A Study on Sensor Systems for Initiating Parachute Deployment for a MARS Entry Vehicle Final Report
1966
116 pages
Report
No indication
English
Astronautics , Decelerator , Mars probe , Parachute , Sensor , Accelerometer , Aerodynamic , Drag , Entry , Honeycomb , Initiator , Mars , Performance , Pressure , Probe , Reliability , Retrorocket , System , Transducer , Weight