AI Formulation Brief
Describe your mission profile and requirements. OrbitChem cross-references MAPTIS, ASTM, NASA MSFC, and ESA ECSS databases to generate a formulation intelligence brief with candidate material systems.
ASTM E595 TML & CVCM
Estimate total mass loss (TML) and collected volatile condensable materials (CVCM) for polymer and adhesive systems. Based on Arrhenius outgassing kinetics — test conditions 125°C / 24h / 7×10⁻⁵ Torr.
Total Ionising Dose
Estimate accumulated total ionising dose (TID) for a given orbit, shielding configuration, and mission duration. Uses simplified AP-8/AE-8 belt models with aluminium shielding attenuation.
Fatigue Life Estimate
Estimate adhesive bondline and coating fatigue life under orbital thermal cycling. Uses Coffin-Manson low-cycle fatigue model with CTE mismatch stress analysis.
Spacecraft Material Qualification
Run outgassing, radiation stability, and thermal cycling fatigue against real space-grade material data simultaneously. Powered by the OrbitChem API — physics-based screening to NASA MSFC-SPEC-1238 and ESA ECSS-Q-ST-70 standards.
Space-Grade Materials
38 qualified aerospace materials with calibrated outgassing, radiation, and thermal properties. Data loaded from OrbitChem API.
| Material | Function | VP kPa ↕ | CTE ppm/K ↕ | E GPa ↕ | UTS MPa ↕ | $/kg ↕ |
|---|---|---|---|---|---|---|
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