Project NXP

Project NXP

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Aerospace Company

01/05/2022

LET ME JUST THROW LITTLE LIGHTS ON ROCKETS
Rockets are gas propelled vehicles to space
It is challenging to determine the propulsion force of rocket engines theoretically, but if followed these tips, you can be accurate in your findings.
To find the propulsion force of rocket engines theoretically, you have to consider a lot;
1. The Rocket Engine/Rocket design
2. The fuel constituent elements
3. Solve out a balanced chemical reaction of its combusting constituents
4. Find specific heat capacity of its combust products
5. Find change in temperature of reaction
6. Find the fuel discharge
7. Find the heat change (heat of combustion)
8. Pressure generated by this reaction in engine design confined combustion chamber space using your Partial Pressure Law, Boyles/Charles laws with respect to the above findings and its force of escape through the nuzzle of the rocket with respect to nuzzle cross sectional area.
9 . Doing all these consider the melting point of the rocket engine material.
With all this in mind, you can archive even hypersonic speed in your design.

Read more from my book

Photos from Project NXP's post 01/05/2022

LET ME JUST THROW LITTLE LIGHTS ON ROCKETS
Rockets are gas propelled vehicles to space
It is challenging to determine the propulsion force of rocket engines theoretically, but if followed these tips, you can be accurate in your findings.
To find the propulsion force of rocket engines theoretically, you have to consider a lot;
1. The Rocket Engine/Rocket design
2. The fuel constituent elements
3. Solve out a balanced chemical reaction of its combusting constituents
4. Find specific heat capacity of its combust products
5. Find change in temperature of reaction
6. Find the fuel discharge
7. Find the heat change (heat of combustion)
8. Pressure generated by this reaction in engine design confined combustion chamber space using your Partial Pressure Law, Boyles/Charles laws with respect to the above findings and its force of escape through the nuzzle of the rocket with respect to nuzzle cross sectional area.
9. Doing all these consider the melting point of the rocket engine material.
With all this in mind, you can archive even hypersonic speed in your design.

Read more from my book

16/02/2021
15/02/2021
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