DocumentCode :
3773359
Title :
Boron nitride utilization in radomes
Author :
R. O. Howe
Author_Institution :
Aerophysics Department Missile Systems, Division Raytheon Company, Bedford, Massachusetts
fYear :
1967
Firstpage :
175
Lastpage :
178
Abstract :
Effective interceptor type homing guided missiles must operate at velocities of more than three thousand feet a second in the atmosphere. Developments and studies have indicated that certain of these may eventually be operational in the velocity regime of six to more than eight thousand feet a second. This operational regime is different from the exo-atmospheric regime with a re-entry type vehicle, which encounters its own set of environmental problems.
Keywords :
"Temperature","Tensile stress","Silicon compounds","Boron","Dielectrics","Shape","Electromagnetics"
Publisher :
ieee
Conference_Titel :
Electrical Insulation Conference, 1967 Seventh
Print_ISBN :
978-1-5090-3106-1
Type :
conf
DOI :
10.1109/EIC.1967.7468798
Filename :
7468798
Link To Document :
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