PhysicsMan
Member
I never said it was easy to do, but none of the things you list is a showstopper, while some arguments are just strange. The aerodynamics doesn't have to suffer, the hollow outer layer doesn't need to change the shape, just follow it. Same goes for wings, nothing needs to be qualitatively different, including lift and air resistance. The example of cockpit glass (such plastics are a class of glass) is just an example of a transparent material, nothing more. Do you doubt that a material can be developed that is thinner, more heat, stress, and impact resistant and also transparent? We may not have it now but that's what makes it a problem for the future (near or far). The coverage of air intakes and exhaust with plasma is just nonsense. Hatches and disassembling is also not impossible, the plasma doesn't have to be in a single cavity, it can be in separate blocks.Let’s start a list of the problems:So, NO the plane won’t work, and probably not the plasma either.
- The outer hull has to standoff from the inner hull, and is therefore the de facto airframe,you’re your aerodynamics have gone to hell. Wing thickness is increased 2x the standoff distance and you have lost most of your lift and massively increased frontal resistance, if you can get off the ground at all.
- No coverage over air intakes and exhaust. One appeal of ‘plasma stealth’ is that it is supposed to cover these areas.
- Requires large hatches operable in flight for weapons bays, gun, cockpit, and refueling. The entire outer hull will have to be easily and quickly to remove and reattach for normal maintenance.
- The cockpit canopy is a laminated plastic composite, not glass. Materials limitation:
- Low impact resistance. Bird strikes happen, they just are not usually a problem unless it is the engine intake of cockpit canopy. Now it is the whole aircraft.
- Material is a plastic, which means it is subject to permanent distortion from normal continuous loads (very low yield strength). Low tensile strength (relative to normal materials) requires small sections or large thicknesses.
- Temperature limit bars use on leading edges, engine intakes, and engine exhaust.
- Supporting structure for the outer hull as a source of discontinuities in plasma coverage and independent source of reflections.
- Very high loading on all panels (14.7 psia / 1 bar at sea level) plus aerodynamic loads. Thickness will be MUCH greater than for cockpit canopy. In flat surfaces material will be under tension instead of compression.
- There is much more, but I am too tired to keep list them.
Again, nothing listed here is impossible, so to say it can't be done is just shortsighted.