Evaluate spacecraft structural sizing and safety margins under launch loads.
npx skills add https://github.com/devideamax/aerospace-team --skill structural-devideamax
Please help me install this Agent Skill. Skill: structural Source: https://github.com/devideamax/aerospace-team/tree/main/skills/structural Command: npx skills add https://github.com/devideamax/aerospace-team --skill structural-devideamax
This skill enables engineers to perform rigorous structural sizing and safety evaluations for spacecraft primary and secondary structures under launch loads, reducing manual calculation time while ensuring design robustness.
Provide spacecraft mass, launch vehicle, and desired structure type to receive a complete structural analysis and margin-of-safety assessment.
High-intent search queries and answers about installing and using this skill.
Spacecraft margin of safety calculations evaluate combined axial and lateral launch loads against material strength and buckling limits. This skill outputs stress margins and mass estimates for monocoque, sandwich, and truss configurations to verify structural robustness.
Buckling checks for thin-walled cylinders compare applied launch loads against critical buckling stress limits. This skill performs hand-calculated buckling evaluations and outputs safety margins compliant with ECSS-E-ST-32C and NASA-STD-5001B structural requirements.
Spacecraft material selection balances strength, weight, thermal compatibility, and outgassing requirements. This skill provides material selection guidance with explicit margin calculations to ensure structural integrity under launch loads while meeting system mass budgets.
Hand-calculated stress and buckling checks for sandwich panels are supported by this skill. It applies ECSS and NASA margins to evaluate combined launch loads, providing stress, buckling margins, and mass estimates for preliminary structural sizing decisions.
Structural analysis performed by this skill meets both ECSS-E-ST-32C and NASA-STD-5001B requirements. It evaluates monocoque, sandwich, and truss configurations under launch loads, outputting compliant stress, buckling margins, and mass estimates.
Spacecraft structural sizing requires spacecraft mass, launch vehicle specifications, and desired structure type as inputs. This skill then delivers a complete structural analysis, including stress checks, buckling margins, and mass estimates for design decisions.
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