Consider the vertical motion of a rocket. Initially, itsaltitude, velocity, and mass are 0.0 m, 0.0 m/s, and m0 kg,respectively. After it is launched, the rocket has altitude ( h ),velocity ( v ), and mass ( m ) .
Note:
1. the rate of fuel consumption phi is a non-zero constant (phi0 ) before the fuel is completely burned, and zeroafterward.
2. The rocket carries a parachute which is programmed to deployat time t1. The value of drag coefficient c_d is cd_0 before timet1, and increases to cd_1 afterwards.
Complete the following flow chart by filling the missing partswith the appropriate task numbers.
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