Test sequence for payload fairings
european standards (ecss) exist for space systems but they are generally outlined for launch vehicles. Do specific standards exist for payload fairings? For example a test sequence is outlined for general space vehicles in (ecss e-10-03A) which is :
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Does a test sequence such as this exist for payload fairings?
![[IMG]](proxy.php?image=http%3A%2F%2Fwww.rotaryforum.com%2Fforum%2Fimages%2Fsmilies%2Fbiggrin.gif&hash=6c5b1a130889e07c32d41238ac31e2af)
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Does a test sequence such as this exist for payload fairings?
![[IMG]](proxy.php?image=http%3A%2F%2Fwww.rotaryforum.com%2Fforum%2Fimages%2Fsmilies%2Fbiggrin.gif&hash=6c5b1a130889e07c32d41238ac31e2af)
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