1. A Feasibility Study of Heat-pipe-cooled Leading Edges for Hypersonic Cruise Aircraft;Silverstein,1971
2. Space Shuttle Orbiter Heat Pipe Application;Alario,1972
3. Four space shuttle wing leading edge concepts;Niblock;J. Spacecraft Rockets,1974
4. Analysis and Radiant Heating Tests of a Heat-pipe-cooled Leading Edge;Camarda,1977
5. Application of Formal Optimization Techniques in Thermal/structural Design of a Heat-pipe-cooled Panel for a Hypersonic Vehicle;Camarda,1987