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Centaur standard shroud (css) full jettison test dynamic analysis
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Kasper, H. J. Donovan, R. M. |
| Copyright Year | 1974 |
| 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. |
| File Size | 1130788 |
| Page Count | 53 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19740014397 |
| Archival Resource Key | ark:/13960/t40s4jd5r |
| Language | English |
| Publisher Date | 1974-04-01 |
| Access Restriction | Open |
| Subject Keyword | Space Vehicles Dynamic Tests Bending Moments Centaur Launch Vehicle Shrouds Jettisoning Prediction Analysis Techniques Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
