Heat transfer software and fluid flow software
   


 SINDA/FLUINT
 Sinaps
 Thermal Desktop
 RadCAD
 FloCAD
 Utilities
 Applications
 Turbomachines
 Electronics
 Cryogenics
 Vapor Compression
 Two-Phase Flow
 Regenerators and  
 Cryocoolers
 JT Cooling
 Heatpipes and LHPs
 Waterhammer
 Thermoelastic
 Stratified Tank
 Thermoelectric
 Thermal Ablation
 Integrated Analysis
 Valve Response
 Shadow Tracking
 Material Flow
Turbocharger
Nozzle Plume Heating
Compartment Venting

 




 




propulsion analysis and design

Liquid Propulsion Modeling an Fluid Flow Design

The NASA standard tool for heat transfer and fluid flow analysis, SINDA/FLUINT, includes thermodynamic and hydrodynamic solutions specifically targeted at the growing demand for design and analysis of liquid propulsion systems.

Many organizations have previously used separate in-house tools specialized for each of the above applications. However, these organizations typically do not have the resources nor infrastructure to maintain these codes when cognizant engineers are lost, nor to modify and validate them for new vehicles or applications, nor to train new engineers on their use. The use of a single general-purpose tool to encompass all such analyses offers not only solutions to these problems, but also enables integrated analyses and the ability to communicate with vendors and customers.

An extensive set of generalized thermal/fluid modeling tools exists that was developed to satisfy the specialized needs of liquid propulsion system design and analysis. These tools can uniquely provide integrated modeling of an entire fuel tank system including pressurization system, feedline, and turbopump. They can also link intimately with thermal models of the structure and environment. Included are high-level design synthesis, statistical design, and model correlation modules. An extensive infrastructure exists of pre- and postprocessing software, training, and user support. While the models made using these tools might be proprietary, the tools themselves are readily available to all organizations, overcoming significant limitations of in-house codes.

Propulsion design applications include:

  • Helium pressurization system design
  • Cryogenic line chilldown transients
  • Regenerative nozzle cooling
  • Cryogenic turbomachinery chilldown transients
  • Hydrazine line filling
  • Feed-line transients, including pogo suppression
  • Feedline anti-geyser design
  • Cryogenic tank pressurization and discharge, including thermal stratification, dissolved pressurant, and capillary liquid acquisition devices

More Information:

 

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For further information, please contact C&R Technologies

 

 



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