A deployment actuator mechanism was developed to drive a two-axis gimbal assembly and a high-gain antenna to a deployed and locked position on the Jet Propulsion Laboratory Ocean Topography Experiment (TOPEX) satellite. The Deployment Actuator Mechanism requirements, design, test, and associated problems and their solutions are discussed.
Topex high-gain antenna system deployment actuator mechanism
1991-05-01
Conference paper
No indication
English
The Galileo high gain antenna deployment anomaly
NTRS | 1994
|The Galileo High Gain Antenna Deployment Anomaly
British Library Conference Proceedings | 1994
|Topex Satellite Concept. Topex Option Study Report
NTIS | 1982
|