A rocket of initial mass 8000 kg ejects gases at a constant rate of 16 kg/s with constant relative speed of 10 km/s. The initial thrust on the rocket is

a. 1.6 * 10 ⁵ N
b. 1.6 * 10 ³ N
c. 3.2 * 10 ⁵ N
d. 3.2 * 10 ³ N



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