Nakajima Kikka
Empty Weight: 2,300 kg
Loaded Weight: 3500kg
Wing Area: 13.20 m²
Engine: 2x Ne-20 - 475kgf thrust / 2x Ne-20 Kai - 570kgf thrust
(Note: Kikka prototypes used Ne-20, the Productions were intended to use Ne-20 Kai engine.)
Max Speed: (According to planned / calculated IJN...
VG.39
Empty Weight: ~2,210 kg
Loaded Weight: ~3000 kg
Wing Area: 14.0 m²
Engine: Hispano-Suiza 12Y-89ter
Take Off: 1160 CV
Nominal: 1088 CV at SL / 1200 CV at 3800m
Max Speed: (According to official data)
625km/h at 5750m
Rate of Climb: (According to most sources)
4:55 to 5000m
Armament:
6 ×...
VG.35 & VG.36
Empty Weight: ~2,080 kg
Loaded Weight: ~2,800 kg
Wing Area: 14.0 m²
Engine: Hispano-Suiza 12Y-51
Take Off: 1100 CV
Nominal: 1000 CV at SL / 1000 CV at 3250m
Max Speed: (According to official data)
590km/h at ????m (VG.35)
Rate of Climb: No Data
Armament:
1 × 20 mm HS-404 (60...
(VG.34-01, the aircraft that first flew 20 January 1940 and was later left at Villacoublay / Toulouse without its engine.)
Empty Weight: ~2,100 kg
Loaded Weight: ~2,740 kg
Wing Area: 14.0 m²
Engine: Hispano-Suiza 12Y-45
Take Off: 935 CV
Nominal: 850CV at SL / 920CV at 4200m
Max Speed...
VG.33
Empty Weight: 2,050 kg
Loaded Weight: 2,680 kg
Wing Area: 14.0 m²
Engine: Hispano-Suiza 12Y-31 (V-12, 36.05 L, 5.8:1, 2,400 rpm)
Take Off: 830 CV
Nominal: 760CV at SL / 860CV at 3250m
Max Speed: (According to official data)
455km/h at Sea Level
558km/h at 5200m
Rate of Climb: (According...
La-7 c/n 38102663 (Plant 381, Moscow)
Yakubovich's factory-data table lists it as:
• SL: 579 / 613 km/h
• 2,850 m: 645 km/h
• 6,000 m: 661 km/h
• Time to 5,000 m: 5.25 min / 4.6 min
597kph you have there is at military power
So actually that La-7 is doing 636 at SL with WEP and 680+ at 6250m, but this is the peak ultra high quality
I did but of reverse calculation of this
La-7 in 1945 with 3 x B-20 cannon: ASh-82FN: 3,223 kg.
613 / S.L.
661 / 6,000 m.
The engine power curve looks like this for ASh-82FN
Then i applied this power curve to La-5FN doing 583km/h at SL as per one of the test flights
Did you however take into account that
XP-55 has no wing slats and J7W1 does?
The reason I didn’t give single direct number but 26-27 at 100% and 24-25 with WEP is it’s both values, 1.10 and 1.15 CL