Design of a subscale propellant slag evaluation motor using two-phase fluid dynamic analysis
Author:
Affiliation:
1. ERC, Inc., Huntsville, AL
2. NASA, Marshall Space Flight Center, Huntsville, AL
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1996-2780
Reference14 articles.
1. Reusable Solid Rocket Motor (RSRM) pressure perturbation characterization - An overview
2. Aluminum Agglomeration in Solid-Propellant Combustion
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1. Update: A Subscale Solid Rocket Motor for Characterization of Submerged Nozzle Erosion;45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2009-08-02
2. Design of a Solid Rocket Motor for Characterization of Submerged Nozzle Erosion;44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2008-07-21
3. Numerical investigation of 3D two-phase turbulent flows in solid rocket motors;34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit;1998-07-13
4. Numerical analysis of the turbulent flow and alumina particle trajectories in solid rocket motors;33rd Joint Propulsion Conference and Exhibit;1997-07-06
5. Application of two-phase CFD analysis to the evaluation of asbestos-free insulation in the RSRM;33rd Joint Propulsion Conference and Exhibit;1997-07-06
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