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AE 267

Space Propulsion Systems

Description
Rocket propulsion fundamentals. propulsion requirements for: multi-stage launch; orbit establishment, maneuvers and maintenance; spacecraft attitude control. Nozzle flow, thermochemical calculation of performance. Design and performance calculations for systems and components of chemical rockets (liquid, solid, hybrid), electric rockets and advanced concepts. Prerequisite: BSAE or Instructor Consent.

Grading
Normal Grade Rules

Units
3