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Aviation History
1935
1935 - 1407.PDF
JUNE 13, 1935. ADVERTISEMENTS. FLIGHT. 7 PERFORMANCE DATA MK.V. (P.F.) Normal engine R.P.M. ... 2100 Maximum engine R.P.M. ... 2400 B.H.P. for take-off at sea level at normal speed ... 270 at full throttle Rated output at normal R.P.M. 270 at sea level B.H.P. at maximum R.P.M. - 303 at sea level Fuel specification - D.T.D. 224 Minimum octane value - - - - 77 " JMGT'C v^A ^^BP ' '•-"» MK.VI. (G.F.) 2100 2300 307 at max. perm, boost 290 at 6000' 321 at 7000' D.T.D. 224 77 330 320 310 290 280 210 gac £ 250 i 240 2 230 !jj 220 ™ 210 20D 190 180 no ISO ISO CHEETAH MK21H ENGINES. PDWER- ALTITUDE CURVES AT MAXIMUM SPEEDS 6-J -i \ ;\K. i, \ t' <-. 6 s 1 § NQT t" 3H^J [UU • TH|iOTT LE \ r-|- Lt" r-n M D 1 2 3 4 5 6 T 8 9 10 II 12 13 14 15 ALTITUDE (ThousftNB rtci) In ARMSTRONG SIDDELEY MOTORS LTD., COVENTRY, ENGLAND AS 130 Kindly mention " Flight " when corresponding with advertisers.
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