A titanium-lined composite overwrapped pressure vessel (COPV) for Xenon storage was designed for the ETS VIII spacecraft. This tank has a nominal propellant volume of 50 liters (3050 cubic inches) and a nominal weight of 7 kg (15.4 pounds). The maximum expected operating pressure is 150 bar (2175 psi), 50 cycles. Proof pressure requirement is 187.5 bar (2719 psi), 5 cycles, and the minimum burst pressure is 225 bar (3264 psi). The tank is designed to hold 89 kg (196 pounds) of Xenon. The ETS VIII Xenon tank design is based on a flight-qualified Xenon tank to take advantage of its design and flight heritage. To minimize risk, the ETS VIII Xenon tank is designed to use only existing manufacturing technology. Manufacturing cost is minimized by using existing tooling. Nonlinear material and geometric modeling techniques were used to analyze this tank. Stress analysis showed positive margins of safety for pressure cycle fatigue, vibration fatigue and minimum burst pressure over the design requirements. Development and Qualification testing verified the design margins and showed the design analyses to be conservative. The liner is constructed from 6AL-4V titanium. This material was chosen due to heritage and for its superb manufacturability, relative high strength, excellent corrosion and oxidation resistance characteristics, good low and high cycle fatigue characteristics, and competitive manufacturing cost. The overwrap consists of high strength Torayca T1000GB carbon fiber and Epon 826 cured resin system. Several composite layers were applied, including helical and hoop wraps. A leak-before-burst (LBB) demonstration program was conducted to verify the LBB characteristics of the Xenon tank. A complete qualification program was conducted to verify the tank design, including a destructive burst pressure test. The tank successfully completed qualification testing on 10 September 1999. The production program completed in December 1999.