Session
Technical Session IV: Hardware in Space
Abstract
WEBERSAT, a 27 pound LEO satellite launched by the Ariane 40 on January 21, 1990 into an 800 Km polar orbit, carries several inexpensive payload experiments that were developed as a learning experience for engineering students at Weber State College. The experiments include a color CCD camera, a CCD light spectrometer, video flash digitizer, 1.26 GHz NTSC video uplink, micro-impact sensor, and optical horizon sensors. Operational command and control of the spacecraft and its payloads is performed by students in the School of Technology, from a ground station located on the WSC campus. Here, the students and their advisors monitor on-board systems, plan and execute experiments, and observe test results. This paper describes the satellite experiments, ground station requirements, and experiment results as of this date.
WEBERSAT Operations and Experiment Results
WEBERSAT, a 27 pound LEO satellite launched by the Ariane 40 on January 21, 1990 into an 800 Km polar orbit, carries several inexpensive payload experiments that were developed as a learning experience for engineering students at Weber State College. The experiments include a color CCD camera, a CCD light spectrometer, video flash digitizer, 1.26 GHz NTSC video uplink, micro-impact sensor, and optical horizon sensors. Operational command and control of the spacecraft and its payloads is performed by students in the School of Technology, from a ground station located on the WSC campus. Here, the students and their advisors monitor on-board systems, plan and execute experiments, and observe test results. This paper describes the satellite experiments, ground station requirements, and experiment results as of this date.
