Dream Chaser

by Stephen Miller, Sierra Nevada Corporation

Thermal analysis of Dream ChaserThe Dream Chaser spacecraft is a reusable, lifting-body vehicle capable of traveling to low Earth orbit and landing on a runway, currently in development by Sierra Nevada Corporation (SNC) Space Systems of Colorado. The engineers at SNC use Thermal Desktop to perform system-level and detailed thermal analysis of the Dream Chaser spacecraft, making use of the following advanced features:

  • The Boundary Condition Mapper is used to map transient reentry heat loads and pressures generated using external computational fluid dynamics (CFD) to the vehicle model.
  •  User-controllable logic (controlled by the Case Set Manager) is used to model non-linear events such as switching on/off avionics boxes and to simplify changing between hot and cold environments.
  • Liquid and gaseous flow loops are simulated using simple one-way thermal networks and FloCAD.
  • Tag Sets are used to simplify connecting assembly-level meshes in the system-level model.
  • The model uses a wide range of thermophysical (anisotropic, temperature- and pressure-dependent) and optical properties.
  • The vehicle’s solar arrays track the sun using Articulators
  • The Stack Manger is used to easily generate aggregate properties for thermal protection system (TPS) multi-material insulation.

Click here to learn more about the Dream Chaser spacecraft

 

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flow regimes

Introduction to Two-phase Flow

September 24, 2-3pm MDT

This webinar introduces basic concepts in two-phase flow modeling including quality, void fraction, flow regimes, slip flow, pressure drops and accelerations, and heat transfer.

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