New post from armchair rocket engineer department.
A bit of generic engine theory as I understand it, please correct me whereever I am wrong.
What is the problem with more efficient rocket engines? At the first (very naive) glance "more efficient" rocket engines are those with higher Isp. But in practice there is a problem. In order to increase Isp by x2 you need to increase _kinetic_ energy_ of exhaust by x4, because p=mv, but E=(mv^2)/2. Why is this a problem? Required power levels grow quadratically and with very high Isp's are becoming truely astronomical.
What is the problem with _that_, one might ask? Aren't we getting much better fuel efficiency instead? The problem: with those power levels you *have to* be very efficient (I mean, like 99,99...%) in converting energy to thrust, or more precisely, in NOT converting it to heat. That's exactly why the rocket with "best possible" Isp, the photonic rocket, is unlikely to ever work. It needs godawful amounts of power, and if you accidentally convert 0.000..001% of it to heat, the rocket will instantly vaporize.
Thus any high-Isp + high- or moderate-thrust engine inevitably has to employ some advanced means of using more power for thrust and less power for waste heat.
Back to topic of "Nuclear thermal rocket + nuclear pumped laser".
I was thinking about improving nuclear thermal engines. They said to have Isp of ~900 (with solid core reactor, the only one tested so far). How to improve that? What about making core reactor to also generate laser beam ("nuclear pumped laser"), and use that for additional heating of exhaust?
["nuclear pumped laser" picture:
http://www.ippe.obninsk.ru/podr/tpl/device/lael_a.html ]
ASCII picture of the engine (copy-paste into e.g. Notepad and use fixed font to see it clearly):
--------------\------/....
-||||||||||||..\----/.....
-|||||||||||||..----...***
-||||||||||||||......*****
-##########=====**********
-##########=====**********
-||||||||||||||......*****
-|||||||||||||..----...***
-||||||||||||../----\.....
--------------/------\....
---, /, \ - chamber, nozzle walls
### - nuclear reactor core - heats gas and also generates laser beam
=== - laser beam
... - chemically different gas is injected into the chamber, one which is effectively absorbing laser's wavelength ("opaque gas")
*** - laser beam passes thru the engine throat, meets opaque gas and heats it up.
||| - the rest of the reactor chamber is filled with gas which is used as lasing medium.
proportion of ||| and ... are not to scale - to be determined by "real" engineers if they ever consider building the thing.
What's the idea? The idea is to take a "usual" nuclear thermal design, increase reactor power, convert some % of power to laser beam, and convert beam's energy to more heat in a place where we don't risk melting down the reactor - in the throat. Note that a optically thick layer of "opaque gas" is protecting throat's walls from extreme overheat.
Is it viable at all? In particular, which gases can be used for that?