Design, construction, and quality control tests on a dual screen liner device for the space shuttle orbiter cryogenic fuel tank and feedliner system are summarized. The dual stainless steel mesh of the device encloses eight liquid fuel channels and provides the liquid/vapor interface stability required for low gravity orbits.
Acquisition/expulsion system for earth orbital propulsion system study. Volume 1: Summary report
1973-10-01
Report
Keine Angabe
Englisch