Aerospace Propulsion

Aerospace Propulsion covers airbreathing engines, rocket performance, thrust chambers, nozzles, and combustion, applying gasdynamics to predict thrust.

no offering record for this termCredits unavailable
Recorded instructors · Spring 2027 No instructors listed

Summary

1 / 2

Lectures are small, with a median of 28 enrolled students in the recorded sections.

Section enrollment · Fall 2026 snapshot ↗

What you’ll be able to do

  • Quantitatively describe the thermodynamics of the different stages of an airbreathing engine

  • Optimize a rocket’s mass distribution

  • Apply basic one-dimensional gasdynamics and combustion fundamentals to predict a rocket’s thrust

  • Report in written form their understanding of aerospace propulsion-related issues not covered in class

Source: UW Guide

Grade history

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average GPA
letter grades

No recorded grade history.

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Prerequisites

Course map

M E/​E M A 425(or M E 572 prior to Fall 2026), graduate/professional standing, or member of Engineering Guest Students

    • take one
    • graduate/professional standing
    • member of Engineering Guest Students
    take one
EMA 426

This is a best-effort interpretation; check the catalog requirements above.

Prerequisite text tree
  • Any of

Professors

Spring 2027

No instructors recorded for this selection.

Historical instructors & teaching patterns

Recorded history may be incomplete and does not establish a future schedule.

Calendar & sections

Spring 2027

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SectionModeEnrolled / capacityWaitlist

Times are Central. Select a meeting for details; export includes recorded dates for the selected sections.

Meeting source records

Student experience

the class

Airbreathing engines. Rocket performance. Thrust chambers, nozzle design criteria. Fundamentals of combustion. Was E M A 524 prior to Fall 2026.

difficulty & workload

No workload feedback recorded.

Topics

  • Airbreathing engines and rocket performance
  • Thrust chambers, nozzle design, and combustion fundamentals
  • One-dimensional gasdynamics for thrust prediction

Skills

  • Quantitative description of airbreathing engine stage thermodynamics
  • Rocket mass distribution optimization
  • Predicting rocket thrust using one-dimensional gasdynamics and combustion
  • Written reporting on aerospace propulsion issues

Grades

Instructor

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Sources & history

UW–Madison

Catalog & offerings

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Model outputs & technical records
Qwen/Qwen3.8-27B
LLM outputs across runs
Full model traces

Recorded model configuration, reasoning, and tool conversations.

Model & dataset provenance
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  "task_version": "17",
  "output_id": "37060913ce94520b2c3ff937179284bb1728457dc57a141032b7685afe921f75",
  "requirements_status": "needs_review",
  "dataset_revision": "fc1811fa52e581ea57a35c0cf3343f8740a8ffbf",
  "observed_at": "2026-10-14 17:50:09.728220+00:00"
}