Calculation of the exhaust velocity of a Hot Water Rocket

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SUMMARY

The discussion centers on the feasibility of using a Hot Water Rocket or Steam rocket to reach outer space. It concludes that calculating the exhaust velocity involves determining the change in enthalpy, but the specific state of water during the process remains uncertain. The conversation highlights that a rocket engine based on heating water is unlikely to succeed in achieving space travel. Additionally, it references the importance of understanding thermodynamics tables for accurate calculations.

PREREQUISITES
  • Thermodynamics principles, specifically enthalpy calculations
  • Understanding of rocket propulsion systems
  • Knowledge of DeLaval nozzle design and function
  • Familiarity with liquid propellant rocket engines, including Liquid Hydrogen/Liquid Oxygen systems
NEXT STEPS
  • Research the thermodynamic properties of water and how to use thermodynamics tables
  • Learn about the performance characteristics of Liquid Hydrogen/Liquid Oxygen rocket engines
  • Study the design and operation of Hydrogen Peroxide catalytic rocket engines
  • Explore the flow dynamics in convergent-divergent nozzles, particularly DeLaval nozzles
USEFUL FOR

Aerospace engineers, rocket propulsion researchers, and students interested in thermodynamics and rocket design will benefit from this discussion.

Basimalasi
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inb4 "google it", I did. There aren't a lot of information about this topic.

Can a Hot Water Rocket or a Steam rocket ever succeed to reach outer space?
I can calculate the exhaust velocity by determining the change in enthalpy I guess but I don't in which state will it exist in and how can I get the values from the thermodynamics table, so imagine we have a 5MW heater then we heated a tank full of water, how much is the mass and energy needed to fly is and which state will the water have?
 
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Basic answer is that a rocket engine based on heating a tank of water is unlikely to be successful .

You might find a lot of explanation and background interest in these topics though :

(1) Liquid Hydrogen/Liquid oxygen rocket engines .

(2) Hydrogen Peroxide catalytic rocket engines .

(3) Flow in a convergent -divergent nozzle - usually called a DeLaval nozzle .
 

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