Can a Vacuum-based Buoyancy System Outperform Traditional Helium Balloons?

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Discussion Overview

The discussion centers around the feasibility of a vacuum-based buoyancy system as an alternative to traditional helium balloons. Participants explore theoretical concepts, material requirements, and potential applications, including the use of advanced materials and structural designs to maintain a vacuum while achieving sufficient lift.

Discussion Character

  • Exploratory
  • Technical explanation
  • Debate/contested
  • Mathematical reasoning

Main Points Raised

  • One participant suggests that using a vacuum could theoretically provide more lift than helium by reducing internal mass, but acknowledges the challenge of maintaining a vacuum with current materials.
  • Another participant references a previous discussion, noting that a vacuum balloon may not be significantly more buoyant than a hydrogen balloon, questioning the practicality of the concept.
  • Some participants propose using electromagnetism to create a structure that counters atmospheric pressure, potentially allowing for a lighter design.
  • There is mention of using a mylar balloon with an internal support grid made of concrete to withstand pressure, raising concerns about torsional forces rather than compressive strength.
  • Mathematical considerations are introduced regarding lift calculations based on air density and balloon volume, emphasizing the need for the entire structure to weigh less than the air displaced.
  • Participants discuss the implications of achieving lift for proof of concept versus practical applications, with some arguing that even a demonstration would require the system to be lighter than the air displaced.

Areas of Agreement / Disagreement

Participants express differing views on the practicality and efficiency of vacuum balloons compared to helium or hydrogen balloons. There is no consensus on whether the benefits of a vacuum-based system outweigh the complexities involved in its design and construction.

Contextual Notes

Limitations include the dependence on advanced materials that may not yet be available, unresolved mathematical steps in the calculations presented, and the challenge of designing a structure that can withstand atmospheric pressure while remaining lightweight.

CHollman82
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Hi, first time posting here.

I was watching a show about hydrogen/helium balloons and it got me thinking about buoyancy in atmospheric gasses (nitrogen) and what might work better than the common gasses and I considered that since the goal of a balloon is to reduce the internal mass relative to the mass of the medium why not just eliminate it entirely and use a vacuum? I understand ordinary balloon material would not work as it would simply be crushed by atmospheric pressure... so my question to you guys is can you think of any way to maintain a volume of vacuum or near-vacuum while still keeping the object light enough to provide more lift than a traditional helium balloon? If someone loves doing math you could come up with the equation to relate the volume of the vacuum with the lift capacity it would have if it could be maintained in the atmosphere...

Now, I've seen video of a train car (the cylindrical ones that carry liquids) being completely crushed by nothing but atmospheric pressure due to very low internal pressure, so I know this container would have to be fairly robust and we likely are lacking the material to make this feasible, but what about materials that are on the horizon, like something made with carbon nanotubes maybe? Maybe with a reinforced internal structure like a honeycomb structure with thousands of pockets of vacuum?

It would be great if we could create something like this with significant lift capacity to deliver space vehicles high into the atmosphere where they would "launch" from the floating platform or something, since that would be reusable ad infinitum it would reduce the cost to deliver a payload to LEO by a great deal I would imagine.
 
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Thanks for the link, I read through that thread and came up with another idea in the meantime...

What about using electromagnetism to force metal foil apart to counteract the pressure of the atmosphere? You'd still need a rigid frame but it and the membrane itself would not have to withstand nearly as much pressure, meaning it could be lighter.

Also, one distinct advantage a vacuum balloon would have over a helium or hydrogen balloon is that it would strengthen as it increased in altitude and would find an equilibrium point and float there, where other balloons will eventually burst.
 
CHollman82 said:
What about using electromagnetism to force metal foil apart to counteract the pressure of the atmosphere? You'd still need a rigid frame but it and the membrane itself would not have to withstand nearly as much pressure, meaning it could be lighter.

And how much would this electromagnetic generator weigh??


CHollman82 said:
Also, one distinct advantage a vacuum balloon would have over a helium or hydrogen balloon is that it would strengthen as it increased in altitude and would find an equilibrium point and float there, where other balloons will eventually burst.

I pointed this out in the other thread, but it is a small advantage for the short range before the balloon reached equilibirum. And weather balloons have solved this problem anyway. They don't burst.
 
How about a fairly large mylar balloon of the same material as the party balloons, thin film of aluminum I think, with an internal support grid of something like concrete (very high compression strength, so it can be very thin)?

BTW fun is rarely doing something the obvious practical way.
 
MikeTheLost said:
How about a fairly large mylar balloon of the same material as the party balloons, thin film of aluminum I think, with an internal support grid of something like concrete (very high compression strength, so it can be very thin)?

BTW fun is rarely doing something the obvious practical way.
You won't need to worry about compressions strength so much as you will torsional forces.

In general, pick a volume for the balloon, say 1000m^3. Find the wight of that much air. Your entire structure, including mylar, support and 1000m^3 of helium (178kg) would have to weigh less than that.
 
DaveC426913 said:
You won't need to worry about compressions strength so much as you will torsional forces.

In general, pick a volume for the balloon, say 1000m^3. Find the wight of that much air. Your entire structure, including mylar, support and 1000m^3 of helium (178kg) would have to weigh less than that.

That would be for a practical solution, as opposed to a demonstration of technology where all I would need to do is make it off the ground.
 
DaveC426913 said:
Thing is, a vacuum balloon is not all that much more buoyant than a hydrogen balloon.

I think this is the show stopper here. There just isn't enough payoff for a complex solution, so unless a vacuum balloon can be cheap and easy, why bother?
 
MikeTheLost said:
That would be for a practical solution, as opposed to a demonstration of technology where all I would need to do is make it off the ground.
:confused:

No, even just to make a demonstration and make it off the ground your entire setup would indeed have to weigh less than the air displaced.

If you wanted a practical solution beyond that then it would need to weigh significantly less, enough to haul a payload as well.
 
  • #10
DaveC426913 said:
:confused:

No, even just to make a demonstration and make it off the ground your entire setup would indeed have to weigh less than the air displaced.

If you wanted a practical solution beyond that then it would need to weigh significantly less, enough to haul a payload as well.

Right, but not less than helium, except as a practical, ie boring solution.
 
  • #11
Right. I see your point now. You were referring to your vacuum balloon. It would not have to be more efficient than helium. Simply getting off the ground would suffice to be a proof of concept.
 
  • #12
I had this same idea, here some figure about the feasibility of the system:

Note: the idea on this calculation is to see how shape and structural factors go with the characteristic dimension. the value of those factor in turn give information about the feasibility of the design with the current materials.

balloon LIFT:
The lift force depend on the weight of the air, that the balloon volume occupy, so:

g [m/s3] = gravity
RoAir [kg/m3] = air density at a given altitude and temperature
BV [m3] = balloon Volume

Lift [N] = g [m/s2] * RoAir [kg/m3] * BV [m3]

The balloon volume will be the cube of the characteristic dimension multiplied by a geometrical constant which account for the balloon shape

d[m] = characteristic dimension
Kv [1] = volume shape factor (for a sphere is equal to Pi*4/3)

BV [m3] = (d [m] ^3) * Kv [1]

balloon WEIGHT:
It's very difficult for a sphere to withstand compression (it will deformate and crush), so the best way to make a light balloon is probably to apply a thin surface on a structure with high compressive strength over weight ratio. in this case, the balloon weight will be given by two component:
-The surface (that withold the vacuum)
-The structure (that withstand the compressive force)

balloon SURFACE WEIGHT:
The balloon weight will depend on the balloon surface area, the surface thickness and the surface material density (some sort of plastic may be the best)

g [m/s2] = gravity (9.8)
BS [m2] = balloon surface area
T [m] = Surface thickness
RoSurface [Kg/m3] = balloon surface density (for rubber is 1200)

BSW [ N ] = g [m/s2] * BS [m2] * T [m] * RoSurface [Kg/m3]

Again i can generally express the surface area the square of the characteristic multiplied by another shape factor

d[m] = characteristic dimension
Ksa [1] = surface area shape factor (for a sphere is equal to Pi*4)

BS [m2] = (d [m] ^2) * Ksa [1]

balloon STRUCTURE WEIGHT:
This is probably the most limiting part of the design, i will compute the Crushing Force that the balloon feel, and express the weight of the structure as a fraction of this force. (example. if the Structure Weight constant need to be 1/1000, mean that a balloon structure of 1N of weight, need to withstand 1000N of compressive force from the surface)

The Crushing Force the structure need to withstand is the balloon surface area multiplied be the pressure difference

DeltaP [pa] [N/m2] = difference in pressure between outside and inside of the balloon
BS[m2] = balloon surface area

CF [N] = BS [m2] * DeltaP [pa]

The structure weight will be the crushing force multiplied by a structure constant, which account for the structure shape and material

CF [N] = Crushing Force felt by the balloon structure
Kx [1] = structure weight over resistance ratio

BXW [N] = CF [N] * Kx [1]

FINAL CONSIDERATION:
The fly limit happen when the balloon weight equal the lift (the weight need to be lower for pratical porpouse, so this give the lower bound of the shape and structural constant)

LIFT [N] = BaloonSurfaceWeight [N] + balloon Structure Weight (BXW) [N]

Doing some math and semplification and resolving in respect to the Kx constant:

g [m/s2] = gravity (9.8)
T [m] = Surface thickness
RoSurface [Kg/m3] = balloon surface density (for rubber is 1200)
Kx [1] = structure weight over resistance ratio
d[m] = characteristic dimension
Ksa [1] = surface area shape factor (for a sphere is equal to Pi*4)
DeltaP [pa] [N/m2] = difference in pressure between outside and inside of the balloon
Kv [1] = volume shape factor (for a sphere is equal to Pi*4/3)

Kx [1] = g [m/s2] * { d [m] *RoAir [Kg/m3] *Kv [1] - T [m] *Ka [1] *RoSurface [kg/m3] } / DeltaP [pa]

Kx of 1/100 is easier to obtain then 1/1000, the higher Kx, the better.

This formula tell that:

1) Bigger balloon have advantage over small balloon since d (the characteristic dimension) is on the numerator (it make sense, since the lift force increase with volume but crushing force increase only with the square of d).
This does not account for the difficulty to achieve let's say Kv = 1/100 with a structure that weight 1N or one that weight 10N)

2) Shape that have higher volume over dimension ratio is better (it make sense since moving more air, increase the lift) (example: cube)

3) Shape that have lower surface over dimension ratio is better (it make sense since i lower the crushing force exerted on the structure) (example sphere:)

4) Point 2 and 3 go in opposit direction, in the design you need to balance them in order to not have a bottleneck (highest value for the difference)

5) Higher gravity make thing easier, the balloon would work better on Jupiter then Earth (make sense since the gravity will influence more the liquid than the structure weight)
the same can be said for higher liquid density (example: water better than air)

6) Having lower surface density or lower thickness (aka better surface material) is better (obvious, but if the formula get at least the obvious thing right there is chance for it to be right also)
 

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