Preliminary tests for an intelligent thermal protection system for space vehicles

Proceedings of SPIE- The International Society for Optical Engineering

Volumn 4234, Issue , 2001, Pages 160-167

  Paolozzi, A ^a   Felli, F ^a   Valente, T ^a   Caponero, M A ^a   Tului, M ^a  

^a SAPIENZA UNIVERSITY OF ROME   (Italy)

Author keywords

Coating; Optical fibers; Structural health monitoring; Thermal protection system

Indexed keywords

HEAT TREATMENT; HIGH PRESSURE EFFECTS; POWDER METALS; SPACE APPLICATIONS;

STRUCTURAL HEALTH MONITORING; THERMAL PROTECTION SYSTEMS;

FIBER OPTIC SENSORS;

EID: 0034988453     PISSN: 0277786X     EISSN: None     Source Type: Journal    
DOI: 10.1117/12.424402     Document Type: Article

References (8)

1. The X-33 program: Proving feasibility of the next generation reusable launch vehicles
2. Materials for air and space. The future of space flight: Challenges in materials
3. Health monitoring of a continuous fiber reinforced aluminum composite with embedded optical fiber
4. Mechanical and optical properties of optical fiber embedded super hybrid material
5. Embedding optical fibers into cast aluminum alloy
6. In-situ formation of sensor and actuator in polymer and metal based composites
7. Global temperature measurement of aluminum alloy specimens with embedded optical fibers
8. Fabrication of intelligent aluminum matrix composite