Responding to a previous suggestion about the basis for comparing the Goshawk engine.
| Identifier | Morton\M2.1\ img023 | |
| Date | 8th May 1922 | |
| E. {Mr Elliott - Chief Engineer} from Hs. {Lord Ernest Hives - Chair} Hs {Lord Ernest Hives - Chair} 5/LG1.8.5.22. ORIGINAL X4134 X2585 COMPARISON OF GOSHAWK(Aero Engine)(Codename for 20HP Car / Aero Engine after Kestrel(Aero Engine)). I have just come across your memo. E2/M16.3.22 suggesting that the Goshawk(Aero Engine)(Codename for 20HP Car / Aero Engine after Kestrel(Aero Engine)) should be compared on the basis of engine capacity per ton mile. This memo. evidently arrived when I was in France and I have just unearthed it. Hs. {Lord Ernest Hives - Chair} | ||
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).
