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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).
Proposed tests on the Phantom II's cooling system and fuel supply.

Identifier  WestWitteringFiles\U\May1930-July1930\  Scan131
Date  2nd July 1930 guessed
  
-7- He/28.1/A.L.R.L.H.D.Contd.

the minimum quantity of fuel under the bonnet and at the
same time to provide a greater margin between delivery and
consumption than at present. Next to the autovac, we
consider the needle valve in the float chamber is the limiting
factor in the supply.

Having explored the high speed cooling of the Phantom II
we propose to do some tests to reproduce hill climbing at
30 M.P.H. the method used being similar to that adopted on
Phantom I.

We shall also test the square tube radiator and try a
test moving the radiator further forward to give the air a
chance to get away past the shock absorbers and crankcase.


Hs{Lord Ernest Hives - Chair}/Su.
  
  


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