Mariner spacecraft have completed five missions of scientific investigation of the planets. Two additional missions are planned. A description of the thermal design of these seven spacecraft is given herein. The factors which have influenced the thermal design include the mission requirements and constraints, the flight environment, certain programmatic considerations and the experience gained as each mission is completed. These factors are reviewed and the impact of each on thermal design and developmental techniques is assessed. It is concluded that the flight success of these spacecraft indicates that adequate temperature control has been obtained, but that improvements in design data, hardware performance and analytical techniques are needed.
Temperature control of the Mariner class spacecraft - A seven mission summary.
Thermophysics Conference ; 1973 ; Palm Springs, CA
1973-07-01
Conference paper
No indication
English
Temperature control of mariner v spacecraft
Engineering Index Backfile | 1968
|Temperature control of the Mariner V spacecraft.
NTRS | 1968
|Engineering Index Backfile | 1965
|