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Composite reinforced propellant tanks. [space shuttles
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Brown, L. D. Landes, R. Aleck, B. J. Martin, M. J. |
| Copyright Year | 1975 |
| Description | Design studies involving weight and cost were carried out for several structural concepts applicable to space shuttle disposable tankage. An effective design, a honeycomb stabilized pressure vessel, was chosen. A test model was designed and fabricated. |
| File Size | 9284294 |
| Page Count | 213 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19750013268 |
| Archival Resource Key | ark:/13960/t8tb5wf49 |
| Language | English |
| Publisher Date | 1975-02-01 |
| Access Restriction | Open |
| Subject Keyword | Spacecraft Design, Testing And Performance S Glass Weight Analysis Composite Materials Pressure Vessels Low Cost Space Shuttles Aluminum Alloys Stiffening Honeycomb Structures Design Analysis Propellant Tanks 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 |