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Nuclear Propulsion in Space

Nuclear Propulsion in Space

US National Archives
2 HN recommenders · discussed 2018–2020
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About this video

A 1968 NASA film from the US National Archives explaining why the US needed a nuclear rocket and how the engine works. It also shows combined nuclear and chemical stages for a manned Mars mission.

Why it appears in the archive

HN people link it as an old-timey explainer for nuclear thermal propulsion, and as evidence these engines were already built and tested.

AI-generated summary and labels from the source dataset; verify important details against the video. Source & credits.

From the Hacker News discussion

wizardforhire · 2018-06 · rec

aerospikes There’s a lot of reason why they haven’t been used yet, but I think most the compelling argument against them is that they won’t be used until fuel costs become the competitive factor in launch prices. [LINK] [LINK] Nuclear rockets are quite the concept but have their obvious limitations. This video is worth checking out if you haven’t seen it yet. [VIDEO]

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cwojno · 2020-10 · rec

This article didn't explain it at all, so you're right to ask. tl;dr: Gaseous propellant (I'm guessing hydrogen) is heated with fission then pointed in the opposite direction of intended travel. The uranium in this design is not a propellant, but a heat source. Aside: you can use photons/heat as a propellant, but it's thrust is very low [LINK] . Ideal propellants typically have a high exit velocity and low mass. That gives you the longest amount of "burn" time, and the greatest amount of control for the weight. [LINK] Back in the day when the US was building more of these nuclear rockets, the propellant of choice was typically hydrogen [LINK] . Old timey video explaining it [VIDEO] . I'm assuming this proposed design would also use hydrogen, but I couldn't find any sources on the propellant for their design. Liquid hydrogen served to keep the reactor cool as it transitioned from liquid to gas as that phase change absorbs energy. The gas is the directed through the reactor core where the gas heats up. As gases heat up, they absorb energy, their average particle velocities increase. Eventually, the hydrogen molecules (mostly H2 or H-H gaseous hydrogen), makes it to the nozzle and is ejected. The high-velocity hydrogen is what actually provides the bulk of the thrust to the spacecraft. Compare this to Project Orion ( [LINK] ) which intended to detonate nuclear warheads and the craft essentially rode the shock wave into the stars. I would classify this method of propulsion, not s

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inamberclad · 2019-09 · reference

It's much more likely to look like NERVA than Orion. [LINK] These types of engines have already been run: [VIDEO]

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stqism · 2020-06 · reference

I don’t know if any real rockets were built, but according to this old video we’d see a reduction of weight due to the absence of heavy chemical fuel. [VIDEO]

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