Originally posted by gripen
I think G-6/G-14 supposed difference has been covered earlier. Regarding the rest, does the rarity of the gondolas actually speak for the larger airframe like the G.55 which could carry comparable load internally?
Nope, it simply speak for the need of an air superiority fighter, not another bomber destroyer.
Since there wasnt a DB603 available in big numbers, there couldnt be a G56.
The german fighters was so smal, cause the available engines dont had that much power and was smal. When the fighters got developed there wasnt a Jumo or Db603, although documents from 1941 already saw this engines as successor of the BMW801 for the FW190, but as we know, this engines came very late. With the size of the G55, the 109 would have been another Hurricane, Spitfire, P40 or G55, while the allied planes got particular much stronger engines in 1943. As result the "big" 109 would have been lost. With the disadvantage in power the 109´s still could disengage by diving and they was still fast(at least faster than the G55).
When germany got powerfull big engines they also created more big fighters, like the Ta152, Do335, Me309 etc, but that was in 1944, already much to late. And actually the Luftwaffe had a very big fighter from the beginning, the 110, strangewise this construction didnt follow the way of the 109, of an heavy wingload, otherwise the Luftwaffe would have had a german "P38" already in 1939. Not to manouverable, but very fast. A single seat version also would have been very interesting(200 -300 kg less weight right away).
Last but not least, the wingload absolutly dont matter, its the lift, produced by the wing that matter and due to the slats the 109 did produce the max lift of a more big wing. Most tests which refer to a bad turning 109 refer to the heavy elevator anyway, not to the smal wings, while the experienced pilot could use the trim to overcome this problem. Hermann Graf wrote about it and also Hartmann often did refer to the trim before making manouvers, while most experienced pilots simply didnt turnfight anyway. They used the good vertical behaviour, the speed and the excellent slow speed handling(specialy important while high alt fights).
Originally posted by gripen
For various reasons there were a lot G-14s without the MW50. In practice the factories tried to produce planes from what ever parts were available; as an example there is photo evidence of K type airframe with the DB 605AS.
I doubt there was many G14´s without MW50, while the G´s got the MW50 Rüstsatz. If a G14 was without MW50 it must have been very late in the war, or it was a AS only used for the high alt task, above rathed altitude, where the MW50 mainly gave weight, but in general the MW50 equipment was installed.
btw, was the 109´s able to use the MW50 tank as aux tank?? Never did read about it, unlike to the 190A´s, but they had fuel inside their "Sondernot-Tanks" anyway.
Originally posted by gripen
Basicly there is plans and then there is reality. Often these are not similar.
I dont found any proov that the reality wasnt similar to the plans regarding the G14´s and K4´s. There was variations, but where are the proofs that this variations was normal??
If the G14 dont had MW50 equipment, it would have been nothing else than the late G6 or G6AS, also they got the wooden tail and a "Erla Haube".
Originally posted by gripen
These values comes from the datasheet dated 13.8.1944 ie before the production of the K-4 was started. In January 1945 Mtt listed weight as 3400kg.
The 3400kg is a rounded calculation value that we see in many german tests, or do you think the K4 had exact 3400kg?? In the datasheets we also see a 3300kg 109G14, while the exact weight was below this.
In the datasheet from 13.8.1944 you can also find this rounded weight of 3300kg for comparison and calculations, while the take off weight vary up and down, depending to the plane.
Greetings,
Knegel