1. Glass DE, Merrigan MA, Sena JT, Reid RS (1998) Fabrication and testing of a leading-edge-shaped heat pipe [R]. NASA CR-1998-208720, October
2. Glass DE, Merrigan MA, Sena JT (1998) Fabrication and testing of mo-re heat pipes Embedded in carbon/carbon [R]. NASA CR-1998-207642, March
3. Glass DE, Merrigan MA, Sena JT, Reid RS (1998) Fabrication and testing of a leading-edge-shaped heat pipe [R]. NASA CR-1998-208720, October
4. Glass DE, Camarda CJ (1992) Preliminary thermal/structural analysis of a carbon/carbon refractory- metal heat-pipe-cooled wing leading edge [M]. Thermal structures and materials for high-speed Flight. In: Thornton EA (ed) Progress in astronautics and aeronautics. AIAA, New York, pp 301–322
5. Curry DM (1993) Space shuttle orbiter thermal protection system design and flight experience [C]. In: 1st ESA/ESTEC workshop on thermal protection systems, ESA/ESTEC