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Space vehicle integrated thermal protection/structural/meteoroid protection system, volume 1
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Zimmerman, D. K. Bartlett, D. H. |
| Copyright Year | 1973 |
| Description | A program was conducted to determine the merit of a combined structure/thermal meteoroid protection system for a cryogenic vehicle propulsion module. Structural concepts were evaluated to identify least weight designs. Thermal analyses determined optimum tank arrangements and insulation materials. Meteoroid penetration experiments provided data for design of protection systems. Preliminary designs were made and compared on the basis of payload capability. Thermal performance tests demonstrated heat transfer rates typical for the selected design. Meteoroid impact tests verified the protection characteristics. A mockup was made to demonstrate protection system installation. The best design found combined multilayer insulation with a truss structure vehicle body. The multilayer served as the thermal/meteoroid protection system. |
| File Size | 35074095 |
| Page Count | 426 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19730016138 |
| Archival Resource Key | ark:/13960/t3518rz63 |
| Language | English |
| Publisher Date | 1973-04-01 |
| Access Restriction | Open |
| Subject Keyword | Space Vehicles Thermal Protection Meteoroid Protection Multilayer Insulation Heat Transfer Cryogenic Rocket Propellants Spacecraft Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |