A feasibility study of heat-pipe-cooled leading edges for hypersonic cruise aircraft
NASA contractor report ; CR-1857
1971
IX, 141 S
graph. Darst
Contract no. NAS 1-9872
Report
Englisch
Heat-Pipe-Cooled Leading Edges for Hypersonic Vehicles
NTIS | 2006
|Heat-Pipe-Cooled Leading Edges for Hypersonic Vehicles
NTRS | 2006
|