AN EXPERIMENTAL EVALUATION OF METALLIC DIAPHRAGMS FOR POSITIVE FUEL EXPULSION IN THE ATMOSPHERE EXPLORER HYDRAZINE PROPULSION SUBSYSTEM

摘要

Four Arde conospheroid metallic diaphragms were tested at Goddard Space Flight Center to evaluate their capability for use in the orbit adjust propulsion subsystem (OAPS) of the Atmosphere Explorer spacecraft. The diaphragms will be used for positive propellant expulsion and spacecraft center of mass control. A leak-free cycle life capability of nine reversals was demonstrated. The diaphragms rolled smoothly from ring to ring in a predictable manner on the first reversal. Varying amounts of diaphragm cocking and ring skipping were observed on subsequent reversals. The diaphragm pressure differential did not exceed 7 N/cm2 (10 psid) during any reversal. Cycle life capability, reversal mode, and pressure differential were not affected by sudden reversals, environmental tests, or 18,000 partial reversals. An expulsion efficiency of approximately 97 percent was demonstrated. The results of these tests show that metallic diaphragms can be used as an effective means of positive fuel expulsion; however, to achieve spacecraft center of mass (cm.) control, the diaphragm must not be reversed prior to flight.