In matlab code Find the velocity of mars, earth, venus. In the descent phase of an extraterrestrial space mission, a spacecraft free falls through the planet's atmosphere. As it falls, it will reach a constant or terminal velocity when the air resistance force balances the gravitational attraction force. The terminal velocity is given by V₁ = where m is the spacecraft's mass [m], g is the acceleration due to gravity on the planet, p is the atmosphere's density [kg/m³), Cp is the spacecraft's drag coefficient, and A is the spacecraft's cross-sectional area (m²). 2mg PCDA a) Write a function named terminalVelocity which calculates the terminal velocity of an object. The function should . input m, g, P. Cp. and A . output the terminal velocity b) Write a program named q03.m which calculates the terminal velocity of a spacecraft at 10 km above the surface of various planets. The spacecraft's properties are m= 240 [kg], A= 15 [m²], and Cp=0.5. The program should use the gravity and terminal Velocity functions. Complete the following table: Planet Venus Density [kg/m] Vr (m/s) 67 Earth 0.413 Marsi 0.020 approximate atmospheric density at the surface Vr/Vrearth
In matlab code Find the velocity of mars, earth, venus. In the descent phase of an extraterrestrial space mission, a spacecraft free falls through the planet's atmosphere. As it falls, it will reach a constant or terminal velocity when the air resistance force balances the gravitational attraction force. The terminal velocity is given by V₁ = where m is the spacecraft's mass [m], g is the acceleration due to gravity on the planet, p is the atmosphere's density [kg/m³), Cp is the spacecraft's drag coefficient, and A is the spacecraft's cross-sectional area (m²). 2mg PCDA a) Write a function named terminalVelocity which calculates the terminal velocity of an object. The function should . input m, g, P. Cp. and A . output the terminal velocity b) Write a program named q03.m which calculates the terminal velocity of a spacecraft at 10 km above the surface of various planets. The spacecraft's properties are m= 240 [kg], A= 15 [m²], and Cp=0.5. The program should use the gravity and terminal Velocity functions. Complete the following table: Planet Venus Density [kg/m] Vr (m/s) 67 Earth 0.413 Marsi 0.020 approximate atmospheric density at the surface Vr/Vrearth
C++ for Engineers and Scientists
4th Edition
ISBN:9781133187844
Author:Bronson, Gary J.
Publisher:Bronson, Gary J.
Chapter1: Fundamentals Of C++ Programming
Section: Chapter Questions
Problem 2PP: (Conversion) An object’s polar moment of inertia, J, represents its resistance to twisting. For a...
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