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power-systems

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Ship power budgets, solar sizing, and EPS design.

Education & Research#eps#power-system#eclipse#energy-balance#battery-sizing#spacecraft#solar-array
Authordevideamax
Version1.0.0
Installs0

System Documentation

What problem does it solve?

Spacecraft EPS design involves sizing solar arrays, selecting energy storage, and ensuring reliable power across maneuvering and eclipse cycles. This Skill provides a structured methodology to model, size, and validate EPS subsystems for any mission profile, from CubeSats to deep-space probes.

Core Features & Use Cases

  • EPS sizing and bus architecture decisions for varying orbits
  • Eclipse energy balance, DoD, and cycle-life aware battery selection
  • End-to-end power budgets with margin checks and energy balance verification
  • Cross-skill connectors with orbital-mechanics, thermal, and mission-architect data
  • Use Case: design a 6U CubeSat power system for a 2-year mission in LEO

Quick Start

Trigger orbit, payload power profile, and mission life to generate a complete EPS design in minutes.

Dependency Matrix

Required Modules

None required

Components

Standard package

💻 Claude Code Installation

Recommended: Let Claude install automatically. Simply copy and paste the text below to Claude Code.

Please help me install this Skill:
Name: power-systems
Download link: https://github.com/devideamax/aerospace-team/archive/main.zip#power-systems

Please download this .zip file, extract it, and install it in the .claude/skills/ directory.
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