RWD 10
{{Short description|Polish aerobatics sports plane}}
{{Infobox aircraft
|name =RWD-10
|image =RWD 10.jpg
|caption =
|type =Aerobatics plane
|manufacturer =DWL
|designer = RWD team
|first_flight =July 1933
|introduction =1935
|retired =1939
|status =
|primary_user =Poland
|more_users =
|produced =1937-1938
|number_built =~22+1
|unit cost =
|variants =
}}
The RWD-10 was a Polish aerobatics sports plane, single-seat parasol wing monoplane, used from 1933 to 1939 and constructed by the RWD team.
Development
The aircraft was designed as a single-seater aerobatic sports plane that could also be used as a trainer for fighter pilots. Its chief designer was Jerzy Drzewiecki of the RWD design team at the DWL (Doświadczalne Warsztaty Lotnicze) aircraft factory. Its silhouette was similar to the RWD-8. The first prototype (registration SP-ALC), was flown in July 1933 by Drzewiecki. Its stability was not satisfactory, but after modifications, including lengthening of the fuselage, it turned out to be a successful design, completing state trials in 1935. In a mock dogfight with the PZL P.11c fighter, the RWD-10 kept on the P.11's tail. The first public aerobatics show of the RWD-10 took place during the Gordon Bennett Cup in ballooning on September 14–15, 1935 in Warsaw.
In 1936, the LOPP paramilitary organization ordered 20 aircraft, the purchase funded by a public collection for aviation development. They were built in 1937 and then distributed among the Polish regional aero clubs - the largest number going to the Warsaw Aero Club. In 1938, another two were built. In total, approximately 22 serial RWD-10s were produced.
Three aircraft crashed before the war, the rest were probably destroyed during the Invasion of Poland in 1939.{{citation needed|date=January 2018}}
Description
Mixed construction single-engine single-seat braced high-wing (parasol wing) monoplane, conventional in layout. Fuselage of a steel frame, covered with canvas on a wooden frame, in aluminum in engine section. Straight double-trapezoid two-part wing, of wooden construction, covered with canvas and plywood in front, two-spar. The wing was supported by a central pyramid and twin struts. Wooden construction cantilever empennage, covered with plywood (stabilizers) and canvas (rudder and elevators). A pilot in an open cockpit, had a windshield. Conventional fixed landing gear, with a rear skid. Four-cylinder air-cooled inverted straight engine PZInż. Junior (licence built Walter Junior) with 82 kW (110 hp) nominal power and 90 kW (120 hp) take-off power. Two-blade wooden propeller Szomański, of a fixed pitch. Fuel tank in the fuselage: 54 L (fuel consumption 25 L/h).
Specifications (RWD-10)
{{Aircraft specs
|ref=Polish aircraft 1893-1939{{cite book |last1=Cynk |first1=Jerzy B |title=Polish aircraft 1893-1939 |publisher=Putnam |date=1971 |isbn=0-370-00085-4 |pages=[https://archive.org/details/polishaircraft1800cynk/page/530 530-534] |url=https://archive.org/details/polishaircraft1800cynk/page/530 }}
|prime units?=met
|crew=1
|length m=6.2
|length note=
|span m=7.5
|span note=
|height m=1.9
|height note=
|wing area sqm=9
|wing area note=
|aspect ratio=
|airfoil=
|empty weight kg=350
|empty weight note=
|gross weight kg=4775
|gross weight note=
|max takeoff weight kg=
|max takeoff weight note=
|fuel capacity={{cvt|54|L|USgal impgal}}
|more general=
|eng1 number=1
|eng1 name=PZ Inż. Junior
|eng1 type= 4-cylinder air-cooled inverted in-line piston engine
|eng1 kw=90
|eng1 note=
|prop blade number=2
|prop name=Szomański fixed pitch propeller
|prop dia m=
|prop dia note=
|max speed kmh=230
|max speed note=at sea level
|cruise speed kmh=180
|cruise speed note={{citation needed|date=September 2019}}
- Landing speed: {{cvt|95|km/h|mph kn}}
|stall speed kmh=
|stall speed note=
|never exceed speed kmh=
|never exceed speed note=
|range km=400
|range note=
|ferry range km=
|ferry range note=
|endurance=
|ceiling m=6000
|ceiling note=
|g limits=
|roll rate=
|climb rate ms=6.2
|climb rate note={{citation needed|date=September 2019}}
|time to altitude={{cvt|1000|m}} in 2 minutes 55 seconds
|wing loading kg/m2=52.8
|wing loading note=
|fuel consumption kg/km=
|power/mass={{cvt|0.105|hp/lb|order=flip}}
|more performance=
- Take-off run: {{cvt|67|m}}
- Landing run: {{cvt|100|m}}{{citation needed|date=September 2019}}
|avionics=
}}
See also
References
{{Reflist}}
Further reading
- {{cite book|last1=Glass|first1=Andrzej|title=Polskie konstrukcje lotnicze 1893–1939|date=1977|publisher=WKiŁ|location=Warsaw|language=pl}}
External links
{{commons category|RWD 10}}
- [http://www.airwar.ru/enc/other2/rwd10.html Photos and drawings at Ugolok Neba site]
{{RWD aircraft}}
Category:1930s Polish sport aircraft
Category:Parasol-wing aircraft
Category:Single-engined tractor aircraft
Category:Aircraft first flown in 1933