PWS-1
| {{Infobox aircraft begin
| name = PWS-1 | image = PWS-1.jpg | caption = PWS-1 }}{{Infobox aircraft type | type = Fighter aircraft | manufacturer = Podlaska Wytwórnia Samolotów | designer = Zbysław Ciołkosz, Aleksander Grzędzielski | first flight = 25 April 1927 | introduced = | retired = 1929 | status = prototype | primary user = Polish Air Force | more users = | produced = | number built = 1 | unit cost = | variants with their own articles = }} |
The PWS-1 was a Polish two-seat fighter and reconnaissance aircraft constructed by Podlaska Wytwórnia Samolotów (PWS) in 1927. It remained a prototype for its entire lifespan.
Design and development
The PWS-1 was the first aircraft design produced by the Podlaska Wytwórnia Samolotów (Podlasie Aircraft Factory), and the second aircraft designed and built in Poland, after the CWL WZ-X. It was conceived as a single-engine high-wing two-seat fighter whose main purpose was to escort bombers. The design was produced in 1926 by Zbysław Ciołkosz and Aleksander Grzędzielski under the direction of Stanisław Cywiński.
After static testing, the prototype first flew on 25 April 1927 in Biała Podlaska. Although it had STOL capability, its maximum speed and maneuverability were low due to its thick wings.
In 1928, the aircraft was reworked, receiving a new lighter-weight, straight wing with a thinner profile and duralumin construction instead of a wooden, slightly swept one. It also received a large rectangular vertical stabilizer with a rounded top. After these modifications were made, the plane was again tested in early 1929 under the designation PWS-1bis. Its performance improved, but because of its relatively low speed compared to other fighters, its primary role was changed to reconnaissance. However, development was discontinued because the plane had a small payload and Poland had recently bought a large number of better Breguet 19 and Potez 25 reconnaissance and bomber aircraft.
Description
The PWS-1 was a high-wing parasol braced monoplane of mixed construction, featuring a single engine. It sported a fuselage with a steel frame in front and wooden frame in the rear covered with canvas and duralumin in the engine section. Its wing was slightly swept, two spar, and wooden, and was covered with plywood and canvas. The PWS-1bis had a straight, trapezoidal duralumin wing that was two-spar and also covered with plywood and canvas.
Both versions featured wooden stabilizers, rudders and elevators, all covered in canvas, and an open pilot's cab with a windshield. Behind the pilot's cab was an open observer's cab with two 7.7 mm Lewis machine guns on a ring mount. The two cabs featured twin controls. The pilot manned two 7.7 mm Vickers machine guns fixed in the fuselage through an interrupter gear. The plane featured a conventional fixed landing gear with a rear skid.
The PWS-1's engine was a Lorraine-Dietrich 12Eb water-cooled inline W-12 built in the Polish Skoda Works. The water radiator was located in front of the engine.
Acceleration was provided through a two-blade wooden propeller of a fixed pitch.
A 375-liter fuel tank was located in the front fuselage. It could be jettisoned in an emergency situation.
Specifications (PWS 1bis)
{{Aircraft specs
|ref=Jane's all the World's Aircraft 1928,{{cite book |title=Jane's all the World's Aircraft 1928 |editor1-last=Grey |editor1-first=C.G. |year=1928 |publisher=Sampson Low, Marston & company, ltd |location=London |pages=179c}} Polish Aircraft 1893–1939{{cite book |last=Cynk |first=Jerzy B. |title=Polish Aircraft 1893–1939 |year=1971 |publisher=Putnam |location=London |isbn=978-0-370-00085-5 |url-access=registration |url=https://archive.org/details/polishaircraft1800cynk }}
|prime units?=met
|crew=2
|length m=8.375
|span m=12.65
|height m=3.34
|wing area sqm=30.5
|aspect ratio=
|airfoil=Bobek-Zdanewski No.4 (Göttingen 648)
|empty weight kg=1445
|gross weight kg=1990
|max takeoff weight kg=
|max takeoff weight lb=
|max takeoff weight note=
|fuel capacity={{cvt|375|L|USgal impgal}}
|more general=
|eng1 number=1
|eng1 name=Lorraine-Dietrich 12Eb
|eng1 type=W-12 water-cooled piston engine
|eng1 hp=450
|prop blade number=2
|prop name=wooden fixed pitch propeller
|prop dia m=
|prop dia ft=
|prop dia in=
|prop dia note=
|max speed kmh=232
|max speed note=at sea level; {{cvt|210|km/h|mph kn}} at {{cvt|5000|m}}
- Landing speed:{{cvt|98|km/h|mph kn}}
|cruise speed kmh=
|cruise speed mph=
|cruise speed kts=
|cruise speed note=
|stall speed kmh=
|stall speed mph=
|stall speed kts=
|stall speed note=
|never exceed speed kmh=
|never exceed speed mph=
|never exceed speed kts=
|never exceed speed note=
|range km=750
|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=6000
|ceiling note= at normal weight
|g limits=
|roll rate=
|climb rate ms=5.4
|time to altitude={{cvt|1000|m}} in 3 minutes 25 seconds; {{cvt|3000|m}} in 13 minutes
|wing loading kg/m2=65.4
|fuel consumption kg/km=
|fuel consumption lb/mi=
|power/mass={{cvt|0.1031|hp/lb|kW/kg}}
|more performance=
|armament= 2 x fixed forward firing synchronised {{cvt|7.7|mm|3}} Vickers machine guns; 2 x flexibly mounted {{cvt|7.7|mm|3}} Lewis machine guns in the rear cockpit
}}
References
{{Reflist}}
- Andrzej Glass: "Polskie konstrukcje lotnicze 1893-1939" (Polish aviation constructions 1893-1939), WKiŁ, Warsaw 1977 (Polish language, no ISBN)
External links
{{commons category|PWS-1}}
- [http://www.airwar.ru/enc/fww1/pws1.html Photos and drawings at Ugolok Neba]
{{PWS aircraft}}
Category:1920s Polish fighter aircraft
Category:1920s Polish military reconnaissance aircraft
Category:Single-engined tractor aircraft