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VOLUME ANE5 MARCH 1958 NUMBER
An EvaporativeGravity Technique for Airborne Equipment Cooling
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Aeronautical and Navigational air traffic control airborne aircraft altitude angle angular antenna approach automatic aviation axis azimuth beacon Busignies Capacitors cent cold plate collision components convection coolant cooling system craft Dayton device direction dissipation Doppler East Coast Conference electrical electronic equipment engineer equation error feet flight flow frequency function glide glide slope glide-slope gyro heat exchanger heat transfer indicated inertial inertial space input installation instrument landing system Laboratory landing system liquid loop maximum measured ment modulation navigation systems Navigational Electronics obtained operation output paper path performance PGANE phase pilot plane position problem pulse radar radiation radio range received runway Schuler tuning shown in Fig signal space speed surface Tacan target technical techniques temperature tests thermal thermocouple tion torque touchdown Trans transistors transmitted tube unit vacuum tube vector velocity vertical voltage Vortac weight zero