Curtiss XP-62: Difference between revisions
Content deleted Content added
mNo edit summary |
grammar, and added cvt conversions |
||
| (64 intermediate revisions by 53 users not shown) | |||
| Line 1: | Line 1: | ||
{{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 |
||
| name = XP-62 |
|||
| image = XP-62_-_Ray_Wagner_Collection_Image_(28023153805).jpg |
|||
|type =Fighter |
|||
| caption = A Curtiss-XP-62 on the tarmac |
|||
}}{{Infobox Aircraft Type |
|||
|image =image:Curtiss XP-62.jpg |
|||
| type = [[Fighter aircraft|Fighter]] [[Interceptor aircraft|interceptor]] |
|||
|caption = |
|||
| manufacturer = [[Curtiss-Wright]] |
|||
|designer = |
|||
| designer = |
|||
|first flight =[[1943-07-21]] |
|||
| first flight = 21 July 1943 |
|||
|introduced = |
|||
| introduced = |
|||
|retired = |
|||
| retired = |
|||
|status =Cancelled [[1943-09-21]] |
|||
| status = Cancelled 21 September 1943 |
|||
|primary user = |
|||
| primary user = [[United States Army Air Forces]] |
|||
|more users = |
|||
| more users = |
|||
| produced = 1943 |
|||
|number built =1 |
|||
| number built = 1 |
|||
|unit cost = |
|||
|variants with their own articles = |
| unit cost = |
||
| variants with their own articles = |
|||
}} |
}} |
||
|} |
|||
The ''' |
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. 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]]. |
|||
On [[August 2]], 1941, the specifications were submitted for the XP-62 reducing the maximum speed to 448 mph with eight cannon armament and increasing the loaded weight by 1,537 lb. During a project review of [[January 1]], [[1942 in aviation|1942]] under findings of a study that the loaded weight be reduced by eliminating four cannon and removal of the [[propeller]] anti-icing equipment. On [[May 25]], 1942 a contract for 100 P-62 fighters was awarded, but on [[July 27]], 1942 the contract was terminated as it would affect deliveries of urgently needed Curtiss-built [[P-47 Thunderbolts]]. |
|||
Delays in delivery of the unique pressure-cabin supercharger and engine modifications delayed the first flight of the XP-62 until [[July 21]], [[1943 in aviation|1943]]. The XP-62A was canceled on [[September 21]], 1943 and only a limited amount of flight testing was conducted with the XP-62. Owing to its low priority work progressed slowly and in the autumn [[1944 in aviation|1942]] the XP-62 was scrapped. Because of the insuffucient flight testing, full performance charactistics were not obtained. |
|||
==Design and development== |
|||
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'''. |
|||
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}}. |
|||
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. |
|||
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) because of the effect on deliveries of Curtiss-built [[Republic P-47 Thunderbolt]]s. |
|||
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. |
|||
==Specifications (XP-62)== |
==Specifications (XP-62)== |
||
{{Aircraft |
{{Aircraft specs |
||
|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> |
|||
<!-- if you do not understand how to use this template, please ask at [[Wikipedia talk:WikiProject Aircraft]] --> |
|||
|prime units?=imp |
|||
<!-- please answer the following questions --> |
|||
|crew=1 |
|||
|plane or copter?=plane |
|||
|length ft=39|length in=6 |
|||
|jet or prop?=prop |
|||
|span ft=53|span in=8 |
|||
<!-- 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 |ref=, |more general=, |more performance=, |power original=, and |thrust original= see [[Template talk:Aircraft specification]]. --> |
|||
|height ft=16|height in=3 |
|||
|crew=One |
|||
|wing area sqft=420 |
|||
|length main=39 ft 6 in |
|||
|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> |
|||
|length alt=12.04 m |
|||
|empty weight lb=11775|gross weight lb=16650 |
|||
|span main=53 ft 8 in |
|||
|span alt=16.36 m |
|||
|height main=16 ft 3 in |
|||
|height alt=4.95 m |
|||
|area main=420 ft² |
|||
|area alt=39.0 m² |
|||
|empty weight main=11,773 lb |
|||
|empty weight alt=5,340 kg |
|||
|loaded weight main=14,660 lb |
|||
|loaded weight alt=6,650 kg |
|||
|max takeoff weight main=16,651 lb |
|||
|max takeoff weight alt=7,553 kg |
|||
|more general= |
|more general= |
||
<!--Powerplant--> |
|||
|engine (prop)=[[Wright R-3350]]-17 |
|||
|eng1 number=1|eng1 name=[[Wright R-3350-17 Duplex Cyclone]]|eng1 type=18-cylinder air-cooled radial piston engine|eng1 hp=2300 |
|||
|type of prop=[[radial engine]] |
|||
|prop blade number=6|prop name=contra-rotating constant-speed propeller |
|||
|number of props=1 |
|||
|prop dia ft=|prop dia in= |
|||
|power main=2,300 hp |
|||
<!-- Performance --> |
|||
|power alt=1,716 kW |
|||
|max speed |
|max speed mph=448 |
||
|max speed |
|max speed note=at {{cvt|27000|ft}} |
||
|cruise speed mph= |
|||
|range main=1,500 mi |
|||
|range |
|range miles=1300 |
||
|ceiling |
|ceiling ft=37500 |
||
|climb rate ftmin= |
|||
|ceiling alt=10,884 m |
|||
|time to altitude={{cvt|15000|ft}} in 6.9 minutes |
|||
|climb rate main= |
|||
|wing loading lb/sqft=35 |
|||
|climb rate alt= |
|||
|loading |
|wing loading note= |
||
|fuel consumption lb/mi= |
|||
|loading alt=171 kg/m² |
|||
|power/mass |
|power/mass={{cvt|0.16|hp/lb}} |
||
<!-- Armament --> |
|||
|power/mass alt=0.26 kW/kg |
|||
|guns= 8 x {{cvt|20|mm|3}} cannon |
|||
|more performance= |
|||
* 4x 20 mm cannon |
|||
}} |
}} |
||
== |
==See also== |
||
{{Portal|Aviation}} |
|||
* Green, William (1961). ''War Planes of the Second World War - Fighters'' (Vol 4). London: Macdonald. |
|||
{{aircontent |
|||
==External link== |
|||
*[http://www.wpafb.af.mil/museum/research/p62.htm XP-62 information, including a picture] (from USAF Museum) |
|||
==Related content== |
|||
{{aircontent| |
|||
|related= |
|related= |
||
|similar aircraft= |
|similar aircraft= |
||
|lists= |
|||
* [[List of fighter aircraft]] |
|||
* [[List of military aircraft of the United States]] |
|||
}} |
|||
==References== |
|||
|sequence= |
|||
{{reflist}} |
|||
[[P-59 Airacomet|P-59]] - |
|||
* Green, William. ''War Planes of the Second World War – Fighters, Volume 4''. London: Macdonald. 1961. |
|||
[[Curtiss P-60|P-60]] - |
|||
[[P-61 Black Widow|P-61]] - |
|||
'''XP-62''' - |
|||
[[P-63 Kingcobra|P-63]] - |
|||
[[North American P-64|P-64]] - |
|||
[[Grumman XP-65|XP-65]] |
|||
==External links== |
|||
}} |
|||
{{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 |
|||
{{Curtiss aircraft}} |
|||
[[Category:U.S. fighter aircraft 1940-1949|P-62]] |
|||
{{USAF fighters}} |
|||
{{DEFAULTSORT:Curtiss Xp-62}} |
|||
[[ja:XP-62 (航空機)]] |
|||
[[Category:1940s United States fighter aircraft|Curtiss P-62]] |
|||
[[Category:Single-engined tractor aircraft]] |
|||
[[Category:Curtiss aircraft|P-62]] |
|||
[[Category:Aircraft with contra-rotating propellers]] |
|||
[[Category:Aircraft first flown in 1943]] |
|||
Latest revision as of 09:32, 13 March 2024
| XP-62 | |
|---|---|
.jpg)
| |
| A Curtiss-XP-62 on the tarmac | |
| Role | Fighter interceptor |
| Manufacturer | Curtiss-Wright |
| First flight | 21 July 1943 |
| Status | Cancelled 21 September 1943 |
| Primary user | United States Army Air Forces |
| Produced | 1943 |
| Number built | 1 |
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. 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.
- Maximum level flight speed at 27,000 ft (8,200 m) had to exceed 468 mph (753 km/h).
- It was to feature an air-conditioned pressurized cockpit.
- 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 (although not, apparently, the XP-62A) because of the effect on deliveries of Curtiss-built Republic P-47 Thunderbolts.
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.
Specifications (XP-62)[edit]
Data from Curtiss Aircraft 1907–1947[1]
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[2]
- 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]
- ^ Bowers, Peter M. (1979). Curtiss aircraft, 1907-1947. London: Putnam. pp. 327–331. ISBN 0370100298.
- ^ 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.
External links[edit]
Wikimedia Commons has media related to Curtiss XP-62.
- Curtis XP-62 – National Museum of the USAF