Mars balloon , forces, pressure

Click For Summary

Homework Help Overview

The discussion revolves around the buoyancy of a balloon in Mars' atmosphere, specifically how to determine the radius required for the balloon to hover. The problem also explores the behavior of the same balloon in Earth's atmosphere, questioning the resulting acceleration and forces acting on it.

Discussion Character

  • Exploratory, Assumption checking, Conceptual clarification

Approaches and Questions Raised

  • The original poster attempts to calculate the radius of the balloon needed for buoyancy on Mars and raises concerns about the acceleration calculated for the balloon in Earth's atmosphere, questioning the role of the gas inside the balloon.
  • Some participants discuss the implications of air resistance and terminal velocity, suggesting that the initial acceleration calculated may not be physically realistic.
  • Others inquire about the drag equation and its components, seeking clarification on how terminal velocity is derived.

Discussion Status

The discussion is ongoing, with participants providing insights into the effects of air resistance and terminal velocity. Some guidance has been offered regarding the drag force and its calculation, but there remains a lack of consensus on the original poster's calculations and assumptions.

Contextual Notes

Participants are considering the effects of different atmospheric densities and the implications of neglecting the gas inside the balloon. There is also a focus on the complexities introduced by real-world factors such as air resistance.

Bassalisk
Messages
946
Reaction score
2

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?
 
Physics news on Phys.org
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.
 

Similar threads

  • · Replies 12 ·
Replies
12
Views
2K
Replies
170
Views
8K
Replies
2
Views
1K
  • · Replies 1 ·
Replies
1
Views
3K
  • · Replies 62 ·
3
Replies
62
Views
5K
Replies
18
Views
8K
Replies
2
Views
2K
  • · Replies 6 ·
Replies
6
Views
3K
  • · Replies 9 ·
Replies
9
Views
2K
  • · Replies 3 ·
Replies
3
Views
4K