Atmospheric Entry Thermal Protection Simulator

Multi-Planet Hypersonic Shockwave & 1D Transient Heat Diffusion Engine

Telemetry Summary Successful Entry

Peak Surface Temp 1680 K
Max Bondline Temp 385 K
Peak Heating Flux 112.4 W/cm²
Peak Deceleration 4.20 g
Entry Survival Status Successful Entry
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