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Gcd techport data sheets thermal protection system materials (tpsm) project
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Chinnapongse, Ronald L. |
| Copyright Year | 2014 |
| Description | The Thermal Protection System Materials (TPSM) Project consists of three distinct project elements: the 3-Dimensional Multifunctional Ablative Thermal Protection System (3D MAT) project element; the Conformal Ablative Thermal Protection System (CA-TPS) project element; and the Heatshield for Extreme Entry Environment Technology (HEEET) project element. 3D MAT seeks to design, develop and deliver a game changing material solution based on 3-dimensional weaving and resin infusion approach for manufacturing a material that can function as a robust structure as well as a thermal protection system. CA-TPS seeks to develop and deliver a conformal ablative material designed to be efficient and capable of withstanding peak heat flux up to 500 W/ sq cm, peak pressure up to 0.4 atm, and shear up to 500 Pa. HEEET is developing a new ablative TPS that takes advantage of state-of-the-art 3D weaving technologies and traditional manufacturing processes to infuse woven preforms with a resin, machine them to shape, and assemble them as a tiled solution on the entry vehicle substructure or heatshield. |
| File Size | 319321 |
| Page Count | 9 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20140016745 |
| Archival Resource Key | ark:/13960/t3mw7f82r |
| Language | English |
| Publisher Date | 2014-05-13 |
| Access Restriction | Open |
| Subject Keyword | Heeet Woven Tps Thermal Protection System Spacecraft Shielding Thermal Protection Heat Shielding Ablative Materials Weaving Manufacturing Ablation 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 |