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Brake test results for a R.R. Goshawk starter motor with brushes fully advanced.


Identifier  ExFiles\Box 35\4\  scan 104
Date  24th February 1922
  
MOTOR FORM 5.
With brushes fully advanced
X.3009 - BRAKE TEST OF STARTER MOTOR.
Date:- 24.2.22
No:- 2
Motor under test:- R.R. Goshawk(Aero Engine)(Codename for 20HP Car / Aero Engine after Kestrel(Aero Engine)).
Dia. of brake wheel:) 10
Weight of pan and portion of rope - 4 lbs. 14 ozs.
Reduction gear ratio:- -
Load in pan (W) | Spr.ng Balance Reading (S) lbs. ozs. | Speed R.P.M. | Amps. | Volts. | W-S (lbs) | T-t (lbs) | Torque (lb-ins) | E.M.F. | B.H.P. | Efficiency.
3 | 1 | 1 | 1344 | 92.0 | 10.16 | Noisy 1 | 15 | 6.81 | 34.1 | .73 | 1.25 | .584
2 | | 12 | 1466 | 86.0 | 10.28 | 1 | 4 | 6.13 | 30.7 | .715 | 1.18 | .606
1 | | 11 | 1640 | 78.0 | 10.44 | 5 | 5.19 | 26.0 | .68 | 1.09 | .624
0 | | 7 | 1820 | 71.0 | 10.58 | -| 4 | 4.40 | 22.0 | .64 | 1.01 | .634
22.2.22.
  
  
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).


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