An analysis and definition at subsystem level is presented for the spacecraft which forms ESA's contribution to a joint ESA/NASA Jupiter swingby out-of-ecliptic mission. Subsystems considered are: telecommunications data handling, power supply, attitude and orbit control, thermal control, structure, and booms. A reliability and safety analysis is included.
Solar out-of-Ecliptic Study. Volume 3: Subsystem Analysis and Definition
1976
219 pages
Report
Keine Angabe
Englisch