Vought XSO2U

{{Short description|American observation floatplane}}

{{good article}}

{{Infobox Aircraft Begin

|name = XSO2U-1

|image = File:Vought XSO2U-1.jpg{{!}}border

|caption =

}}{{Infobox Aircraft Type

|type = Observation floatplane

|national origin = United States

|manufacturer = Vought-Sikorsky

|designer =

|first flight = July 1939

|introduced =

|retired = July 1944

|primary user = United States Navy

|more users =

|produced =

|number built = 1

|unit cost =

|developed from= OS2U Kingfisher

|variants with their own articles =

|developed into =

}}

The Vought XSO2U was an American observation floatplane developed by Vought-Sikorsky for the United States Navy during the late 1930s. Intended to replace the Curtiss SOC Seagull in service as a scout aboard cruisers, it proved superior to the Curtiss SO3C in evaluation, but failed to win a production contract due to Vought's lack of manufacturing capacity.

Design and development

In the late 1930s the United States Navy developed a set of specifications for a new scout-observation aircraft to operate from its cruisers in the reconnaissance and gunnery spotting roles. Intended to replace the Curtiss SOC biplane, the requirements included that the aircraft should have folding wings, have a superior range and speed to that of the SOC, and that the new type should be powered by the Ranger V-770 inline engine.Adcock 1991, p.44.

Designs were submitted in response to the Navy's specifications by Vought-Sikorsky and Curtiss-Wright. The Vought design, designated Model 403 by the company, was similar to the company's OS2U Kingfisher, which was then under development to replace the SOC aboard U.S. Navy battleships, but had its monoplane wing moved higher on the fuselage than that of the Kingfisher, and differed in the attachment method used by its single-float landing gear. In addition, the radial engine of the OS2U was replaced by an inline Ranger V-770 in a squared-off cowling.Green 1967, p.162.

Capable of being operated with either the float as a seaplane or with a conventional taildragger undercarriage as a landplane, the XSO2U utilised all-metal construction, with the exception of its control surfaces which were fabric-covered. The wings folded to the rear for storage in a manner similar to that of the Grumman TBF Avenger torpedo bomber, .

The aircraft was capable of performing dive bombing, and could be fitted with a single bomb or depth charge on a hardpoint under each wing for the mission, or for anti-submarine warfare. Gun armament consisted of two M2 Browning machine guns, one mounted in a fixed position firing forwards through the propeller using synchronizer gear, while the other was in a flexible position in the observer's cockpit for rear defense.

Operational history

Assigned the serial number 1440,Baugher 2010 the XSO2U-1 flew for the first time, as a landplane, in July 1939; its first flight as a seaplane took place that December. Flight testing of the SO2U showed that the aircraft lacked directional stability; the addition of a large ventral fin, connecting the rear of the float to the tail, helped to cure the problem.

The aircraft also suffered from engine problems, however, that were not so easily cured; the Ranger engine was well known for unreliability, and was particularly prone to overheating problems that were never satisfactorily solved. The aircraft's original XV-770-4 engine was replaced by a XV-770-6, with a repositioned oil cooler, during flight testing; despite this, the problems continued.

Despite the engine issues, the SO2U-1 was considered overall to be superior to the competing Curtiss XSO3C-1; however, Vought's production capacity was already taken up by manufacture of the OS2U Kingfisher scout and F4U Corsair fighter. As a result, the XSO3C was declared the winner of the contract, and was ordered into production.Bowers 1979, p.419. Named Seagull by the U.S. Navy, and Seamew by the Royal Navy, the SO3C developed a disastrous reputation in service, and was retired before the SOC biplane which it was intended to replace.Polmar 2004, p.117.

Following the end of the flyoff competition, the XSO2U-1 was used as a general utility aircraft and hack by the Navy, before being supplied to the Ranger Engine Corporation in July 1942 for use in tests of the V-770 engine. These tests were intended to assist in debugging the engine for the Bell XP-77 lightweight fighter and Edo XOSE floatplane, but the V-770 remained troublesome, and after two years of testing the XSO2U was returned to the Navy. Having no further use for the aircraft, the XSO2U-1 was removed from the Navy's rolls on 6 July 1944, being subsequently scrapped.

Operators

Specifications (XSO2U-1)

File:Vought XSO2U-1 wheels.jpg

{{Aircraft specs

|ref=OS2U Kingfisher in action

|prime units?=imp

|crew=2 (pilot and observer)

|length m=

|length ft=36

|length in=1

|length note=

|span m=

|span ft=38

|span in=2

|span note=

|height m=

|height ft=15

|height in=11

|height note=

|wing area sqm=

|wing area sqft=300

|wing area note=

|aspect ratio=

|airfoil=

|empty weight kg=

|empty weight lb=4016

|empty weight note=

|gross weight kg=

|gross weight lb=

|gross weight note=

|max takeoff weight kg=

|max takeoff weight lb=5624

|max takeoff weight note=

|fuel capacity={{convert|128|USgal}}

|more general=

|eng1 number=1

|eng1 name=Ranger XV-770

|eng1 type=inline engine

|eng1 kw=

|eng1 hp=450

|eng1 note=

|power original=

|more power=

|prop blade number=2

|prop name=Hamilton Standard constant-speed

|prop dia m=

|prop dia ft=

|prop dia in=

|prop note=

|max speed kmh=

|max speed mph=190

|max speed kts=

|max speed note=at {{convert|9000|ft}}

|cruise speed kmh=

|cruise speed mph=

|cruise speed kts=

|cruise speed note=

|stall speed kmh=

|stall speed mph=

|stall speed kts=

|stall speed note=

|range km=

|range miles=

|range nmi=

|range note=

|combat range km=

|combat range miles=

|combat range nmi=

|combat range note=

|ferry range km=

|ferry range miles=

|ferry range nmi=

|ferry range note=

|endurance=

|ceiling m=

|ceiling ft=22200

|ceiling note=

|g limits=

|roll rate=

|glide ratio=

|climb rate ms=

|climb rate ftmin=

|climb rate note=

|time to altitude=

|lift to drag=

|wing loading kg/m2=

|wing loading lb/sqft=

|wing loading note=

|fuel consumption kg/km=

|fuel consumption lb/mi=

|power/mass=

|more performance=

|guns=2 x M2 Browning machine guns, one fixed forwards-firing, one flexible rear-firing.

|bombs=Two light bombs or depth charges on underwing racks.

|avionics=

}}

See also

References

=Citations=

{{reflist|2}}

=Bibliography=

{{refbegin}}

  • {{cite book |last1=Adcock |first1=Al |title=OS2U Kingfisher in action |series=Aircraft In Action |volume=119 |year=1991 |publisher=Squadron/Signal Publications |location=Carrollton, TX |isbn=0-89747-270-5}}
  • {{cite web |url=http://www.joebaugher.com/navy_serials/secondseries1.html |title=US Navy and US Marine Corps BuNos, Second Series (0001 to 5029) |first=Joe |last=Baugher |author-link=Joe Baugher |date=September 18, 2010 |work=US Navy and US Marine Corps Aircraft Serial Numbers and Bureau Numbers--1911 to Present |access-date=2011-01-12}}
  • {{cite book |last1=Bowers |first1=Peter M. |title=Curtiss Aircraft, 1907-1947 |year=1979 |publisher=Putnam |location=New York |isbn=978-0-370-10029-6}}
  • {{cite book |last1=Green |first1=William |author-link=William Green (author) |title=Floatplanes |series=War Planes of the Second World War |volume=6 |year=1967 |publisher=Doubleday |location=New York |asin=B0000CLL8R }}
  • {{cite book |last1=Polmar |first1=Norman |title=Historic Naval Aircraft: from the pages of Naval History Magazine |year=2004 |publisher=Brassey's Inc |location=Dulles, VA |isbn=1-57488-572-3 |url-access=registration |url=https://archive.org/details/historicnavalair00polm }}

{{refend}}