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X-33 lh2 tank failure investigation findings (Document No: 20010020398)
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Niedermeyer, Mindy |
| Copyright Year | 2000 |
| Description | This presentation focuses on the tank history, test objectives, failure description, investigation and conclusions. The test objectives include verify structural integrity at 105% expected flight load limit varying the following parameters: cryogenic temperature; internal pressure; and mechanical loading. The Failure description includes structural component of the aft body, quad-lobe design, and sandwich - honeycomb graphite epoxy construction. |
| File Size | 24502760 |
| File Format | |
| Language | English |
| Publisher Date | 2000-01-01 |
| Access Restriction | Open |
| Subject Keyword | Composite Materials Structural Failure X-33 Reusable Launch Vehicle Cryogenic Fluid Storage Graphite-epoxy Composites Honeycomb Structures Liquid Hydrogen Sandwich Structures Cryogenic Temperature Cryogenic Rocket Propellants Internal Pressure Structural Analysis Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
