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Numerical Base Heating Sensitivity Study for a Four-Rocket Engine Core Configuration

  • Published:2013-05 Issue:3 Volume:50 Page:509-526
  • ISSN:0022-4650
  • Container-title:Journal of Spacecraft and Rockets
  • language:en
  • Short-container-title:Journal of Spacecraft and Rockets

Author:

Mehta Manish1,Canabal Francisco1,Tashakkor Scott B.2,Smith Sheldon D.3

Affiliation:

1. Aerosciences Branch, NASA Marshall Space Flight Center, Huntsville, Alabama 35812

2. Aerosciences Branch, Jacobs Engineering Science and Technical Services Group, Huntsville, Alabama 35812

3. Aerosciences Branch, Jacobs Engineering Science and Technical Services Group–Plumetech, Huntsville, Alabama 35812

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Reference28 articles.

1. MullenC. R.BenderR. L.BevillR. L.ReardonJ.HartleyL. “Saturn Base Heating Handbook,” NASA CR-61390, May 1972.

2. Space Shuttle base heating

3. Loci: a rule-based framework for parallel multi-disciplinary simulation synthesis

4. Verification of RANS Turbulence Models in Loci-CHEM using the Method of Manufactured Solutions

5. GoethertB. H. “Base Flow Characteristics of Missiles with Cluster-Rocket Exhausts,” Institute of Aeronautical Sciences (IAS) Paper 60-89, 1960.

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