Astronautical Engineering 557:

Spacecraft Structural Strength and Materials (3.0 units)

Spacecraft structural strength analysis and design concepts overview; spacecraft material selection; analysis of composite materials; finite element method; spacecraft configuration; structural testing; bolted joint design.
  • Restriction: Registration open to the following class level(s): Master Student, Professional Year 1, Doctoral Student
SectionSessionTypeTimeDaysRegisteredInstructorLocationSyllabusInfo
29172D034Lecture7:00-9:40pmThursday18 of 30Robert WilliamsDEN@ViterbiPDF (191875 KB)feesession datesbook list
Information accurate as of October 10, 2019 11:02 am.