Abstract

Long-duration scientific balloon flights using conventional ballasting methods to compensate for daily loss of lift suffer a severe payload weight penalty. Typically, the weight of the expendable ballast approaches or exceeds the weight of the balloon and payload. This paper examines the concept of correcting for degraded lift by “gas replenishment” techniques, that is, by replacing lost helium inflatant from an on-board dewar. Appropriate equations are developed and curves are presented which demonstrate the clear theoretical superiority of the replenishment method. Design problems associated with the dewars and heat exchangers required to implement the gas replenishment concept are also discussed in detail. A series of curves is presented in which net load, dewar weight and quantity of helium required are plotted for specific balloons and float altitudes as a function of daily loss rate. The lack of relevant heat exchange data in the literature is cited as an obstacle to immediate prototype development.

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