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
SectionSessionTypeTimeDaysRegisteredInstructorLocationSyllabusInfo
29138R048Lecture6:40-9:20pmThursday1 of 20Ghanshyam PurohitOHE100Bsession dates
29168D034Lecture6:40-9:20pmThursday13 of 40Ghanshyam PurohitDEN@Viterbisession dates
Information accurate as of January 19, 2024 5:02 pm.