Effort was made to include as much engineering information on each component as possible, consistent with usefulness and catalog size limitations. The contents of this catalog contain components which were qualified for use with spacecraft monopropellant hydrazine and inert gas attitude control systems. Thrust ranges up to 44.5 N (10.0 lbf) for hydrazine and inert gas systems were considered. Additionally, some components qualified for uses other than spacecraft attitude control are included because they are suitable for use in attitude controls systems. (Author)
Attitude Control Propulsion Components, Volume 1
1974
309 pages
Report
No indication
English
Attitude Control Propulsion Components, Volume 2
NTRS | 1974
Attitude Control Propulsion Components, Volume 1
NTRS | 1974
Attitude Control Propulsion Components, Volume 2
NTIS | 1974
Characterization of Attitude Control Propulsion Systems
NTRS | 1971
|Characterization of Attitude Control Propulsion Systems
NTIS | 1971
|