Development tests of LOX/LH2 tank for H-I launch vehicle

The design and preliminary test performance of an integrated LOX/LH2 tank for the second-stage propulsion system of the H-I launch be vehicle being developed by NASDA are presented and illustrated with drawings, diagrams, photographs, graphs, and tables. The tank has length 5.7 m, diameter 2.5 m, and capacity 8.7 tons and is constructed of 2219 Al alloy. The common bulkhead of Al-alloy-covered GFRP honeycomb, identified as the most critical component, has successfully completed extensive mechanical and thermal testing of both subscale and prototype models.