Weird nuclear propulsion concept

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Discussion Overview

The discussion revolves around the concept of nuclear propulsion, specifically focusing on the rationale behind its use in rocket technology, the safety concerns associated with retrofitting nuclear reactors for this purpose, and the exploration of alternative nuclear propulsion methods. The scope includes theoretical considerations, technical explanations, and conceptual clarifications regarding propulsion efficiency and safety.

Discussion Character

  • Exploratory
  • Technical explanation
  • Debate/contested

Main Points Raised

  • One participant questions the choice of nuclear propulsion, suggesting it may be dangerous to retrofit a nuclear reactor onto rockets and wonders why other options are not being pursued.
  • Another participant explains that Nuclear Thermal Rockets (NRTs) are favored for their efficiency, citing a Specific Impulse (Isp) of 850-1000 for NRTs compared to 348 for SpaceX's Merlin engines, which could enable faster missions to destinations like Mars.
  • Concerns are raised about the potential dangers of nuclear fuel not reaching orbit, which could lead to widespread distribution of radioisotopes in the event of a disaster.
  • Some participants mention that there are other methods of utilizing nuclear energy for propulsion, indicating that the discussion is not limited to NRTs alone.
  • A participant references a Wikipedia article that discusses various nuclear propulsion methods, highlighting the historical context of using nuclear material for propulsion since the early 20th century.

Areas of Agreement / Disagreement

Participants express differing views on the safety and practicality of nuclear propulsion, with some advocating for its efficiency while others question the risks involved. The discussion remains unresolved regarding the best approach to nuclear propulsion and the exploration of alternative methods.

Contextual Notes

The discussion includes assumptions about the safety of nuclear propulsion and the efficiency metrics of various propulsion methods, which may depend on specific definitions and contexts that are not fully explored.

hagopbul
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TL;DR
A question about nuclear propulsion and it's choices
Hello all:

I have a small question about nuclear propulsion , why everyone are trying to use it ,and why this wired choice of nuclear option , retrofitting a nuclear reactor to mount it on the rocket , isn't that a little dangerous , why they don't use other option or research it , there is few obvious ones
 
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I presume you're talking about concepts for a Nuclear Thermal Rocket, because I've seen a few articles on them recently.

Why nuclear? It's a question of efficiency, really. NRTs can generally get more thrust out of a given mass of propellant. This is measured as Specific Impulse, per the NRT article they expect 850-1000 Isp for an NRT. For comparison, the Merlin rocket engines SpaceX uses on the Falcon 9 get about 348 Isp (Merlin 1D Vacuum). This let's you go places (like Mars) faster. [Further, NRTs get this Isp and have high thrust, unlike Ion Thrusters which have Isp values in the thousands, but produce very little thrust.]

As far as dangers go, I think the one that gets the most attention is the danger that the nuclear fuel doesn't make it to orbit due to one disaster or another and radioisotopes are distributed over a large swath of the planet.

Why not use another option? Those result in longer missions to deep space, and the less time spent exposing your astronauts to cosmic radiation the better.
 
Last edited:
I was talking about other options for nuclear propulsion ,there is other ways for using nuclear energy in propulsion
 
hagopbul said:
I was talking about other options for nuclear propulsion ,there is other ways for using nuclear energy in propulsion
What research have you done so far? This article mentions several ways.
https://en.wikipedia.org/wiki/Nuclear_propulsion
Nuclear propulsion includes a wide variety of propulsion methods that fulfill the promise of the Atomic Age by using some form of nuclear reaction as their primary power source. The idea of using nuclear material for propulsion dates back to the beginning of the 20th century. I
 

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