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projects:splat [2020/11/17 10:07]
rocketboy [Super Pressure Musings]
projects:splat [2020/11/18 10:24] (current)
rocketboy [Super Pressure Musings]
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 The ascent rate will be more or less linear until the envelope fully inflates (this is because the drag effects due to increasing size of the balloon cancels out that of the reducing air density). Beyond that the ascent rate should continue to reduce as the float altitude is approached. The ascent rate will be more or less linear until the envelope fully inflates (this is because the drag effects due to increasing size of the balloon cancels out that of the reducing air density). Beyond that the ascent rate should continue to reduce as the float altitude is approached.
  
-A spreadsheet SP pressure calculator {{:​projects:​float1e.xls|float1e}} has been written to calculate float altitude and differential pressure to confirm this theory. Previous versions here:​{{:​projects:​float1b.xls|float1b}} ​ {{:​projects:​float1c.xls|float1c}} ​ {{:​projects:​float1d.xls|float1d}} ​+A spreadsheet SP pressure calculator {{:​projects:​float1g.xls|float1g}} has been written to calculate float altitude and differential pressure to confirm this theory. Previous versions here:​{{:​projects:​float1b.xls|float1b}} ​ {{:​projects:​float1c.xls|float1c}} ​ {{:​projects:​float1d.xls|float1d}} {{:​projects:​float1e.xls|float1e}}
  
  
projects/splat.txt · Last modified: 2020/11/18 10:24 by rocketboy