From the Rolls-Royce experimental archive: a quarter of a million communications from Rolls-Royce, 1906 to 1960's. Documents from the Sir Henry Royce Memorial Foundation (SHRMF).
Altitude power curve graph for an M.S. engine at 2400 RPM.
| Identifier | ExFiles\Box 36\2\ scan 219 | |
| Date | 6th May 1929 | |
| 2400 RPM TYPE TEST ALTITUDE POWER CURVE FOR RATING M.S. ENGINE AT 2400 R.P.M. ENGINE FXIV-MS-13 5.5/1 COMP. RATIO FUEL SHELL 80/20 AVIATION/BENZOLE PLUGS LODGE A 40 CAMS TO C306B1 I.C. 40° A.B.D.C. MAGS. F.A. 40° B.T.D.C. WATER HEATED CARB, VARIABLE JETS RATING FOUND TO BE 525 B.H.P AT 4,000 FT. C/B HP FULL CORRECTED POWER ALTITUDE FT 525 B.H.P AT 4,225 FT. 6529 | ||