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