TEST ARTICLES FOR SOUNDING ROCKETS

• Author(s):

  Sourav Chand

• Keywords:

  Burn Rate, Burn Rate Coefficient, Burn Rate Exponent, Total Impulse, Burn Time, Nominal Thrust, Specific Impulse, Exhaust Velocity, Acceleration, Propellant Weight, Web Thickness, Casing Thickness, Factor Of Safety, Casing Outer Diameter, Casing Inner Dia

• Abstract:

  This Paper Details The Designing Of An M-class Solid Rocket Engine For Testing Purposes And A Stage Separation Mechanism For A Two-stage Sounding Rocket.Designing Of The Motor Was Completed By Hand Calculations And Analysis Was Done With The Help Of Vario

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Other Details

• Paper id:

  IJSARTV7I850525

• Published in:

  Volume: 7 Issue: 8 August 2021

• Publication Date:

  2021-08-18

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