Impact Factor
7.883
Call For Paper
Volume 12 Issue 07
July 2026
Download Paper Format
Copyright Form
Author(s)
Sourav Chand
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
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
Paper ID
IJSARTV7I850525
Publication Date
August 18, 2021
Research Area
Mechanical Engineering