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Anik C

Spacecraft Name
Anik C
COSPAR ID
N/A
Launch Date
1985-04-12 (Anik C1), 1983-06-18 (Anik C2), 1982-11-11 (Anik C3)
Spacecraft Description
N/A

Thermal Analysis

Analysis Object
System
Analysis Description
To cover the distinct mission phases, two thermal models were constructed: one for launch/transfer orbit, and another for synchronous orbit. The results of system level thermal analyses were used as boundary temperatures for the detailed analyses.
Software Used

References