PARAGON SPACE DEVELOPMENT CORPORATION — National Aeronautics and Space Administration SBIR Phase I: Z10

Description

Paragon proposes an Ellipsoidal Propellant Tank (EPT) inflatable cryogenic tank structure that will provide up to 30% mass savings compared to existing composite systems. EPT extends knowledge from prior NASA funded Ultra-High-Performance-Vessel (UHPV) development to deep cryogenic, ellipsoidal, inflatable propellant structures. UHPV utilizes multiple layers including unloaded inner barrier material, minimally loaded carrier cloth, and primary load bearing meridional tendons. This allows each material to be optimized for its functional contribution to the system leading to an overall simpler and lower mass solution. Prior work has proven UHPV feasibility for the barrier material intended for EPT and the utility of our complementary CELSIUS conformal, deployable cryogenic tank insulation. UHPV is most optimal in ellipsoidal configurations and in EPT Phase I we determine the feasibility of UHPV for large, high pressure, cryogenic tank structures by completing a conceptual design, performing more detailed hull, barrier, and interface design, and demonstrating a subscale barrier film EPT including helium leak testing. nbsp;