4-cyl in-line, air-cooled, direct-drive engine; 95 mm bore; 127 mm stroke; normal bhp 70 at 2400 rpm; weight 210 lb; fuel consumption 0.54 pt per hp-hr at normal rpm. (Similar description) (See also - Aeroplane v 48 n 1240 Feb 27 1935 p 241-3)
Cirrus minor
Flight
Flight ; 27 , n 1366
1935
2 pages
Article (Journal)
English
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Engineering Index Backfile | 1935
Engineering Index Backfile | 1945
Engineering Index Backfile | 1945
Engineering Index Backfile | 1945
Engineering Index Backfile | 1945