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, Aeroplane v 43 n 15 Oct 12 1932 p 694 and 696-7 and Engineering v 134 n 3488 Nov 18 1932 p 594-5)
Light-weight radial engine
Aircraft Eng
Aircraft Engineering ; 4 , n 41
1932
Article (Journal)
English
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Engineering Index Backfile | 1932
Engineering Index Backfile | 1932
Engineering Index Backfile | 1932
Emerald Group Publishing | 1932
A Radial Engine for Light Aircraft
Emerald Group Publishing | 1932
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