Spacecraft Systems, Power, Thermal & Space Environments
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Curated Certification CAS06
Integrate spacecraft subsystems across electrical power, thermal control, radiation, structures, mechanisms, propulsion, environmental constraints and verification.
Benchmark: Curated source set: NASA NESC Academy + MIT OpenCourseWare + NASA S3VI -- Credential note: this is a Zuyini mastery certificate built from the cited public courses. It is not issued, sponsored or endorsed by the source institutions, providers or companies.
Core Course Stack
1. Space Solar Arrays - 8 Part Series
2. Thermal Testing and Verification - 5 Part Series
3. Radiation Engineering for Designers - 8 Part Series
4. Overview of Spacecraft Thermal Control
5. Aircraft Systems Engineering - Orbiter Subsystems
6. High Voltage Engineering for Space Applications
7. Thermal Control & Protection Video Catalog
8. Small Spacecraft Systems Engineering Series - Integration & Test
Hands-On Mastery Capstone
Create a preliminary spacecraft subsystem budget and verification plan. Allocate mass, power, thermal and data needs; define subsystem interfaces; model at least one hot/cold or power case; identify radiation/environment risks; and specify integration/test evidence.
Proof Rubric
- subsystem block diagram
- mass/power/data budgets
- thermal case
- environment/radiation assessment
- interface matrix
- verification matrix
- test plan
- margin/risk dashboard