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.Google Scholar
- Eliot, A., 2002, General Design and Interface Requirement Specification (GDIR), Austrian, AE.RS.ASU.SY.004, issue 2.Google Scholar
- Vineyard, J.K., Street, R.L., 1975, Elementary Fluid Mechanics, John Welly & Sons, Inc., ISBN 0-471-90587-9.Google Scholar
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