Experiments to determine the correct proportions for Goshawk engine carburettor throats.
| Identifier | ExFiles\Box 5\4\ 04-page005 | |
| Date | 17th December 1920 | |
| X 3582 To - De/Stt, from Ha/TMW. c. to RH. {R. Hollingworth} c. to HED. c. to EWE. Ha/TMW2/LGC.18.20. X 3582 GOSHAWK(Aero Engine)(Codename for 20HP Car / Aero Engine after Kestrel(Aero Engine)) ENGINE - CARBURETTOR THROATS. De/Stt1/CBT.12.20. Referring to your note ref: above, please note, that contrary to your statement that the throats you refer to are satisfactory, we are at present experimenting with a view to finding out the correct proportions, when we will at once advise you of the diameter of the throats. Ha/TMW. RECEIVED 17 DEC 1920 | ||
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).