Propellants Tab: Difference between revisions
Jump to navigation
Jump to search
No edit summary |
No edit summary |
||
| Line 4: | Line 4: | ||
File:BurnSimPropellantsTab.png|700px|alt=BurnSim Main Window | File:BurnSimPropellantsTab.png|700px|alt=BurnSim Main Window | ||
default [[Main Page|Go to main page]] | default [[Main Page|Go to main page]] | ||
rect 1050 161 1481 193 [[Propellant Name|]] | rect 1050 161 1481 193 [[Propellant Name|Name of the propellant]] | ||
rect 1061 209 1215 236 [[Propellant Standard Properties|]] | rect 1061 209 1215 236 [[Propellant Standard Properties|Common propellant properties, including characterization numbers]] | ||
rect 1226 209 1428 233 [[Propellant Pressure Varied Properties|]] | rect 1226 209 1428 233 [[Propellant Pressure Varied Properties|Here you can specify propellant properties based on chamber pressure. For some propellants, properties change with chamber pressure]] | ||
rect 1440 213 1490 235 [[Notes|]] | rect 1440 213 1490 235 [[Notes|Propellant Notes]] | ||
rect 1060 244 1358 278 [[C Star|]] | rect 1060 244 1358 278 [[C Star|C* or Characteristic Exhaust Velocity. This can be calculated in ProPep]] | ||
rect 1062 279 1355 310 [[Characteristic ISP|]] | rect 1062 279 1355 310 [[Characteristic ISP|Characteristic ISP is simply another representation of C*, above]] | ||
rect 1065 312 1281 344 [[Burn Rate Coefficient|]] | rect 1065 312 1281 344 [[Burn Rate Coefficient|Burn Rate Coefficient (A)]] | ||
rect 1069 353 1278 389 [[Burn Rate Exponent|]] | rect 1069 353 1278 389 [[Burn Rate Exponent|Burn Rate Coefficient (N)]] | ||
rect 1069 388 1360 412 [[Propellant Density|]] | rect 1069 388 1360 412 [[Propellant Density|Propellant Density, measured or theoretical from ProPep]] | ||
rect 1364 247 1574 276 [[Specific Heat Ratio|]] | rect 1364 247 1574 276 [[Specific Heat Ratio|Specific Heat Ratio is currently not required, will be used for Startup Transient Simulation in the future]] | ||
rect 1364 278 1577 310 [[Molar Mass|]] | rect 1364 278 1577 310 [[Molar Mass|Molar Mass is currently not required, will be used for Startup Transient Simulation in the future]] | ||
rect 1196 486 1269 528 [[New Propellant|]] | rect 1196 486 1269 528 [[New Propellant|Click this button to add a new propellant]] | ||
rect 1279 488 1354 526 [[Edit Propellant|]] | rect 1279 488 1354 526 [[Edit Propellant|Click this button to edit selected propellant]] | ||
rect 1358 490 1444 522 [[Delete Propellant|]] | rect 1358 490 1444 522 [[Delete Propellant|Click this button to delete the selected propellant]] | ||
rect 2 46 54 76 [[FileMenu|File Menu]] | rect 2 46 54 76 [[FileMenu|File Menu]] | ||
rect 57 47 118 75 [[ActionMenu|Action Menu]] | rect 57 47 118 75 [[ActionMenu|Action Menu]] | ||
Revision as of 16:38, 16 November 2022
Hover over or click on various fields in the image below to get more details on each field.
