60-hp. 4-cylinder inverted air-cooled Hirth with coil-ignition; bore, 15 in.; stroke, 4 1/2 in.; maximum permissible power 65 hp. at 2100 r.p.m.; weight 181 lb.; fuel consumption 0.495 lb./hp./hr.; oil consumption, 0.025 lz./hp./hr.
New light aeroplane engine
Aircraft Eng
Aircraft Engineering ; 3 , n 31
1931
3 Figs.
Aufsatz (Zeitschrift)
Englisch
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Light aeroplane engine development
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