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Orbiter structural design and verification
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Moser, T. L. Glynn, P. C. |
| Copyright Year | 1985 |
| Description | The space shuttle development program provided the opportunity to challenge many of the established practices and approaches used in prior manned space flight programs. The most significant accomplishments and resulting precedents which emerged during the structural development of the space shuttle and the space shuttle orbiter are reviewed. Innovations in criteria, design solutions, and certification are highlighted, and brief comments on the lessons learned are included. Thermal stress, graphite epoxy moisture, window structure, and structural inspection are discussed under lessons learned. |
| File Size | 5236274 |
| Page Count | 12 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19850008606 |
| Archival Resource Key | ark:/13960/t9j43n647 |
| Language | English |
| Publisher Date | 1985-01-01 |
| Access Restriction | Open |
| Subject Keyword | Space Transportation Structural Design Airframes Acoustic Fatigue Moisture Space Shuttles Windows Apertures Graphite-epoxy Composites Space Shuttle Orbiters Spacecraft Design Thermal Stresses Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
