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Centaur Standard Shroud (CSS) full jettison test dynamic analysis (1974)

Kasper, H. J. ; Donovan, R. M.

In: CASI

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Publication Date: 2019-06-27

Description: During the space power facility jettison tests, the non-domed half of the Centaur standard shroud was allowed to completely separate from its hinge connection and was caught in a horizontal catch net. A rigid body dynamic analysis that was performed to predict the half shroud prior to and after net contact is presented. Analytical predictions of the longitudinal and circumferential bending moments imposed on the half shroud by the catch net and the net pressure on the half shroud corrugated skin are also presented.

Keywords: SPACE VEHICLES

Type: NASA-TM-X-71537 , E-7943

Format: application/pdf

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