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Development of the Junkers-diesel Aircraft Engine (1930)

NASA Technical Reports Server (NTRS) · leaf 21

An illustration from Development of the Junkers-diesel Aircraft Engine, 1930, leaf 21
Technical Memorandum No. 565 Fige. 1,2,3,6,7,8,12 * 16 … "F03n 1916 Beniine- Two - s froke - cycle Four- s fro he -cycle injeotion,capsule- double"piston engine volve engine explosion^ cylin- Like displacement der ; diam .115 mm Like r.p.m. stroke 150 mm n 1800,Ne-450 hp ■ K*/m*r> Volume Weight 750 kg. Exhaus 1 side Scavenging side Fi g • 8 Com-…

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