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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).
Page of calculations for pedal pressure and front to rear brake ratios.

Identifier  ExFiles\Box 121\1\  scan0373
Date  29th October 1940
  
Rm{William Robotham - Chief Engineer}/MHR.{M. H. Rigby}3/ET.29.10.40 - 2 -

Thus for a 32.2 ft/sec² stop we require a pedal pressure of
12950 / 138.4 = 93.5 lbs. theoretically

or 12950 / 95.3 = 136 lbs. actually.

It will be noticed that the actual front to rear brakes ratio is in each case 1.30. In the case of the all Lockheed system, a ratio of 1.37 has been decided upon, and as the efficiencies of front and rear will be nearly the same, this will in fact be the actual ratio, and should be satisfactory for our project.

Rm{William Robotham - Chief Engineer}/MHR.{M. H. Rigby}
  
  


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