Difference between revisions of "Rethkir"
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(Created page with "===Rocketry info=== I've added my notes on decompiled rocket engine code on User:RA2lover/Sandbox/Thermodynamics_machinery_notes. I refuse to post on reddit since getting...") |
(Evaporation Coefficients) |
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Is the PFGE max thrust figure obtained from running both inputs with premixed 60.7MPa fuel at 196 K? You can add up to 0.05 mol/L of frozen gases or liquids to a pipe network before it starts taking damage and i wonder if adding ~0.134% of frozen liquid nitrous oxide is enough to get another 100-200N of thrust. [[User:RA2lover|RA2lover]] ([[User talk:RA2lover|talk]]) 03:18, 21 January 2026 (CST) | Is the PFGE max thrust figure obtained from running both inputs with premixed 60.7MPa fuel at 196 K? You can add up to 0.05 mol/L of frozen gases or liquids to a pipe network before it starts taking damage and i wonder if adding ~0.134% of frozen liquid nitrous oxide is enough to get another 100-200N of thrust. [[User:RA2lover|RA2lover]] ([[User talk:RA2lover|talk]]) 03:18, 21 January 2026 (CST) | ||
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| + | ===Evaporation coefficients=== | ||
| + | Saw your reddit post asking for these so i went looking for them. | ||
| + | The game does, in fact, use exponential curves for these and they can be found in the MoleHelper class as EvaporationCoefficientA And EvaporationCoefficientB. | ||
| + | |||
| + | The evaporation pressure for a given temperature and liquid is EvaporationCoefficientA * Temperature^EvaporationCoefficientB | ||
| + | The evaporation temperature for a given pressure and liquid is ( Pressure / EvaporationCoefficientA )^( 1 / EvaporationCoefficientB ) | ||
| + | |||
| + | Here are the coefficients for each liquid: | ||
| + | |||
| + | Liquid A B | ||
| + | Oxygen 2.6854996004e-11 6.49214937325 | ||
| + | Nitrogen 5.5757107833e-7 4.40221368946 | ||
| + | Carbon Dioxide 1.579573e-26 12.195837931 | ||
| + | Volatiles 5.863496734e-15 7.8643601035 | ||
| + | Pollutant 2.079033884 1.31202194555 | ||
| + | Water 3.8782059839e-19 7.90030107708 | ||
| + | Polluted Water 4e-20 8.27025711260823 | ||
| + | Nitrous Oxide 0.065353501531 1.70297431874 | ||
| + | Hydrogen 3.18041E-05 4.4843872973 | ||
| + | |||
| + | Steam uses the same coefficients as water. | ||
| + | [[User:RA2lover|RA2lover]] ([[User talk:RA2lover|talk]]) 14:39, 22 January 2026 (CST) | ||
Revision as of 14:39, 22 January 2026
Rocketry info
I've added my notes on decompiled rocket engine code on User:RA2lover/Sandbox/Thermodynamics_machinery_notes. I refuse to post on reddit since getting disgusted by its API changes and i'm not on discord since getting banned from it, but still occasionally check /r/stationeers. saw your post there and figured maybe some info may be useful.
Is the PFGE max thrust figure obtained from running both inputs with premixed 60.7MPa fuel at 196 K? You can add up to 0.05 mol/L of frozen gases or liquids to a pipe network before it starts taking damage and i wonder if adding ~0.134% of frozen liquid nitrous oxide is enough to get another 100-200N of thrust. RA2lover (talk) 03:18, 21 January 2026 (CST)
Evaporation coefficients
Saw your reddit post asking for these so i went looking for them. The game does, in fact, use exponential curves for these and they can be found in the MoleHelper class as EvaporationCoefficientA And EvaporationCoefficientB.
The evaporation pressure for a given temperature and liquid is EvaporationCoefficientA * Temperature^EvaporationCoefficientB The evaporation temperature for a given pressure and liquid is ( Pressure / EvaporationCoefficientA )^( 1 / EvaporationCoefficientB )
Here are the coefficients for each liquid:
Liquid A B Oxygen 2.6854996004e-11 6.49214937325 Nitrogen 5.5757107833e-7 4.40221368946 Carbon Dioxide 1.579573e-26 12.195837931 Volatiles 5.863496734e-15 7.8643601035 Pollutant 2.079033884 1.31202194555 Water 3.8782059839e-19 7.90030107708 Polluted Water 4e-20 8.27025711260823 Nitrous Oxide 0.065353501531 1.70297431874 Hydrogen 3.18041E-05 4.4843872973
Steam uses the same coefficients as water. RA2lover (talk) 14:39, 22 January 2026 (CST)