Originally posted by Vermillion
My understanding on the engine is that the WWII version of the engine of the Yak-9U was the VK107, the VK107A was introduced after the war which had water injection I believe (or some other form of WEP). The Korean vintage Yak-9U used the VK107A.
Its my bad........... the figures for the Yak 3 given were the VK107 -A figures and the only ones given for the VK 105 PF-2 are stated as 43 therefore they are prototype.............
G& K also wrote Soviet Combat Aircraft V I & II where one finds the same numbers..............
VVS test data usually show the test pilots name whose name/s is on your data??? if its a certain Major AG Kubyshkin then it will be relevant. (he also did the bulok of the La7 trials)
to correct my data for the prototype Yak 3 VK 105 PF-2
1) Yak 3 wings break at moderately high G
2) faster climb to 16400ft (yak 3=4.1 mins yak9U=5 mins)
3) slower at sea level Yak 3 =565 km/hr, yak 9U= 575 km/hr.
4) slower at 5000 m alt (a bit)
5) longer range 850 km v 675 km
6) less wing area 14.85 v 17.11 (roll rates?)
7) better std turn 19 v 20 secs
So this shows a comparatively (but slightly) better turning, climbing, accelerating, rolling AC with a tad slower top speed and a delicate disposition.............
Given it was lighter (and less power full) its dive accel will be less IMHO. But it may show a bit less drag allowing it to hold e a little easier.
I have translated the tables so if you want some help send me some copies...................alth
ough I am sure we have folk here who can read Russian