How to Calculate Pressure Exerted by an Engine in a Vacuum?

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SUMMARY

The calculation of pressure exerted by an engine in a vacuum, such as during a Mars lander landing, involves understanding both static and dynamic pressure. The fundamental equation P=F/A applies for static pressure, while dynamic pressure is calculated using the formula total pressure = P_hyd + P_stat + 1/2 * Rho * V^2, where V represents bulk velocity. This distinction is crucial for accurately assessing the pressure on the surface due to exhaust in a vacuum environment.

PREREQUISITES
  • Understanding of static pressure and its calculation using P=F/A
  • Knowledge of dynamic pressure and its components
  • Familiarity with fluid dynamics principles
  • Basic physics concepts related to pressure and force
NEXT STEPS
  • Research the principles of fluid dynamics in vacuum environments
  • Learn about the calculation of dynamic pressure and its applications
  • Explore the effects of exhaust velocity on surface pressure during landings
  • Study the implications of pressure calculations for spacecraft design
USEFUL FOR

Aerospace engineers, physicists, and anyone involved in spacecraft design or analysis of pressure dynamics in vacuum conditions will benefit from this discussion.

Space259
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Hello all,

How would I calculate the pressure exerted on a surface by an engine in a vacuum, for example, if a lander was landing on Mars, I'm trying to calculate the pressure exerted on the surface by the exhaust. Should I simply be looking at P=F/A or should I be looking at dynamic pressure?

Thanks in advance
 
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For pressure exerted on a surface by a moving fluid perpendicular to it, the static pressure is equal to the velocity pressure, and p=f/a applies.
 
Last edited:
Hi Russ,

Thanks for your reply, so where does the dynamic pressure come into it? If you were to calculate the Dynamic Pressure what would you be calculating?
 
total pressure = P_hyd + P_stat + 1/2 * Rho * V^2
(V is bulk velocity)
 

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