Ballooning

A hot air balloon works by the buoyancy of the heated air. However, its height is limited by the fact that the air pressure decreases steadily with increasing height.

What is the maximum height h h of the hot air balloon?

Enter the altitude in units of km , \text{km}, to 2 decimal places.

Details and assumptions:

  • The temperatures of the atmosphere and the hot air inside the ballon are T 0 = 300 K T_0 = 300\,\text{K} and T = 400 K T = 400\,\text{K} , respectively.
  • The barometric formula reads p = p 0 exp ( h h 0 ) p = p_0 \exp\left(- \frac{h}{h_0}\right) with the pressure p 0 = 1 0 5 Pa p_0 = 10^5 \,\text{Pa} at the ground and the scale height h 0 = 8.4 km . h_0 = 8.4\,\text{km}.
  • Air has molar mass M = 29 g / mol M = 29 \,\text{g}/\text{mol} and can be treated as an ideal gas.
  • Treate the balloon envelope as a sphere with radius r = 13 m r = 13\,\text{m} . The total mass of the ballon (without air) is m = 1250 kg m = 1250\,\text{kg} .
  • Use the gas constant R = 8.314 J / mol K R = 8.314 \,\text{J} / \text{mol}\, \text{K} and the gravity g = 9.81 m / s 2 . g = 9.81\,\text{m}/\text{s}^2.


The answer is 6.39.

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1 solution

Markus Michelmann
Oct 22, 2017

The volume of the ballon results to V = 4 3 π r 3 = 9203 m 3 V = \frac{4}{3} \pi r^3 = 9203 \,\text{m}^3 With the help of the ideal gas equation p V = n R T p V = n R T we can write for the air density ρ = M n V = M p R T \rho = \frac{M n}{V} = \frac{M p}{RT} Therefore, the buoyancy force reads F b = ( ρ ext ρ ) g V = M g V R p ( 1 T 0 1 T ) F_b = (\rho_\text{ext} - \rho) g V = \frac{M g V}{R} p \left( \frac{1}{T_0} - \frac{1}{T} \right) with the densities of the atmosphere, ρ ext \rho_\text{ext} , and of the air inside the ballon, ρ \rho . At maximal altitude, the buoyancy is compensated by the weight of the balloon F b = ! F g = m g p = p 0 e h / h 0 = m R M V T T 0 T T 0 e h / h 0 = m ρ 0 V T T T 0 h = h 0 log ( m ρ 0 V T T T 0 ) = h 0 log ( ρ 0 V m T T 0 T ) = 6391 m \begin{aligned} & & F_b &\stackrel{!}{=} F_g = m g \\ \Rightarrow & & p &= p_0 e^{-h/h_0} = \frac{m R}{M V} \frac{T T_0}{T - T_0}\\ \Rightarrow & & e^{-h/h_0} &= \frac{m}{\rho_0 V} \frac{T}{T - T_0} \\ \Rightarrow & & h &= - h_0 \log \left(\frac{m}{\rho_0 V} \frac{T}{T - T_0} \right) = h_0 \log \left(\frac{\rho_0 V}{m} \frac{T - T_0}{T} \right) = 6391 \,\text{m} \end{aligned} with the air density ρ 0 = M p 0 R T 0 = 1.16 kg / m 3 \rho_0 = \frac{M p_0}{R T_0} = 1.16 \,\text{kg}/\text{m}^3 on the ground.

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