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#1 | |||
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Join Date: Nov 2017
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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. Quote:
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Thank you in advance! Last edited by mindbound; 10-23-2022 at 04:25 PM. Reason: Additional questions, uncertainties |
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#2 | |
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Join Date: Sep 2014
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Yep, T/W is unitless, so multiplying by any weight gives you the thrust for an engine of that weight. All THS drives are 4 tons per space, so multiplying 4 by the T/W is the tons of thrust. |
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#3 |
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Join Date: Sep 2014
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Here’s an example from Atomic Rockets. All I’m using is the info from the Engine List.
ACMF (Antimatter-Catalyzed Micro-Fission/Fusion) Thrust: 2.7 Mass: 4 Cost: 0.8 Output: 0 Power: 0 RMC: 0.005N ISP: 13,500 Thrust is 4 * 0.680 F is 24,030 Ve is 132,300 Flow rate is 0.0154 kg/s Or 0.061 tons/hour RMC is 0.061/12 All pulse drives use generic “nuclear pellets” which are 12 tons per space and we don’t really have anything better to base density on. But as you can see, pretty easy! |
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#4 | |
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Join Date: Nov 2017
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| Tags |
| conversion, rockets, spacecraft design, transhuman space |
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