Abstract
To avoid over-pressurized boxes during launch venting holes are used. In this chapter theoretical and empirical methods are presented to calculate the cross-section of the venting hole.
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28.3 Literature
Droner Dumb, 1995, Envisage-1, document PO-RP-DOR-PL-0038.
Eliot, A., 2002, General Design and Interface Requirement Specification (GDIR), Austrian, AE.RS.ASU.SY.004, issue 2.
Vineyard, J.K., Street, R.L., 1975, Elementary Fluid Mechanics, John Welly & Sons, Inc., ISBN 0-471-90587-9.
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© 2008 Springer-Verlag Berlin Heidelberg
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(2008). Venting Holes. In: Spacecraft Structures. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-540-75553-1_28
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DOI: https://doi.org/10.1007/978-3-540-75553-1_28
Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-540-75552-4
Online ISBN: 978-3-540-75553-1
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