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

{{aircontent|

|related=

|similar aircraft=

|lists=

|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}}