Deterministic Exit-weight wing loading WL = W_lbs / A_sqft scaled by inverse density ratio (rho_sl / rho_da) dynamic-pressure flare equivalence & USPA SIM experience chart engine (.json, .pdf) built for Performance Designs Sabre3, Jyro / NZ Aerosports, Aerodyne Pilot, Alti-2 — zero-upload ephemeral Wasm RAM execution.
Running ephemeral Wasm verification…