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#1 |
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Join Date: May 2009
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According to the rules in Spaceships the delta-V for a chemical rocket is 0.15 mps per tank. From what I can figure, it would be impossible for a chemical rocket to achieve a delta-V high enough to make low Earth orbit even if it were multi-stage.
By my calculations, any size rocket with 1 space for engines, 1 space for armor (because of streamlining) and 18 spaces of rocket fuel could only manage a delta-V of 2.7 mps. Am I doing something wrong? Or, is this an error in the book? The Midnight Sun's rocket engines seem to have a delta-V of 0.24 mps if you do the math with the stats they give with that example. |
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#2 | |
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Join Date: Jul 2008
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Quote:
For one, you're missing the extremely important rule on page 17 about delta-V for ships with high fuel fractions. Factoring that in your all-out booster gets a delta-V of 6.75 mps. For another, your calculation in no way would bar multi-stage rockets from getting to orbit. A multistage rocket can have an arbitrarily high delta-V, by achieving an arbitrarily high ratio of reaction mass to payload mass. |
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#3 |
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Join Date: Feb 2005
Location: Berkeley, CA
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Spaceships is highly simplified; as such, you can't really expect it to be able to replicate systems that operate at the ragged edge of the performance envelope.
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#4 | |
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Join Date: Aug 2004
Location: In the UFO
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Quote:
As the previous poster indicated, the relevant rules are found in the fuel tank section, which incorporate a rounded-off version of the rocket equation.
__________________
Is love like the bittersweet taste of marmalade on burnt toast? |
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#5 | ||
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Join Date: May 2009
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Quote:
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#6 | |
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Banned
Join Date: Oct 2007
Location: Europe
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Quote:
Could you please consider including a more detailed rocket equation table in that supplement, e.g. so that the multiplier for 11 fuel tanks is different from the one for 12 fuel tanks? |
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#7 | |
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Join Date: Oct 2004
Location: Yorkshire, UK
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Spaceships 2, p17 has the Baikonur Launch Vehicle which is a TL7, Chemical Rocket, three-stage spacecraft capable of reaching low-orbit |
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#8 | |
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Join Date: Jul 2008
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Quote:
1: 1 2: 1.027 3: 1.056 4: 1.088 5: 1.122 6: 1.159 7: 1.200 8: 1.245 9: 1.295 10: 1.351 11: 1.415 12: 1.489 13: 1.574 14: 1.677 15: 1.802 16: 1.961 17: 2.176 18: 2.494 19: 3.073 (Table based on: log(20/(20-x))/log(20/19) * 1/x) |
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#9 |
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Join Date: May 2009
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Rocket sciencist use Isp to compare rocket engine and fuels performing. Isp stand for pounds of thrust per pounds of fuel burn per second. Most liquid fuel use LOX get than Isp in the 200 to 400 range.
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#10 | |
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Join Date: Aug 2007
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Quote:
__________________
Fred Brackin |
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