Mars balloon , forces, pressure

AI Thread Summary
To achieve buoyancy in Mars' atmosphere, a balloon with a radius of approximately 0.974 meters is required, based on the density of Mars' atmosphere and the balloon's surface density. When placed in Earth's atmosphere, the balloon's calculated acceleration appears to be 762.34 m/s², which is deemed physically unrealistic due to the neglect of air resistance. The discussion highlights the importance of considering drag forces, which significantly affect the balloon's motion once it begins to ascend. The terminal velocity of the balloon is calculated to be 7.3 m/s, indicating that it will not accelerate indefinitely but rather reach a steady speed. Overall, the complexities of real-world physics, including drag and buoyancy, make the scenario more intricate than initial calculations suggest.
Bassalisk
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Homework Statement


We have a balloon that is need to stay buoyant in Mars atmosphere, to make it hover.
Density given for Mars's atmosphere is 0,0154 kg/m^3. Let's assume that we have to make balloons out of thin firm plastic, with surface density of 5 g/m^2. Balloons would be inflated with a very light gas that we can neglect.

What radius(spherical balloon) would balloon have to have, to make it hover above Mars surface.

When we would put the same balloon in Earths atmosphere, with air density of 1,2 kg/m^3, what would happen? Would the balloon go up or down? Find starting acceleration.


Homework Equations



G=mg
F=rho*g*v (Buoyant force)
V=4/3*r^3* pi
A=4pi*r

The Attempt at a Solution




I solved the first part. U equalize mg and rho*g*v. g of Mars cancels. Mass u get from surface density * surface it self. etc etc.

u get effective radius of: r = 0,974 m.


BUT second part is a bit tricky.

we have Newtons first law, ma= rho(air)*g*V - mg.

m we calculated before, and we get that ma=44,97 N

m was 0,059 kg. And from these statements we get that

a=762,34 m/s^2 which is physical absurd imho.


Help? Does now air inside balloon matter or?
 
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I can find no fault in your calculation. Of course the moment it started to move, air-resistance would come into effect and the balloon would very quickly reach terminal velocity.
 
Very non intuitive! That is my problem. I almost get the speed of sound in a second an a half. But i think real-case scenario is much more complicated.

Thanks
 
Bassalisk said:
Very non intuitive! That is my problem. I almost get the speed of sound in a second an a half. But i think real-case scenario is much more complicated.

Thanks

But it will not accelerate at this rate for any appreciable length of time. When it starts to move you have to consider air resistance.

Using the drag equation the terminal velocity of your balloon is 7.3m/s, so it will not get any faster than this.
 
Mr.A.Gibson said:
But it will not accelerate at this rate for any appreciable length of time. When it starts to move you have to consider air resistance.

Using the drag equation the terminal velocity of your balloon is 7.3m/s, so it will not get any faster than this.

Can you explain this equation? I found it on wiki, but components are not as clear.

Thanks
 
You calculate the drag force from the eqation, it's components are:
ρ the density of air,
v the velocity of the balloon, when the forces are balanced this is the terminal velocity
A cross-sectional area of the balloon, calculate from the radius
C_d Drag coefficient, this changes for different shapes for a sphere it is 0.47
 
Mr.A.Gibson said:
You calculate the drag force from the eqation, it's components are:
ρ the density of air,
v the velocity of the balloon, when the forces are balanced this is the terminal velocity
A cross-sectional area of the balloon, calculate from the radius
C_d Drag coefficient, this changes for different shapes for a sphere it is 0.47

K but i still don't get how did u end up with 7,3 m/s ?
 
When at terminal velocity the forces are in balance Bouancy = weight + drag
Put in the formula you have and then rearrange for v. Then show an attempted solution.
 
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