FormulaDen.com
Physics
Chemistry
Math
Chemical Engineering
Civil
Electrical
Electronics
Electronics and Instrumentation
Materials Science
Mechanical
Production Engineering
Financial
Health
You are here
-
Home
»
Physics
»
Aerospace
»
Propulsion
Chamber Pressure in Rocket Propulsion Formulas
The Chamber Pressure is the amount of pressure generated inside the combustion chamber of a rocket. And is denoted by P
c
. Chamber Pressure is usually measured using the Megapascal for Pressure. Note that the value of Chamber Pressure is always positive.
Rocket Propulsion formulas that make use of Chamber Pressure
f
x
Rocket Exit Pressure
Go
f
x
Exit Velocity given Molar Specific Heat Capacity
Go
f
x
Exit Velocity given Molar Mass
Go
FAQ
What is the Chamber Pressure?
The Chamber Pressure is the amount of pressure generated inside the combustion chamber of a rocket. Chamber Pressure is usually measured using the Megapascal for Pressure. Note that the value of Chamber Pressure is always positive.
Can the Chamber Pressure be negative?
No, the Chamber Pressure, measured in Pressure cannot be negative.
What unit is used to measure Chamber Pressure?
Chamber Pressure is usually measured using the Megapascal[MPa] for Pressure. Pascal[MPa], Kilopascal[MPa], Bar[MPa] are the few other units in which Chamber Pressure can be measured.
Let Others Know
✖
Facebook
Twitter
Reddit
LinkedIn
Email
WhatsApp
Copied!