The test bed fabricated to demonstrate hydrogen/oxygen propulsion technology readiness for the IOC Space Station application is described and test results are presented. The reliability and safety of the O2/H2 system was demonstrated with blowdowns and thruster firings. The flexibility of the system was demonstrated through the addition of an electrolysis supply module.
Space Station propulsion system test bed and control system testing results
1987-06-01
Conference paper
No indication
English
Space station propulsion system test bed and control system testing results
Tema Archive | 1987
|Space Station propulsion system test bed
NTRS | 1988
|