In matlab codeFind the velocity of mars, earth, venus.In the descent phase of an extraterrestrial space mission, a spacecraft free falls through theplanet's atmosphere. As it falls, it will reach a constant or terminal velocity when the airresistance force balances the gravitational attraction force. The terminal velocity is given byV₁ =where m is the spacecraft's mass [m], g is the acceleration due to gravity on the planet, p is theatmosphere's density [kg/m³], Cp is the spacecraft's drag coefficient, and A is the spacecraft'scross-sectional area [m²].a) Write a function named terminalVelocity which calculates the terminal velocityan object. The function should.2mgpCDAinput m, g, p, CD, and Aoutput the terminal velocityb) Write a program named q03.m which calculates the terminal velocity of a spacecraft at10 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 andterminal Velocity functions. Complete the following table:.Density [kg/m]PlanetVenus67"Earth0.413Mars0.020*approximate atmospheric density at the surface iVr (m/s)VT/VT.earth

We need to write a program to find the velocity of mars, earth, mars. See below steps for code.

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

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Question

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].
a) Write a function named terminalVelocity which calculates the terminal velocity
an object. The function should
.
2mg
pCDA
input m, g, p, CD, 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:
.
Density [kg/m]
Planet
Venus
67"
Earth
0.413
Mars
0.020*
approximate atmospheric density at the surface i
Vr (m/s)
VT/VT.earth

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