THERMAL VACUUM TEST OF ORBITAL STATIC MOISTURE-REMOVAL FUEL CELL.
AIR FORCE AERO PROPULSION LAB WRIGHT-PATTERSON AFB OHIO
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The report presents the results of a thermal vacuum chamber test of an orbital fuel cell of advanced design. The fuel cell package used a static moisture-removal system. The fuel cell, tested in the thermal vacuum chamber at Wright-Patterson AFB, gave satisfactory results. This test constituted the second and final ground qualification of this orbital fuel cell prior to orbital test. Author