PROPULSION SYSTEM CONNECTING APPARATUS FOR DEVICE FOR EXPERIMENTS OF THREE-AXIS ATTITUDE CONTROL SYSTEM OF ARTIFICIAL SATELLITES

摘要

PURPOSE: A propulsion system connecting apparatus is provided to allow a simulation of three-axis attitude control system of artificial satellites to be performed on the ground. CONSTITUTION: A propulsion system connecting apparatus comprises a penetrating clamp and a support clamp for fixing a compressed air tank(4) arranged in a downward direction at the outer surface of a frame(8); a penetrating clamp and a support clamp for fixing a compressed air tank(4') arranged in an upward direction at the outer surface of the frame; and pipelines of the compressed air tanks. The propulsion system connecting apparatus connects the penetrating clamps, support clamps, and the pipeline to a single unit and to thrust units(20,22,23,25) through constant pressure meters(28,29,30).