Is of two-cylinder opposed type and has total cylinder capacity of just under 1100 cc.; bore 3.35 in., stroke 3.80 in., pistol displacement 66.8 cu. in., normal output 22 b.hp. at 2500 r.p.m.
The new Bristol Cherub
Aeroplane
Aeroplane ; 26 , n 23
1924
3 Figs.
Article (Journal)
English
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The bristol "cherub" flat twin aero engine
Engineering Index Backfile | 1923
The Bristol "cherub" flat twin aero engine
Engineering Index Backfile | 1923
The bristol "cherub" flat twin aero engine
Engineering Index Backfile | 1923
Bristol. The Bristol Aeroplane Co., Ltd.
Engineering Index Backfile | 1928
Emerald Group Publishing | 2005
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