OK then, the real world:
Production: P-39N: 500, P-39N-1: 900, P-39N-5: 695 & Yak-9: 459 aircraft produced.
First Deliveries: P-39N: Nov.1942 (U.S.), Late 1943 (U.S.S.R.) & Yak-9: Dec.1942.
Performance:
P-39N & (Yak-9 Series I)
Altitude: Speed / Climb.
Meters: MPH / FPM
S.L......344 / 3980 (325 / 3299)
1km...362 / 4145 (338 / 3415)
2km...381 / 4220 (351 / 3278)
3km...398 / 3940 (352 / 3400)
4km...394 / 3460 (368 / 3030)
5km...388 / 3060 (371 / 2532)
6km...382 / 2685 (365 / 2044)
7km...376 / 2230 (357 / 1515)
8km...367 / 1745 (344 / 1056)
Maximums: 398.5mph/9,700m. & 4360fpm /2,225m. (373mph/4,340m. & 3445fpm/1,185m.)
Combat Ceilings (1,000fpm): 9,700m. (8,120m.)
Operational Ceilings (500fpm): 10,835m. (9,210m.)
Service Ceilings (100fpm): 11,735m. (10,080m.)
Turn Times: 19.0sec/3,311kg. - 7,301lb. (16L-17Rsec./2,825kg. - 6,229lb.)/1,000m.
Engines: Allison V-1710-85: 1,420hp., (Klimov M-105PF: 1,243hp. [1,260ps])
Wing Area: 213.22 sq. ft., (184.6 sq. ft.)
Wing Loadings: 34.15 lb./sq. ft., (33.74 lb./sq. ft.)
Power Loadings: 5.122 lb./hp., (5.011 lb./hp.)
Maximum Roll Rates: P-39D-1: 75 deg./sec. @ 235mph., ( ? )
Those are the numbers, this is part of the rest of the story:
Soviet Airpower in WW2, Yefim Gordon, Page 441 & 442
"...the first 'Cobas (P-400) arrived in December 1941 or January 1942 but it was not until May
that they became operational.
NII VVS sent a special 'task force' to Ivanovo to test the 'Cobras. The test pilots were pleased
by the fighter's handling, performance and excellent view from the cockpit; the tricycle
undercarriage allowed it to taxi at high speed over a snow-covered airfield with virtually no
risk of standing on its nose."
Page 446
" ...maneuvering the Cobra called for a steady hand. At the slightest inaccuracy during a tight
turn, a yo-yo maneuver or at the top of a loop the aircraft would go into a spin - often a flat
spin (from which the P-39 could not recover).
It should be noted that in early 1943 Soviet pilots tested the P-39's spinning characteristics.
Test pilot V. Ye. Golofastov reported that, at CG positions between 25.7 and 29% mean
aerodynamic chord, the aircraft recovered quickly if the spin recovery manoeuvre was executed
immediately after entering a spin. The US standard operational procedure for spin recovery was
rejected as too complicated."
The Yak-9:
Test pilot Fedrovi recorded, "...the new wing delivered a significantly better rate of roll and
aileron response." Compared to the Yak-7A."
" Fedrovi demonstrated the Yak-7DI (Yak-9) could initially outturn any Yak-1." The increase
in maneuverability and roll rate allowed the Yak-9 to outturn the lightened version of the
Yak-1 (1 x 20mm) through the first 360 degrees.
" At the altitudes that almost all of the combat occurred, the Yak-9 could outmaneuver the
Bf 109G." " The improved roll rate allowed the Yak-9 to make use of its superior turning
circle & vertical abilities to full effect against the Fw 190."
PS: Performance figures and information came from the following:
P-39N: Performance test reports for P-39N-1 42-4400.
Yak-9: rkka No. 0211 & 0212 Soviet Graphs and Soviet Combat Aircraft of the 2nd WW by
Yefim Gordon.