Question: Project1_Rocket.m X + function sounding_rocket clc; %% constant parameters diam 56; A = pi/4* (diam)^2; Cd= 0.5; g=9.81; Rho 1.225; 2; H initial 0; H
Project1_Rocket.m X + function sounding_rocket clc; %% constant parameters diam 56; A = pi/4* (diam)^2; Cd= 0.5; g=9.81; Rho 1.225; 2; H initial 0; H max = 130; m0 = 2200; m ratio m0/mfinal; gamma 1.3; 5- R = 287: 6 T_exit 2125; 17 Isp = sqrt (gamma*R*T_exit) 18 - P_O = 50.75; 19 T= (-131 + 0.00299 * (H max = - - H initial)) :
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