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. (see also similar description in Flight v 27 n 1366 Feb 28 1935 p 218-9)
Cirrus minor
Aeroplane
Aeroplane ; 48 , n 1240
1935
3 pages
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Engineering Index Backfile | 1935
Engineering Index Backfile | 1945
Engineering Index Backfile | 1945
Engineering Index Backfile | 1945
Engineering Index Backfile | 1945