Recent content by Basimalasi

  1. Basimalasi

    I Energy needed for achieving this mass flow rate for a rocket

    I will make a plasma container like those used in nuclear reactors and I will launch that rocket, You'll see ;) Thanks for you help!
  2. Basimalasi

    I Energy needed for achieving this mass flow rate for a rocket

    Awesome. I'm going to include this in my graduation project. can you help me find a specific equation that could solve for the required energy input for creating that plasma
  3. Basimalasi

    I Energy needed for achieving this mass flow rate for a rocket

    if we hypothetically had a material that would withstand the high pressure/temperature .would it work?
  4. Basimalasi

    I Energy needed for achieving this mass flow rate for a rocket

    What I mean is can we treat the steam rocket as a thermal battery. we store a huge amount of energy through heating and then launch. The power plant charges the rocket once not constantly. for example if a rocket a mass flow rate of 2,430 kg/sec would require 1000 Gjoules of input energy then we...
  5. Basimalasi

    I Energy needed for achieving this mass flow rate for a rocket

    But even if the power differs those two systems have completely different reactions. one is combustion and the other is straight expansion because of ;pressure deference,Maybe the combustion has less efficiency ? :/ Also I'm kind mixed up with what exactly I am looking for. Why do we care about...
  6. Basimalasi

    I Energy needed for achieving this mass flow rate for a rocket

    I just want to see how much power should I provide to a steam rocket as heat to make it have a same thrust and mass flow rate of NASA's Delta 2 rocket
  7. Basimalasi

    I Energy needed for achieving this mass flow rate for a rocket

    it will be heated with a 400 MW power plant then a high insulation layer will contain it
  8. Basimalasi

    I Energy needed for achieving this mass flow rate for a rocket

    imagine we had a meta-material that can withstand such temp.
  9. Basimalasi

    I Energy needed for achieving this mass flow rate for a rocket

    It's hard to determine the flow of an unsteady two-phase fluid
  10. Basimalasi

    I Energy needed for achieving this mass flow rate for a rocket

    it has the exact area of this rocket engine. But I don't know how to calculate the exit area of the nozzle Rocketdyne RS-27A Propellants: LOX/RP-1 Kerosene O/F Ratio: 2.245 Dry Weight: 2,528 lbs T/W Ratio (sl): 79.11 T/W Ratio (vac): 93.75 Length: 149 inches Diameter: 67 inches Expansion Area...
  11. Basimalasi

    I Energy needed for achieving this mass flow rate for a rocket

    Hey, Suppose you have an enclosed vessel that is full of water. You heat it up then you open a valve, and that will create enough thrust for it to act as a rocket. How much energy is needed for a steam rocket to get heated enough to achieve a mass flow rate of 2430 Kg/s. Mass of water= 256...
  12. Basimalasi

    What is the characteristics of the flow in Hot-water rockets

    https://en.m.wikipedia.org/wiki/Steam_rocket
  13. Basimalasi

    What is the characteristics of the flow in Hot-water rockets

    So I'm trying to make a Hot-Water Rocket. But I want to make the necessary thermodynamics calculations first. What kind of flow will it be in such systems I think it's obviously going to be an unsteady flow but is it uniform or not? I also would love if you guys linked me to unsteady...
  14. Basimalasi

    Calculation of the exhaust velocity of a Hot Water Rocket

    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...
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