LANTR

Whilst we await Firestar's nuclear afterburner, Borowski et al. a decade ago had proposed a chemical one. The subtext, best I gather, was that old solid-core NERVA for all its 900s I_sp wasn't all that great for thrust. Most Mars missions assume NERVAlike NΘP. Or big punches to orbital trajectories, like The Martian to Hohmann.

Borowski's crew was pondering a high-thrust solution as may ignore much I_sp and Earth won't care what is burnt near us. This has a use-case in delta-V punches: a mission to the Lunar poles. I'll bite; even that spaceline only got to equatorial Sinus Medii.

The promise is to achieve liquid-core-temp exhaust whilst still keeping the (fissile) heat-source, solid. That'd be a safer reactor in HEO, might even allow lower-grade fuel. In 2024 the plasma-core was still SDI scy-fy (and in 2026; also none of us knew or know what Howe is doing).

NERVA, it happens, assumes hydrogen for propellant. As the Hindenburg passengers can tell you, it reacts with oxygen. (This blog takes no sides on the cause of that one's initial blowup.) The paper suggests to bring along liquid oxygen - LOX - with that superheated hydrogen. The LOX is introduced after the burn which raises the exhaust velocity. This is thereby an "LANTR". Oxygen is cheap on our moon, maybe the only cheap volatile.

As to why to do this: that is because the N part of NΘP is a nuclear reaction, and not - like Orion - a bomb. As a reaction, it is supposed to run for longer. NERVA hasn't been tested for many hours in, what amounts, a thermos the size of the Universe. Earth might not want a reaction running long in our shared well.

For short bursts of heat one might even swap those nucular roggets for enthalpy. Which segues...