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/sci/ - Science & Math

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>> No.14565756 [View]
File: 606 KB, 772x597, NTR_ship.png [View same] [iqdb] [saucenao] [google]
14565756

>>14565749

>> No.12249974 [View]
File: 606 KB, 772x597, wLc2MqJFkY.png [View same] [iqdb] [saucenao] [google]
12249974

>>12249931
Using it for a reusable transorbital shuttle would've been awesome and enabled the delivery of large large (40-ton+) payloads to the lunar surface with one saturn V launch's worth of propellant.

>>12249953
The version that would have flown in space would have had around double the specific impulse of an RS-25. The ISP is higher because you have only hydrogen in your exhaust instead of heavier products like water from hydrolox.

Also NERVA is a closed-cycle reactor where the reaction mass isn't being shot THROUGH a reactor - just heated by it. The real limit on its ISP is how hot you can get the reactor without melting it, not unlike the problem with controlled fusion reactors.

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