Spacecraft Thermal Analysis

Application ID: 109811


This model demonstrates how to compute satellite temperature over multiple orbit periods by coupling Orbital Thermal Loads to Heat Transfer in Solids. The direct solar, albedo, and Earth infrared thermal loads are computed over a single orbit, and are periodically repeated over multiple orbits.

この model の例は, 通常次の製品を使用して構築されるこのタイプのアプリケーションを示しています.