Mathematical Modeling, Mathematical Optimization, Numerical Methods, Numerical Computation, Astrophysics.
ROCKET EQUATIONS IV for clarity) $(0.05–0.002t)\frac{dv}{dt}+v(-0.02v)=14.51+0.196t-0.002v²$\\ $\frac{dv}{dt}=\frac{14.51+0.196t-0.02v²+0.002v}{0.05–0.002t}$\\ We set up the initial conditions: $v(t_{0})=v_{0}$ $v(0)=0$ \Delta t =0.01\\; Manual Implementation of Euler method in Rocket equation: