Photon Propulsion Thrust Solution

STEP 0: Pre-Calculation Summary
Formula Used
Thrust = 1000*Power in Jet/[c]
F = 1000*Pe/[c]
This formula uses 1 Constants, 2 Variables
Constants Used
[c] - Light speed in vacuum Value Taken As 299792458.0
Variables Used
Thrust - (Measured in Newton) - Thrust is the force produced by the expulsion of high-speed exhaust gases from a rocket engine.
Power in Jet - (Measured in Watt) - Power in Jet is the amount of power providing thrust through the propelling nozzle.
STEP 1: Convert Input(s) to Base Unit
Power in Jet: 1746392 Kilowatt --> 1746392000 Watt (Check conversion ​here)
STEP 2: Evaluate Formula
Substituting Input Values in Formula
F = 1000*Pe/[c] --> 1000*1746392000/[c]
Evaluating ... ...
F = 5825.33667341291
STEP 3: Convert Result to Output's Unit
5825.33667341291 Newton --> No Conversion Required
FINAL ANSWER
5825.33667341291 5825.337 Newton <-- Thrust
(Calculation completed in 00.004 seconds)

Credits

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Created by Chilvera Bhanu Teja
Institute of Aeronautical Engineering (IARE), Hyderabad
Chilvera Bhanu Teja has created this Calculator and 300+ more calculators!
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Verified by Vaibhav Malani
National Institute of Technology (NIT), Tiruchirapalli
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Thrust and Power Generation Calculators

Power required to produce Exhaust Jet Velocity
​ LaTeX ​ Go Power Required = 1/2*Mass Flow Rate*Exit Velocity^2
Thrust given Exhaust Velocity and Mass Flow Rate
​ LaTeX ​ Go Thrust = Mass Flow Rate*Exit Velocity
Thrust given Mass and Acceleration of Rocket
​ LaTeX ​ Go Thrust = Mass of Rocket*Acceleration
Acceleration of Rocket
​ LaTeX ​ Go Acceleration = Thrust/Mass of Rocket

Photon Propulsion Thrust Formula

​LaTeX ​Go
Thrust = 1000*Power in Jet/[c]
F = 1000*Pe/[c]

What is thrust?

Thrust is a reaction force, When a system expels or accelerates mass in one direction, the accelerated mass will cause a force of equal magnitude but in opposite direction, to be applied to that system. The force applied on a surface in a direction perpendicular to the surface is also called thrust.

How to Calculate Photon Propulsion Thrust?

Photon Propulsion Thrust calculator uses Thrust = 1000*Power in Jet/[c] to calculate the Thrust, Photon Propulsion Thrust formula is defined as a measure of the thrust generated by a spacecraft using photon emissions. It illustrates the relationship between emitted power and the resulting force, highlighting the principles of momentum transfer in space propulsion systems. Thrust is denoted by F symbol.

How to calculate Photon Propulsion Thrust using this online calculator? To use this online calculator for Photon Propulsion Thrust, enter Power in Jet (Pe) and hit the calculate button. Here is how the Photon Propulsion Thrust calculation can be explained with given input values -> 5824.67 = 1000*1746392000/[c].

FAQ

What is Photon Propulsion Thrust?
Photon Propulsion Thrust formula is defined as a measure of the thrust generated by a spacecraft using photon emissions. It illustrates the relationship between emitted power and the resulting force, highlighting the principles of momentum transfer in space propulsion systems and is represented as F = 1000*Pe/[c] or Thrust = 1000*Power in Jet/[c]. Power in Jet is the amount of power providing thrust through the propelling nozzle.
How to calculate Photon Propulsion Thrust?
Photon Propulsion Thrust formula is defined as a measure of the thrust generated by a spacecraft using photon emissions. It illustrates the relationship between emitted power and the resulting force, highlighting the principles of momentum transfer in space propulsion systems is calculated using Thrust = 1000*Power in Jet/[c]. To calculate Photon Propulsion Thrust, you need Power in Jet (Pe). With our tool, you need to enter the respective value for Power in Jet and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.
How many ways are there to calculate Thrust?
In this formula, Thrust uses Power in Jet. We can use 2 other way(s) to calculate the same, which is/are as follows -
  • Thrust = Mass Flow Rate*Exit Velocity
  • Thrust = Mass of Rocket*Acceleration
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