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).
Required carburetter, compression, and fuel consumption specifications for 200 HP Aero Engines.
| Identifier | ExFiles\Box 121\3\ scan0022 | |
| Date | 26th February 1915 | |
| C O P Y. To E.{Mr Elliott - Chief Engineer} from R.{Sir Henry Royce} Copy to J.{Mr Johnson W.M.} " " Na.{Mr Nadin} Hives 23/5. R2/IB26215. February 26th. 1915. COPY Re 200 HP Aero Engines. From recent tests it appears that we shall require to have a 36 m/m carburetter and a compression of not less than 80 lbs to enable the aero engine to do its full horse power, and to get a consumption of between .5 and .55 lbs. of fuel per horse power hour. R.{Sir Henry Royce} 452. DICKINSON BOND | ||