Mars balloon , forces, pressure

Click For Summary
SUMMARY

The discussion focuses on calculating the radius of a balloon required to hover in Mars' atmosphere, which has a density of 0.0154 kg/m³. The effective radius calculated is 0.974 m, based on the buoyant force equation F = ρgV. The second part of the problem examines the balloon's behavior in Earth's atmosphere, where the air density is 1.2 kg/m³. The calculated acceleration of 762.34 m/s² is deemed physically absurd, as it does not account for air resistance. The terminal velocity of the balloon is determined to be 7.3 m/s, indicating that the balloon will not accelerate indefinitely due to drag forces.

PREREQUISITES
  • Understanding of buoyant force and its calculation using F = ρgV
  • Familiarity with Newton's laws of motion, particularly the first law
  • Knowledge of the drag equation and its components, including drag coefficient (C_d)
  • Basic principles of fluid dynamics and terminal velocity
NEXT STEPS
  • Study the drag equation in detail, focusing on its components and applications
  • Learn about buoyancy in different atmospheric conditions, comparing Mars and Earth
  • Explore the concept of terminal velocity and how it applies to various shapes
  • Investigate the effects of air resistance on objects in motion through different mediums
USEFUL FOR

Students in physics or engineering, aerospace engineers, and anyone interested in the dynamics of buoyancy and drag in different atmospheric conditions.

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
7K
Replies
2
Views
2K
  • · Replies 6 ·
Replies
6
Views
3K
  • · Replies 9 ·
Replies
9
Views
2K
  • · Replies 3 ·
Replies
3
Views
4K