Warner Scarab Junior
{{short description|1930s American piston aircraft engine}}
| {{Infobox Aircraft Begin
|name= Scarab Junior |image = |caption = }} {{Infobox Aircraft Engine |type= Radial engine |national origin = |manufacturer= Warner Aircraft Corporation |first run= November 1930 |major applications= |number built = |program cost = |unit cost = |developed from = Warner Scarab |developed into = |variants with their own articles = }} |
The Warner Scarab Junior was an American, five-cylinder, air-cooled, radial aero engine first produced in 1930. It was a scaled-down derivative of the seven-cylinder Warner Scarab, developing 90 hp (70 kW) against the Scarab's 110 hp (80 kW).
Applications
Specifications (Warner Scarab Junior 50)
{{pistonspecs
|
|ref=FAA Type Certificate Data Sheet (TCDS).[http://rgl.faa.gov/Regulatory_and_Guidance_Library/rgMakeModel.nsf/0/73064f41b13b15bd8625764200609230/$FILE/e-54.pdf FAA TCDS - E-54] Retrieved: November 19, 2010.]
|type=Five-cylinder, air-cooled, radial piston engine
|bore=4.25 in (108 mm)
|stroke=4.25 (108 mm)
|displacement=301 cu in (4.93 L)
|length=14 in (35.5 cm)
|diameter=
|width=
|height=36.5 in (93 cm)
|weight=237 lb (107.5 kg)
|valvetrain=1 inlet and 1 exhaust valve per cylinder
|supercharger=
|turbocharger=
|fuelsystem=1 Holley carburetor
|oilsystem=
|coolingsystem=
|power=90 hp (67 kW) at 2,050 rpm
|specpower=
|compression=5.2:1
|fuelcon=
|specfuelcon=
|oilcon=
|power/weight=0.38 hp/lb (0.62 kW/kg)
}}
See also
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|related=
|similar aircraft=
|lists=
|similar engines=
}}
References
{{reflist}}
- Gunston, Bill. (1986). World Encyclopaedia of Aero Engines. Patrick Stephens: Wellingborough. p. 169
- [http://www.oldengine.org/members/diesel/Duxford/usaero13.htm Oldengine.org - US Aero engines page]
{{Warner Aircraft Corporation aeroengines}}