Linear theory of optimum hot air balloon performance – application to Titan
2008 ◽
Vol 112
(1132)
◽
pp. 353-355
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Keyword(s):
Hot Air
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Abstract We develop a simple theory for hot air balloon performance with fixed thermal power and linear heat transfer to the environment, applicable to low-temperature situations such as Titan’s atmosphere. The theory results in a closed-form solution and it is shown that an optimum balloon diameter exists – the maximum payload is achieved when the envelope mass and payload mass are equal. It is also shown simply that the floating mass for a given power has a stronger sensitivity to heat transfer coefficient than to the envelope specific mass. A hot air balloon on Titan with a ~2kW heat source could loft a theoretical maximum payload of ~195kg or ~100kg with appropriate margins.
1988 ◽
Vol 31
(8)
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pp. 1613-1617
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Keyword(s):
2019 ◽
Vol 145
(3)
◽
pp. 04019004
2013 ◽
Vol 732-733
◽
pp. 78-82