PERANCANGAN AKUISISI DATA SUMBER INFRA MERAH SEBAGAI AWAL PENELITIAN SISTEM SEEKER BERBASIS INFRA MERAH

Abstract

Diagnostic tool in the thermal imaging using the thermovision has been developed to characterize the plume gas of solid AP-HTPB rocket propellant. The data Acquisition of the infrared source has been developed based on microcontroller and labview as a Software. This software can increase the capability of the thermovision camera with the real time process. Infrared source BaF2 was used as an object and this test has given the result: voltage 1.8 volt, thermal 390 Kelvin, and can be converted to 7-8 um wavelength. In the future, this system can be integrated with the actuator robotic or the fin of the rocket. Key words: Rocket plume, Acquisition, Infrared, Thermovision