An analytical rationale is presented for the configuration of the NASA Space Station's two-element propulsion system, and attention is given to the cost benefits accruing to this system over the Space Station's service life. The principal system element uses gaseous oxygen and hydrogen obtained through water electrolysis to furnish attitude control, backup attitude control, and contingency maneuvering. The secondary element uses resistojets to augment Space Station reboost through the acceleration of waste gases in the direction opposite the Station's flight path.
Selection of combined water electrolysis and resistojet propulsion for Space Station Freedom
01.10.1988
Aufsatz (Konferenz)
Keine Angabe
Englisch
Space Station Freedom resistojet system study
NTRS | 1989
|Space Station Freedom resistojet system study
AIAA | 1989
|