Elements Of Electromagnetics
7th Edition
ISBN: 9780190698614
Author: Sadiku, Matthew N. O.
Publisher: Oxford University Press
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The following data are given for a certain rocket unit: Thrust, 8000 N Propellant weight flow rate, 36 N/sec Speed of rocket, 800 m/s internal efficiency
32%
combustion efficiency 97 %
Determine (a) the effective velocity; (b) total kinetic energy per second (c) calorific value of propellant (d) the propulsive efficiency (e) the overall efficiency (f) the specific impulse (g) the specific propellant consumption
????? =1/3 ?(?^2) h
V cylinder = ?(?^2) h
V frustrum = 1/3 ?ℎ(?^2 +?^2 +? ×?)
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