Hello
As for the Mig, you are correct, different circumstances, an intial production run of 100 planes was started before the completion of state trials where the the prototype was unanimously censured for
handling characteristics, manoeuverability and stability. Minor modifications to the aircraft on the assembly line slowed production to 20 delieveries by the end of 1940 compared to the planned over 60. Further production after the first 100 was held up while the redesign was completed. Granted this was done very quickly and the first MiG-3 came off the line in Februry of 1941. Should the first 100 aircraft even have been made?
No, not exactly. The first production batch was composed from 50 MiG-1, the secund from 50 MiG-3, and then 50 more MiG-1. All following planes were MiG-3. It means that both planes were produced in parallel assembly lines. The main difference between a MiG-1 and MiG-3 is an extra 250 litres tank behind the pilot's seat. Due to extra 200-250 kg and the aft CG, handling characteristics, manoeuvrability and stability of the MiG-3 were much worse than MiG-1 one's. The only reason for transformation was the 1000 km range NKAP request issued in the meantime instead of the previous 600 km at 0.9 V max speed. Exactly as for the LaGG-1/LaGG-3 and Yakovlev I-26/I-28 family. But it's just a detail.
Really? Mig-1s could fly at 626kph at 7000m is max continous speed? or was max continous more like 550kph for the MIG 1?
Look, we spoke about that question several times
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http://www.ww2aircraft.net/forum/aviation/p-40-vs-yak-1-vs-hurricane-17485-4.html#post532071
http://www.ww2aircraft.net/forum/aviation/p-40-vs-yak-1-vs-hurricane-17485-4.html#post533425
Soviet
rules and procedures are were very simple: the nominal engine power is the max continuous power (means with no time limits). In the opposite case it was indicated "forsage".
Moreover measurements of the max speed ware to be validated only at conditions of
-constant speed
-constant height
-constant power
-
constant engine heat (no oil, water, cylinder head temperature increase)
Really? Mig-1s could fly at 626kph at 7000m is max continous speed? or was max continous more like 550kph for the MIG 1?
Really, the range from soviet
us and coutumes for fighters was given at 0.9 Vmax (0.9 x 626-657 = 560-580 km/h for the MiG-1) for soviet planes and at 0.8 V max for bombers.
So i don't understand where is it taken from that 0.8 V max of the Tu-2 (and Pe-2, Yer 2, Il-4...) should be the max cruse speed?
Well, this does get back to which set of plans, when?
B-26 was ordered off the drawing board just like several soviet planes.
If U.S. is given the planes for the ANT-58 in Dec of 1940 how long is it going to take them to turn it into the TU-2?
-Why are you so obsessed by plans? From driving boards to the real plane it's far from being a simple formality but a real challenge. Both P-51 and ANT-58 encountered success, but it is not a general law.
Then prototypes should be satisfactory enough to be commanded
and serial builded. Both of them won that secund challenge.
-Why do you absolutly want to transmit plans and to change the ANT-58 to the 59? The lower firing point? It coasts the bomb load reduction. ANT-58 was intended to carry 3000 kg of bombs inside the fuselage, latter reduced to 2500.
"Design was revised and became more technological, number of joints was decreased and whole assembly procedure was revised. Cuts were made even on total length of electric wiring."
All that could have been modified progressivly on the assembly lines, exactly as for the other planes of the world.
Of course this is in addition to redoing the engine installation. Granted the Russians had a few detours but first radial engined prototype doesn't fly until Dec 1941?
THe M-82 first under goes state tests in the spring of 1940. A batch pf protoypes are built May 13,1941 NKAP issues a decree initiating series production even theough M-82 doesn't complete second second series of state tests until May 22 1941. Power rating is 1700HP.
And why americans and britishs should have been waiting for
soviet radial engines? The deal was just to go to Moscow (Ramenskoyé in fact). Study and test the ANT-58. Built or not a joint venture if being interested with the plane. I'd rather see american or english help on mounting a factory in USSR, in exchange of a part of produced airframes.
Nice to note that you are a time traveler or that you are such an expert that you could identify which aircraft are winners and which ones are losers before they even fly.Another thing to consider is that while many of these aircraft couldn't do what a TU-2 does the TU-2 might have trouble doing the jobs that many of those aircraft did.
Nobody knows, even it the Pe-2 or a Tu-2 could have been praised by allied pilots. For instance soviet comission made a lot of trials with the Martin B-26, disliked it, every time making a rough opposition to american proposals to include it to LL deliveries.
Also refences that suggest the max sized bomb as 1000kg witch would cast doubt about dive bombing attacks with a 1500kg bomb.
The FAB 1500 bomb was simply not a serial one, only small experimental parts were delivered, from Ozerov memories even mock-ups of FBB 2500 kg bombs were dropped from the plane. (Toupolevskaya sharaga)
What was the capability of the 1940-41 design vrs Western Designs?
Early B-25s were rated for 5200lbs of bombs, later versions swapped guns for bomb load.
On paper, all kind of planes are looking good. In order to estimate performance evolution of the Tu-2 with american engines, look at La-5FN TsaGI calculations.
Regards