Milos, 1998 - Google Patents
Thermostructural analysis of SIRCA tile for X-34 wing leading edge TPSMilos, 1998
- Document ID
- 17530037166086941255
- Author
- Milos F
- Publication year
- Publication venue
- 36th AIAA Aerospace Sciences Meeting and Exhibit
External Links
Snippet
Finite element thermal and linear stress analyses of SIRCA tiles, assemblies, and arc jet models are presented. The analyses were performed to verify thermal and structural models for SIRCA, to establish a failure criteria for stressed tiles, to simulate the response of the X …
- 238000004458 analytical method 0 title description 10
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/52—Protection, safety or emergency devices; Survival aids
- B64G1/58—Thermal protection, e.g. heat shields
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/46—Arrangements or adaptations of devices for control of environment or living conditions
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