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 | 14 of 20 | Ghanshyam Purohit, Dan Erwin | OHE100C | PDF (178927 KB) |   |
| 29168D | 034 | Lecture | 6:40-9:20pm | Thursday | 16 of 20 | Ghanshyam Purohit, Dan Erwin | DEN@Viterbi | PDF (178927 KB) | |