PERFORMANCE ANALYSIS OF LINEAR AEROSPIKE NOZZLE USING COMPUTATIONAL STUDY

• Author(s):

  C. Ted Solomon | Dr. P. Vasanthakumar

• Keywords:

  SSTO, Launch Vehicle, Linear Aerospike, ANSYS.

• Abstract:

  As We All Know The Importance And Need For Space Transportation In The Upcoming Days. The Requirement For Launch Vehicle Has Increased Drastically. So, SSTO Based Launch Vehicles Are Required In Order To Achieve Our Missions In A Cost Effective And Afford

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Other Details

• Paper id:

  IJSARTV6I638027

• Published in:

  Volume: 6 Issue: 6 June 2020

• Publication Date:

  2020-06-28

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