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Learning Rocket Science #Software – Rocket Altitude Calculation Program

roket-irtifa-hesaplama-programi-Rocket Altitude Calculation Program

roket-irtifa-hesaplama-programi

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Introduction

 


Rocket Altitude Calculation Program

Rocket Altitude Calculation Program

Weight Data
Rocket Mass(gr)
Rocket Motor Mass(gr)
Rocket Propellant Mass(gr)

Rocket Area Data
Rocket Body Outer Diameter(mm)

Rocket Motor Data
Rocket Motor Total Thrust(N)
Rocket Motor Burn Time(s)
Rocket Motor Average Thrust(N/s)

Additional Data
Maximum Air Resistance(kg*m/s2)

Propellant-to-Total Mass Ratio(%)


Rocket Velocity Data
Maximum Achieved Velocity(m/s)

Maximum Achieved Velocity(km/h)

Maximum Achieved Velocity(mach)


Time Data
Motor Operating Time(s)

Time to Apogee After Burnout(s)

Time to Apogee from Launch(s)


Altitude Data
Altitude Reached During Burn Time(m)

Altitude Reached After Burnout(m)

Total Altitude(m)


This program was written by Ercan Koçlar.

Published:19.07.2021 / Last Updated:29.08.2024


Rocket Altitude Calculation Program Video


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This post is also available in: Türkçe (Turkish)

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