publisher=Putnam |location=London |isbn=0370100298 |pages=327–331}}</ref>
|ref=Curtiss Aircraft 1907–1947<ref name=Bowers>{{cite book |last1=Bowers |first1=Peter M. |title=Curtiss aircraft, 1907-1947 |date=1979 |publisher=Putnam |location=London |isbn=0370100298 |pages=327–331}}</ref>
|prime units?=imp
|prime units?=imp
<!--
General characteristics
-->
|crew=1
|crew=1
|length ft=39|length in=6
|capacity=
|length ft=39
|span ft=53|span in=8
|height ft=16|height in=3
|length in=6
|length note=
|span ft=53
|span in=8
|span note=
|height ft=16
|height in=3
|height note=
|wing area sqft=420
|wing area sqft=420
|wing area note=
|aspect ratio=<!-- sailplanes -->
|airfoil='''root:''' [[NACA airfoil|NACA 66-118]]; '''tip:''' [[NACA airfoil|NACA 66-113]]<ref name="Selig">{{cite web |last1=Lednicer |first1=David |title=The Incomplete Guide to Airfoil Usage |url=https://m-selig.ae.illinois.edu/ads/aircraft.html |website=m-selig.ae.illinois.edu |access-date=16 April 2019}}</ref>
|airfoil='''root:''' [[NACA airfoil|NACA 66-118]]; '''tip:''' [[NACA airfoil|NACA 66-113]]<ref name="Selig">{{cite web |last1=Lednicer |first1=David |title=The Incomplete Guide to Airfoil Usage |url=https://m-selig.ae.illinois.edu/ads/aircraft.html |website=m-selig.ae.illinois.edu |access-date=16 April 2019}}</ref>
|empty weight lb=11775
|empty weight lb=11775|gross weight lb=16650
|empty weight note=
|gross weight lb=16650
|gross weight note=
|max takeoff weight lb=
|max takeoff weight note=
|fuel capacity=
|more general=
|more general=
<!--
<!--Powerplant-->
|eng1 number=1|eng1 name=[[Wright R-3350-17 Duplex Cyclone]]|eng1 type=18-cylinder air-cooled radial piston engine|eng1 hp=2300
Powerplant
|prop blade number=6|prop name=contra-rotating constant-speed propeller
-->
|prop dia ft=|prop dia in=
|eng1 number=1
<!-- Performance -->
|eng1 name=[[Wright R-3350-17 Duplex Cyclone]]
|eng1 type=18-cylinder air-cooled radial piston engine
|eng1 hp=2300

|prop blade number=6
|prop name=contra-rotating constant-speed propeller
|prop dia ft=<!-- propeller aircraft -->
|prop dia in=<!-- propeller aircraft -->
|prop dia note=
<!--
Performance
-->
|max speed mph=448
|max speed mph=448
|max speed note=at {{cvt|27000|ft}}
|max speed note=at {{cvt|27000|ft}}
|cruise speed mph=
|cruise speed mph=
|cruise speed note=
|stall speed mph=
|stall speed note=
|never exceed speed mph=
|never exceed speed note=
|range miles=1300
|range miles=1300
|range note=
|combat range miles=
|combat range note=
|ferry range miles=
|ferry range note=
|endurance=<!-- if range unknown -->
|ceiling ft=37500
|ceiling ft=37500
|ceiling note=
|g limits=<!-- aerobatic -->
|roll rate=<!-- aerobatic -->
|glide ratio=<!-- sailplanes -->
|climb rate ftmin=
|climb rate ftmin=
|time to altitude={{cvt|15000|ft}} in 6.9 minutes
|climb rate note=
|time to altitude={{cvt|15,000|ft}} in 6.9 minutes
|wing loading lb/sqft=35
|wing loading lb/sqft=35
|wing loading note=
|wing loading note=
|fuel consumption lb/mi=
|fuel consumption lb/mi=
|power/mass={{cvt|0.16|hp/lb}}
|power/mass={{cvt|0.16|hp/lb}}
<!-- Armament -->
|thrust/weight=
|guns= 8 x {{cvt|20|mm|3}} cannon

|more performance=
<!--
Armament
-->
|guns= 4x {{cvt|20|mm|3}} cannon

|avionics=
}}
}}


Line 146: Line 95:
{{commons category|Curtiss XP-62}}
{{commons category|Curtiss XP-62}}
*[https://web.archive.org/web/20121010042055/http://www.nationalmuseum.af.mil/factsheets/factsheet.asp?id=2266 Curtis XP-62] – National Museum of the USAF
*[https://web.archive.org/web/20121010042055/http://www.nationalmuseum.af.mil/factsheets/factsheet.asp?id=2266 Curtis XP-62] – National Museum of the USAF
*[https://apps.dtic.mil/sti/pdfs/ADA800803.pdf Wind-Tunnel Tests Of The 1/9-Scale Model Of The Curtiss XP-62 Airplane With Various Vertical Tail Arrangements] – [[DTIC]]


{{Curtiss aircraft}}
{{Curtiss aircraft}}
Line 156: Line 106:
[[Category:Aircraft with contra-rotating propellers]]
[[Category:Aircraft with contra-rotating propellers]]
[[Category:Aircraft first flown in 1943]]
[[Category:Aircraft first flown in 1943]]
[[Category:Low-wing aircraft]]
[[Category:Aircraft with retractable conventional landing gear]]
[[Category:Single-engined piston aircraft]]

Latest revision as of 00:24, 14 December 2024

XP-62
A Curtiss XP-62 on the tarmac
General information
TypeFighter interceptor
ManufacturerCurtiss-Wright
StatusCancelled 21 September 1943
Primary userUnited States Army Air Forces
Number built1
History
Manufactured1943
First flight21 July 1943

The Curtiss XP-62 was a prototype single-engine interceptor aircraft, that was built for the United States Army Air Forces, by the Curtiss-Wright Corporation. It first flew in 1943.

The design sought to have an improved high-altitude performance and higher speeds, at all altitudes, which was to be assisted by the 18-cylinder Wright R-3350 Duplex-Cyclone engine.[1] It was to be armed with four 20 mm (0.79 in) autocannons, a heavier armament than contemporary USAAF fighter aircraft, and was fitted with a pressurized cockpit.

Design and development

[edit]

The terms of the contract proposal of 29 April 1941 called for the first flight within fifteen months of the award and meet the following objectives.

  1. Maximum level flight speed at 27,000 ft (8,200 m) had to exceed 468 mph (753 km/h).
  2. It was to feature an air-conditioned pressurized cockpit.
  3. Armament to be either eight 20 mm (0.79 in) cannons or twelve 0.50 in (12.7 mm) machine guns, mounted in the wings.

Two prototypes were ordered; the first designated XP-62 and the second designated XP-62A.

On 2 August 1941, the specifications were amended for the XP-62, reducing the maximum speed to 448 mph (721 km/h) with eight 20 mm (0.79 in) cannons, and increasing the loaded weight by 1,537 lb (697 kg).

During a project review of 1 January 1942, the specification was again revised, with the loaded weight reduced by eliminating four cannons and removing the propeller de-icing equipment.

On 25 May 1942 a contract for 100 P-62 fighters was awarded. However, on 27 July 1942, before production could begin, the contract for the P-62 was terminated by the USAAF because of the effect on deliveries of Curtiss-built Republic P-47G-CU Thunderbolts.[1]

While work on the XP-62A continued, it progressed slowly, owing to its low priority. Delays in delivery of the pressure-cabin supercharger and engine modifications delayed the first flight until 21 July 1943. Only a limited amount of flight testing was carried out before the XP-62A was canceled on 21 September 1943 and full performance characteristics were not obtained. The prototype was scrapped in early 1944.

Variants

[edit]
XP-62
Prototype, 8 x 20 mm cannons
P-62A
Planned initial production version, 100-aircraft contract cancelled

Specifications (XP-62)

[edit]

Data from Curtiss Aircraft 1907–1947[2]

General characteristics

  • Crew: 1
  • Length: 39 ft 6 in (12.04 m)
  • Wingspan: 53 ft 8 in (16.36 m)
  • Height: 16 ft 3 in (4.95 m)
  • Wing area: 420 sq ft (39 m2)
  • Airfoil: root: NACA 66-118; tip: NACA 66-113[3]
  • Empty weight: 11,775 lb (5,341 kg)
  • Gross weight: 16,650 lb (7,552 kg)
  • Powerplant: 1 × Wright R-3350-17 Duplex Cyclone 18-cylinder air-cooled radial piston engine, 2,300 hp (1,700 kW)
  • Propellers: 6-bladed contra-rotating constant-speed propeller

Performance

  • Maximum speed: 448 mph (721 km/h, 389 kn) at 27,000 ft (8,200 m)
  • Range: 1,300 mi (2,100 km, 1,100 nmi)
  • Service ceiling: 37,500 ft (11,400 m)
  • Time to altitude: 15,000 ft (4,600 m) in 6.9 minutes
  • Wing loading: 35 lb/sq ft (170 kg/m2)
  • Power/mass: 0.16 hp/lb (0.26 kW/kg)

Armament

  • Guns: 8 x 20 mm (0.787 in) cannon

See also

[edit]

Related lists

References

[edit]
  1. ^ a b "Curtiss XP-62". National Museum of the U.S. Air Force. 2009. Archived from the original on 10 October 2012. Retrieved 2 September 2024.
  2. ^ Bowers, Peter M. (1979). Curtiss aircraft, 1907-1947. London: Putnam. pp. 327–331. ISBN 0370100298.
  3. ^ Lednicer, David. "The Incomplete Guide to Airfoil Usage". m-selig.ae.illinois.edu. Retrieved 16 April 2019.
  • Green, William. War Planes of the Second World War – Fighters, Volume 4. London: Macdonald. 1961.
[edit]
Wikimedia Commons has media related to Curtiss XP-62.
Retrieved from "https://en.wikipedia.org/enwiki/w/index.php?title=Curtiss_XP-62&oldid=1262980225"