Accession Number : AD0833976

Title :   HIGH TEMPERATURE TEST ON THE MOD III GUIDANCE ANTENNA FOR THE MERCURY VEHICLE,

Corporate Author : GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Personal Author(s) : Moffatt, V. J.

Report Date : 02 DEC 1959

Pagination or Media Count : 19

Abstract : An analysis of the Mercury vehicle guidance antenna indicates that it will experience considerable aerodynamic heating. The purpose of this report is to describe the test performed to determine to what extent the antenna performance will be affected when subjected to the temperatures anticipated. (Author)

Descriptors :   *SATELLITE ANTENNAS), (*MANNED SPACECRAFT, AERODYNAMIC HEATING, ANTENNA COMPONENTS, BONDING, THERMAL STABILITY, ELECTRICAL IMPEDANCE, ANTENNA RADIATION PATTERNS, ENVIRONMENTAL TESTS.

Subject Categories : Electrical and Electronic Equipment
      Manned Spacecraft

Distribution Statement : APPROVED FOR PUBLIC RELEASE