The feasibility of executing major changes upward or downward from the nominal spin rate for which the Pioneer F&G spacecraft was designed was investigated along with the extent of system and subsystem modifications required to implement these mode changes in future spacecraft evolving from the baseline Pioneer F and G. Results of a previous study are re-examined and updated for an extended range of spin rate variations for missions that include outer planet orbiters, outer planet flyby and outer planet probe delivery. However, in the interest of design simplicity and cost economy, major modifications of the baseline Pioneer system and subsystem concept were avoided.
Pioneer spacecraft operation at low and high spin rates
1973-10-05
Report
Keine Angabe
Englisch
Pioneer Venus spacecraft design and operation
NTRS | 1980
|NTIS | 1966
|NTRS | 1966
|NTRS | 1966
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