Continuation of AA 236A. This course focuses on the design and implementation of spacecraft deployable structure systems. Students will work in teams to propose a solution for a large deployable structure for small satellites. Students will demonstrate that their design meets functional, mechanical, and environmental requirements using analysis, prototyping, and testing. Prerequisite: AA 236A or consent of instructor.
4 units · Letter (ABCD/NP)
Continuation of AA 236A. This course focuses on the design and implementation of spacecraft deployable structure systems. Students will work in teams to propose a solution for a large deployable structure for small satellites. Students will demonstrate that their design meets functional, mechanical, and environmental requirements using analysis, prototyping, and testing. Prerequisite: AA 236A or consent of instructor.
Offered in Winter 2026 at Stanford University.