Please show all your steps and calculations.
2-1): The upward velocity of a rocket can be computed be the following formula: mo mo - qt where ...
PLEASE ALSO SOLVE USING THE SIMPSONS 1/3RULE.PLEASE DONT ATTEMPT THE QUESTION IF YOU CANT SOLVE BOTH GUASS AND SIMPSONS Q2. The upward velocity of a rocket can be computed by the following formula: mo v= uln gt gt mo where v= upward velocity, velocity at which fuel is expelled relative to the rocket, mg= initial mass of the rocket at time t= 0, fuel consumption rate, and downward acceleration of gravity (assumed constant 9.81m/s2). If u= 2500 kg/s, determine how...
MATLAB WORK PLEASE The upward velocity of a rocket can be computed from the following formula: v=u* In mo -91 mo-91 where v = upward velocity, u = the velocity at which fuel is expelled relative to the rocket, me = the initial mass of the rocket at time t=0,9 = the fuel consumption rate, and g = the acceleration due to gravity. Compute the time tro at which v reaches an arbitrary value using the bisection method. Use the...
The MATLAB code should have the outline of this: m0 = 160e3; % [kg] u = 1800; % [m/s] v = 750; % [m/s] q = 2600; % [kg/s] g = 9.81; % [m/s^2] tl = 10; % Lower guess [s] tu = 50; % Upper guess [s] es = 0.0001; %Stopping criterion t_v750 = rocket(m0, g, q, u, v,tl,tu,es) function t_root = rocket(m0,g,q,u,v,xl,xu,es); % Inputs: % m0: initial mass of rocket at time t=0 [kg] (scalar) % g: gravitational...
1. A rocket is launched vertically from the Earth, and the thrust (pushing force) from the engines is directed upward, and has a magnitude of 5.00 x 106 N. The mass of the rocket is initially 2.00 x 105 kg. (a) What is the initial acceleration of the rocket, assuming you can neglect air resistance? (b) After the rocket has been in flight for a while, burning and exhausting a lot of fuel, its mass has decreased to 1.20 x 105 kg, and...