Astronautical Engineering 552:
Spacecraft Thermal Control (3.0 units)
Spacecraft and orbit thermal environments; design, analysis, testing of spacecraft thermal control system and components; active and passive thermal control, spacecraft and launch vehicle interfaces. Graduate standing in engineering or science.
- Restriction: Registration open to the following class level(s): Master Student, Doctoral Student
Section | Session | Type | Time | Days | Registered | Instructor | Location | Syllabus | Info |
---|---|---|---|---|---|---|---|---|---|
29138R | 048 | Lecture | 6:40-9:20pm | Thursday | 1 of 20 | Ghanshyam Purohit | OHE100B | ||
29168D | 034 | Lecture | 6:40-9:20pm | Thursday | 13 of 40 | Ghanshyam Purohit | DEN@Viterbi |