My estimated friends MATRIXONE and TORSTEN:
I see in your diorama an 262 whit the nose put in the floor...tha´ts remind me the testimony of Goering,an history before his prosecutors of the U.S.A.A.F.:
He said that the speed-approach of landing of 262, it was so high, and for that reason they lost many pilots and airplanes; the brakes simply cant work. they need a long tracks.it was very dificult to land.
My instructor of visual flight rules in two engines, he was an Fight Pilot of the F.A.M. (Mexican Air force)he flew moore than 1200 flight hours in a T-33 plane, (the grand child of the P-80, today retired of service) and he said something alike to your comment (he study that topic,because the 262 was an contemporary of the P-80) :
" I have read somewhere that some of the problems with the Jumo 004 were fixed by a better fuel regulator and also by using fan blades that were hollow and were attached differently."
Thats right, and he comments something moore: the 262 have a "flame-out" (failure in its engines) for turn in a marcade degree (moore than 60o for the TRIM, cause the engine had no auxiliary and mechanics intakes, and thats the real reason that the plane needs escort for take- off and landing,it had a low drive (maniubrability? sorry my poor english).
Just for acommplish, let me show you an TRIM intrument, for you can imagine the situation of turn in high degrees:
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In the picture,you can see an light turn of the airplane (around ten degrees), in a 262 ,if the turn was superior to the 60s degrees, in a continuos time, the pilot had the risk to flame out the reactor.
I read that Nowotny had that trouble: flame out of his right reactor, and for the loss of his airspeed,he down to crash, to few minutes after he take off, cause a discussion whit his superiors (nowotny has forbbidden to fly).
Very Interesting theme ,of the very beatiful plane .and very beutiful model and diorama.
CHEERS!! (SALUDOS!!)(HATTS!!)