[{"run_id":"20260906T231458-5fdd2fff","semester":"1272","observed_at":"2026-09-06 23:14:58.172943+00:00","record_version_id":"6958f5b5296691c5031d4c120d3852332c43c671c1b2462e1f947f25d133e81b","course_id":"EMA 426","course_uid":"course_470a1ae93c04b6ff353ec8e4","catalog_version_id":"21e3a08ec46213910479f3851765dda49fd27392ee37e4686f262d180441b087","course_number":426,"subjects":["EMA"],"title":"AEROSPACE PROPULSION","description":"Airbreathing engines. Rocket performance. Thrust chambers, nozzle design criteria. Fundamentals of combustion. Was E M A 524 prior to Fall 2026.","requirements_text":"M E/​E M A  425(or M E 572 prior to Fall 2026), graduate/professional standing, or member of Engineering Guest Students","official_learning_outcomes_json":"[]"},{"run_id":"20260907T155543-ce3781c4","semester":"1272","observed_at":"2026-09-07 15:55:43.033547+00:00","record_version_id":"6958f5b5296691c5031d4c120d3852332c43c671c1b2462e1f947f25d133e81b","course_id":"EMA 426","course_uid":"course_470a1ae93c04b6ff353ec8e4","catalog_version_id":"21e3a08ec46213910479f3851765dda49fd27392ee37e4686f262d180441b087","course_number":426,"subjects":["EMA"],"title":"AEROSPACE PROPULSION","description":"Airbreathing engines. Rocket performance. Thrust chambers, nozzle design criteria. Fundamentals of combustion. Was E M A 524 prior to Fall 2026.","requirements_text":"M E/​E M A  425(or M E 572 prior to Fall 2026), graduate/professional standing, or member of Engineering Guest Students","official_learning_outcomes_json":"[]"},{"run_id":"20261014T203208-0851c9a1","semester":"1274","observed_at":"2026-10-14 17:50:09.728220+00:00","record_version_id":"9b918420a416469c658b73ceb1d7e112881a729c52f43342130844d26a1e74b9","course_id":"EMA 426","course_uid":"course_470a1ae93c04b6ff353ec8e4","catalog_version_id":"63e1e8dedcb0cec268851c005b7165becb60b9ab1c6ce42087c3be8744d2988c","course_number":426,"subjects":["EMA"],"title":"AEROSPACE PROPULSION","description":"Airbreathing engines. Rocket performance. Thrust chambers, nozzle design criteria. Fundamentals of combustion. Was E M A 524 prior to Fall 2026.","requirements_text":"M E/​E M A  425(or M E 572 prior to Fall 2026), graduate/professional standing, or member of Engineering Guest Students","official_learning_outcomes_json":"[{\"catalog_year\":\"2026-2027\",\"observed_at\":\"2026-10-14T17:51:52.399988+00:00\",\"source\":\"catalog\",\"source_url\":\"https://guide.wisc.edu/courses/e_m_a/\",\"term\":null,\"text\":\"Quantitatively describe the thermodynamics of the different stages of an airbreathing engine\"},{\"catalog_year\":\"2026-2027\",\"observed_at\":\"2026-10-14T17:51:52.399988+00:00\",\"source\":\"catalog\",\"source_url\":\"https://guide.wisc.edu/courses/e_m_a/\",\"term\":null,\"text\":\"Optimize a rocket’s mass distribution\"},{\"catalog_year\":\"2026-2027\",\"observed_at\":\"2026-10-14T17:51:52.399988+00:00\",\"source\":\"catalog\",\"source_url\":\"https://guide.wisc.edu/courses/e_m_a/\",\"term\":null,\"text\":\"Apply basic one-dimensional gasdynamics and combustion fundamentals to predict a rocket’s thrust\"},{\"catalog_year\":\"2026-2027\",\"observed_at\":\"2026-10-14T17:51:52.399988+00:00\",\"source\":\"catalog\",\"source_url\":\"https://guide.wisc.edu/courses/e_m_a/\",\"term\":null,\"text\":\"Report in written form their understanding of aerospace propulsion-related issues not covered in class\"}]"}]