nobodyagain
nobodyagain
21 / 0
8th September
13th September
My first ever SRB, created to test the limits of tpt combustables. It has a burntime of approx 18 seconds, and maintains a nearly flat thrust curve.
rocket solid redc

Comments

  • wisco11
    wisco11
    12th September
    i feel like this in ksp
  • KyleTheCreator
    KyleTheCreator
    12th September
    id:3423934 prototypo
  • KyleTheCreator
    KyleTheCreator
    12th September
    nobodyagain: dawg your math shi is broken Nuhuf it correct
  • KyleTheCreator
    KyleTheCreator
    12th September
    nobodyagain: Yo you do know watr doesnt boil at 0 pres and your saying 1 pres is 1 bar but 0 bar is. vacuum... and water.. boils.. in vacuum..
  • nobodyagain
    nobodyagain
    11th September
    meow_Chron1c, do show it, I will be trying to improve the burntime with the next iteration of this, so any examples to work off of is very greatly appreciated.
  • meow_Chron1c
    meow_Chron1c
    11th September
    i have an srb that's similar but it has about 20 less pressure, burns 1.5x as long, and burns with plasma instead of fire
  • nobodyagain
    nobodyagain
    11th September
    But either way it doesn't matter all too much, can't calculate isp accurately because its impossible to determine the speed of particles in any real units, or even the scale of anything.
  • nobodyagain
    nobodyagain
    11th September
    It may very well be that the rest of tpt goes by 1bar = 1 pressure, and if so, that'd mean the srb actually achives a nozzle pressure of 80psi, and a maximum internal pressure of 1150 psi.
  • nobodyagain
    nobodyagain
    11th September
    To get 60 psi in BAR, you actually need 4.13 bar, so, either tpt is physically unable to simulate pressures higher than 29psi, or the rfrg bar eqivelence is wrong, outdated, or not considered on the same scale as to the other elements.
  • nobodyagain
    nobodyagain
    11th September
    Also also