Request for information on the capacity and construction of a Delco Packard condenser for the Goshawk II engine.
| Identifier | ExFiles\Box 34\1\ Scan247 | |
| Date | 28th May 1921 | |
| X 2512 To E C. from E. {Mr Elliott - Chief Engineer} c. to CJ. c. to Wor. {Arthur Wormald - General Works Manager} c. to Hs. {Lord Ernest Hives - Chair} E2/G28.5.21. X.4284 - RE GOSHAWK(Aero Engine)(Codename for 20HP Car / Aero Engine after Kestrel(Aero Engine)) II CONDENSER FOR BATTERY IGNITION. X.2512. In connection with the above, would you please find out, in accordance with Mr. Royce's wishes, what is the capacity of the Delco Packard condenser, and how is it constructed, particularly in what manner the connections are made to the timfoil. E. {Mr Elliott - Chief Engineer} | ||
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).