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Advanced high temperature structural seals (Document No: 20020090799)
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Rorabaugh, Michael Keller, Peter C. Newquist, Charles W. Shorey, Mark Verzemnieks Sr., Juris |
| Copyright Year | 2002 |
| Description | This program addresses the development of high temperature structural seals for control surfaces for a new generation of small reusable launch vehicles. Successful development will contribute significantly to the mission goal of reducing launch cost for small, 200 to 300 pound payloads. Development of high temperature seals is mission enabling. For instance, ineffective control surface seals can result in high temperature (3100 F) flows in the elevon area exceeding structural material limits. Longer sealing life will allow use for many missions before replacement, contributing to the reduction of hardware, operation and launch costs. |
| File Size | 10226520 |
| Page Count | 109 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20020090799 |
| Archival Resource Key | ark:/13960/t4cp22h10 |
| Language | English |
| Publisher Date | 2002-10-01 |
| Access Restriction | Open |
| Subject Keyword | Mechanical Engineering Elevons Launch Costs Life Durability Cost Reduction High Temperature Environments Design Analysis Spacecraft Launching Research and Development Reusable Launch Vehicles Fabrication Seals Stoppers Landing Simulation Product Development Thermal Analysis 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 |
