Sealed-Form, Constrictive-Wrapped, External Insulation System for Liquid-Hydrogen Tanks of Boost Vehicles
1963
161 pages
Report
No indication
English
Foamed material , Liquid hydrogen , Propellant tank , Space environment , Thermal insulation , Aerodynamic , Application , Boost , Centaur launch vehicle , Conductivity , Constriction , Cryopumping , Design , External , Fabrication , Fiberglass , Ground , Heating , Impact , Insulation , Launch , Oxygen , Payload , Polyurethane , Propellant , Seal , Sensitivity , System , Tank , Test , Thermal , Vehicle , Wrap