Analyze rocket propulsion systems to optimize engine selection and delta-v budgets.
npx skills add https://github.com/devideamax/aerospace-team --skill propulsion
Please help me install this Agent Skill. Skill: propulsion Source: https://github.com/devideamax/aerospace-team/tree/main/skills/propulsion Command: npx skills add https://github.com/devideamax/aerospace-team --skill propulsion
Expert rocket propulsion analysis — engine selection, delta-v budgets, staging optimization, mission architecture, and propellant trade studies. Use when designing launch vehicles, evaluating propulsion systems, and reviewing mission feasibility.
Trigger the propulsion skill with a mission brief: specify your destination, payload mass, and reusability goals to generate a complete propulsion architecture.
High-intent search queries and answers about installing and using this skill.
Calculate delta-v budgets by computing mass ratios, accounting for losses, and evaluating orbit feasibility for your mission. Provide reliable engine data and staging constraints to ensure accurate performance models.
Compare rocket engines by evaluating propulsion options against your specific mission requirements to select the best-fit engines. Apply staging constraints and performance models to ensure the selected engines meet your mission architecture.
Optimize staging by determining optimal stage counts, mass splits, and thrust requirements for your launch vehicle. Specify your destination, payload mass, and reusability goals to generate a complete propulsion architecture.
Yes, you can conduct propellant trade studies by evaluating different propellant choices for performance, cost, and risk. This integrates with overall vehicle design and mission feasibility to ensure accurate results.
Yes, reliable engine data and staging constraints are required for accurate rocket propulsion analysis. Apply these inputs alongside performance models to ensure accurate results for mission planning and stage sizing.
Mission architecture requires integrating propulsion with overall vehicle design to review mission feasibility. This ensures engine selection, delta-v budgets, and staging optimization align with your launch vehicle constraints.
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