Immutable package version
publiccourseMCF 1.1
Aerospace, Rocket Propulsion and Space Systems 0.2.0
Published by @apv on August 12, 2026.
- Source checksum
4acae63e6b33fce5c8edca15c8811f350ba2c63ed49a70b825aa43ff9b3d148b- Package size
- 922.5 KiB
- Validation
- valid · 0 diagnostics
- Manifest ID
courses.theoria.polytechnical.aerospace-rocket-propulsion-space-systems- Manifest version
- 0.2.0
- Entry
undefined- Language
- en-CA
- License
- CC-BY-4.0
- Authors
- APV, Theoria
- Subjects
- aerospace engineering, flight mechanics, propulsion, orbital mechanics, space systems engineering
- Level
- advanced
- Structure
- 41 lessons · 71 activities · 210 questions
Learning outcomes
- Model aircraft forces, moments, trim, stability, drag polars, performance and compressibility using explicit assumptions and coordinate systems.
- Analyze propeller/jet/rocket propulsion through control-volume momentum, efficiency, nozzle, specific-impulse and architecture reasoning.
- Use rocket equation, staging, mass fractions and ascent-loss budgets to evaluate launch performance at system level.
- Calculate two-body orbits, conserved energy/angular momentum, Hohmann transfers and plane changes.
- Analyze entry energy, ballistic coefficient, deceleration and thermal-protection scaling while respecting model-fidelity limits.
- Represent spacecraft attitude/orbit state, fuse sensors, and design feedback GNC architecture with saturation/fault awareness.
- Close structural, power, thermal, communications and reliability budgets as coupled spacecraft-system decisions.
- Translate scientific needs into requirements, delta-v/resource budgets, trade studies, verification evidence and failure-mode closure.
Release notes
No release notes were provided.
Canonical source is immutable
This release points to the validated source `.mcf.zip`. Browser-compiled learner output is derived and is not treated as repository source.