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That link doesn't have enough information
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Yes, perhaps the specific example I picked wasn't ideal.
That being said, many thanks for the worked example! I think I'll be able to continue from here.
Edit: A few questions here for
the-red-scare.
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Example: I want my fusion rocket to get 0.005 G from an engine massing 1/20 of loaded mass. I multiply 0.1 by 4/0.05 to get 0.4. The THS thrust is therefore 0.4 tons.
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What is the 0.1 in the calculation, how does the 0.005 factor in there, and how do you get 0.4 from 0.1*4/0.05? I assume I have misunderstood the formula there.
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Thrust is based on the thrust-to-weight ratio of the drive. Atomic Rockets generally provides this. You just multiple the T/W by 4 and you’re done.
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Do I understand it correctly that by multiplying the TWR by 4 (presumably the mass per space of drive?) I'll get the THS' thrust per space of drive figure?
Thank you in advance!