7-cyl air-cooled R engine of geared, dry sump type; bore 3 1/32 in. stroke of 3 27/64 in.; weight with airscrew hub 135-140 lb; max power at 3300 rpm, 85 bhp; weight per hp 1.87 lb; fuel consumption per hr at 0.9 full throttle, 4 1/2 gal. (See also Flight v 24 n 1242 Oct 13 1932 p 955-7, Engineering v 134 n 3488 Nov 18 1932 p 594-5; Aircraft Eng v 4 n 41 July 1932 p 180)
Light-weight radial engine
Aeroplane
Aeroplane ; 43 , n 15
1932
2 pages
Article (Journal)
English
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Engineering Index Backfile | 1932
Emerald Group Publishing | 1932
Radial engine for light aircraft
Engineering Index Backfile | 1932
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Emerald Group Publishing | 1932
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