Hello Shortround6 ,
Correct, I was thinking of the Mig 1. The Mig 3 cruised faster than the P-40E too. although it would be interesting to find some figures for each plane for cruising speed used, at what altitude for what range using what for a fuel load.
Might be useful:
Â.Á. Øàâðîâ. Òîì 2 - òàáëèöû 20
Some older books say the Mig 3 had a 245 liter 'overload' fuel tank and while many fighters used such tanks later in the war with restrictions on combat use if fuel was in the tank I don't believe I have seen anthing on this concerning the Mig 3. It may not apply. Interesting to find out if range figures for P-40 include drop tank or not.
For the I-200 state trials: 580 km at 565 km/h (09 Vmax speed), and from memory 784km at 465 km/h
The I-200/MiG-1 had one fuselage 110l and two 155l wing root tanks.
The P-40E had 35+50+62.5 us.gal tanks. (461l)
The MiG-3 carried an extra 265l ( with less than realy 250 usable litres, due to mis-shapen geometry) tank under the pilots seat and a second oil tank beneath the engine. In order to compensate the aft CG, the engine was moved 100 mm forward, lengthening the plane as same. Total fuel capacity 680litres (usable 640-650)
From P-40E pilot notes
700 miles at 188 IAS at 12000 ft with 100 us gal fuel (23 for warm up)
325 miles at 261 IAS at max continuous power at 9000 ft with 123 us gals.
From MiG 3 NII-VVS trials in 01-02/1941
At 0.9 V max (575-590 km/h) the serial n° 2115 reached 820 km, and the SN° 2107 857km failing to satisfy the NKAP request from October 40, for 1000 km range at 0.9 Vmax speed applied to all the new generation fighters Yak I-26, LaGG I-22, MiG I-200.
A big scandal exploded. Mikoyan and Goorevich quickly wrote to the NKAP
"Real MiG-3 technical range is 1100-1150 km, our calculations are based on NII-VVS and state trials where it was observed a 0.38 kg/km fuel consumption. Moreover, during the state acceptance trials it was found uncumplete fuel use from tanks. This fault is actually corrected." Afterwards it was explained that 0.38 Specific fuel consumption (SFC) was obtained with an altitude corrector. Even without it device, in April 1941 two others serial planes made 1000km range flight between Moscow and Leningrad as usual at 90% max speed and 7300m height.
The sn° 2592 achieved 1100 km at 562 km/h without using security (Warm UP) reserve and the sn° 2597, 970km, probably loosing a little its way in the cloudy sky. Both off them had the new rear smaller tank cutted by full 80 litres. Total capacity: 530l instead of 650l.
First serial MiG to be fitted with reduced tank the sn° 2859 made trials in may 1941, the 21th.
802 of this new tanks were made by the factory n°1 in may-june 41, and send to the units to be retrofitted instead of the older ones.
From the 12th series plane, rear tank was cutted by 110 litres instead of 80.
From the 14th series, wing tanks were cutted by 50 litres more. And reminded like that until the end of production.
Since MiG OKB largely overstepped state requirements, it's look like a success story. But it wasn't and ended tragically. In the meanwhile someone from the country rulling classes get interested in that polemic being only of technical problem kind…and made political conclusion that NII institute
deliberately minimized new plane achievements. In other worlds a sabotage act.
Brutal unjustified repression falled on AI Filin, the very competent NII-VVS manager and he was prosecuted; NII leading engineers Nikichenko and Voevodine were dismissed from their function and retrograded. What for? Without straight quality control the plane soon degenerated. For instance sn° 3943 was just able to reach 628 km, at 7200m height with 355kg (490l) fuel.
From Khazanov Medved, Maslov "Istrebitel' MiG-3"
An old book ,quite possiably out of date with new knowledge from the east says "...stability had been decidedly improved, as were the control forces, and by general consensus, the handling characteristics were now acceptable, although it was tacitly admitted that the MiG-3 was no novices's aeroplane and, while a major improvement on the MiG-1, it called for a high degree of piloting skill."
Since the MiG-3 was al little longer, it may improve longitudinal stability. Since it was 250 kg (3355 kg instead of 3099) heavier this adversely affected
manoeuvrability, and field performance. On the other hand, if the forwaed fuselage lengh was increased, the aft size remaind the same (...probalbly to short for a quick spin recovery. But it's just a supposal.). Probably the MiG-3 sn° 2122 was lost on january 41, the 19th for that reason. The test pilot Balunin being (with some success) in charge from 1940 of the full aerobatics program with MiG's experimental and first serial fighters, was switched to the MiG-3 spin trials programm. On may 1941, he failed to recover from a flat spin, bailing out from the sn° 2109.
The spin program was then stopped: some uncertainly reminds until now about the MiG-3 behavior on a spin, in particular those fitted with wing BS pods (and 250l aft tanks) .
About the control forces; the problem was corrected in statical and dynamical way on the experimental planes themselves, and then with an
unexplained delay on serial ones.
Regards