Back in 2023 I noted a fission-fragment rocket engine - in passing, frankly. I had left to the linked article what this was, mainly because I (1) didn't know much and (2) didn't care to look it up. It had a few unsolved problems which made it not worth my while. Ryan Weed founded something called "Positron Dynamics" for this...
... and then fled the place, shifting to fusion propulsion at AeroFuse. Weed gave up on this too and is now fronting something called Eos Atomics. This is for fusion sparking, compact plasma heating
. So the whole aerogel/fission scheme looks dead. Let's autopsy the corpse.
ToughSF links today that Weed was addressing some of these problems in that banner year 2024, in collab with Sandeep Puri et al.
Classical "atomic rockets" are nuclear-thermal, including NERVA. Heat a gas, offer a hole for escape, vroom at very-many m/s. That last is specific-impulse; Isp opens up new delta-V routes. Among its (many) constraints, is the ability to force the temperatures into vrooming the gas and to control its plasma. The ideal plasma here was the proton, aka hydrogen. Other solutions exist out there to afterburn the hydrogen, like with some oxidiser or even to fuse it; we're not getting into that today.
Weed proposed to harness the energy of the fission-chain's fragments, bypassing other propellants. Much of the energy in fission actually doesn't go directly to heat; it goes to moving the fragments, like neutrons or (for uranium) iodine-135. Elsewhere alpha-decay should count as Nature's most common process. I think most fission-thermal solutions let the fragments bounce around to turn their bouncing into heat. Chernobyl enjoyers will recall, for 2-2.6% U-235 LEU, the fragment I-135. This becomes Xe-135 leading to Xenon Poisoning, gobbling neutrons meant for the reaction. As a heat-generator it's all very indirect so inefficient, and some capitalist reactionaries might consider it somewhat dangerous as well.
Aerogel comes in as a matrix to hold the fissile elements in a fine dust at some mutual distance. The notion is that the aerogel would not interfere with the runaway radioactive iodine (or whatever). These frags are ions, iodine in particular being quite reactive, so Weed added a honkin' magnet to run the ions toward the exit. That redirected iodine might not be the fraction of lightspeed that the sail's helium was, but it is still one hefty Isp. As for the exhaust: this can decay into Xenon or whatever, far from the reactor. Thrust ain't great so it's for robots, as I noted at the time. This is similar to the T-FINER sail proposal.
Puri's crew chose fissile Americium, here -241 rather than -242m, I guess because this isotope could be handled in reasonable times in a lab. Opposite from NΘP they wanted to reduce attenuation
into that Θ. For them a graphene matrix worked best: at 900 microns (μm) they wasted only 7.5%.
Aaaand that is where Weed left us. Radioactive critical-mass aerogel is expensive to manufacture, and difficult to justify launching into LEO. In the low-mass high-delta-V mission space generally, by 2024 several competitors were coming to press (if not to prod).