Presents dynamic thermal simulation results for a reusable inflatable atmospheric decelerator during atmospheric entry and descent from low Earth orbit, using MuSES to evaluate heating environments and structural thermal performance.

Presents a methodology for generating multimodal (EO/IR) synthetic imagery of terrestrial scenes including human subjects using MuSES, providing realistic training data for artificial intelligence and machine learning applications.

Applies YOLO-based deep learning models trained on MuSES-generated synthetic OPIR imagery to automatically detect and identify ground vehicles, demonstrating the utility of synthetic data for developing military target recognition systems.

Conducts a sensitivity analysis on the key parameters affecting the electro-optical and infrared signature of orbiting satellites using MuSES, identifying the dominant factors for signature prediction and satellite design trade-offs.

Evaluates the thermal damage and survivability of satellites subjected to directed energy laser weapon strikes using MuSES thermal simulation, providing physics-based insights into laser effects on orbital assets.

Presents high-fidelity dynamic predictions of electro-optical and infrared satellite signatures using MuSES simulation, demonstrating the capability to generate realistic time-varying signature data for space situational awareness applications. Learn More…

Develops a methodology that couples advanced orbit propagation with high-fidelity 3D thermal-electrical simulation to optimize satellite structural durability and predict component lifetime under realistic on-orbit thermal cycling conditions. Learn More…

Presents a coupled simulation approach that combines a 3D vehicle thermal model, a human thermal comfort model, a battery thermal-electrical model, and a drive cycle model to predict electric vehicle…

Validates a thermal simulation methodology for small satellites by comparing high-fidelity 3D thermal model predictions against on-orbit temperature measurements, demonstrating the approach’s accuracy for spacecraft thermal design. Learn More…