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- The manufacturing tasks for the program included the fabrication and assembly of an epoxy fiberglass purge bag to encapsulate an insulated cryogenic propellant tank. Purge, repressurization and venting hardware were procured and installed on the purge bag assembly in preparation for performance testing. The fabrication and installation of the superfloc multilayer insulation (MLI) on the cryogenic tank was accomplished as part of a continuing program. An abstraction of the results of the MLI fabrication task is included to describe the complete fabrication requirements for a reusable cryogenic propellant space storage system.
- Other Subject(s):
- NASA Technical Reports Server (NTRS) Collection.
- Document ID: 19730023050.
Accession ID: 73N31782.
- No Copyright.
View MARC record | catkey: 15747633