kool kitty89
Senior Master Sergeant
Aside from throwing out the light + heavy fighter concepts entirely, it seems like having both the light-weight PZL.39 and 'heavy' PZL.38 had used the existing Mercury VI.S2 engines as alternatives. (some of the engines actually considered for those planes -like the Gypsy twelve- were already about as heavy or heavier than the older Mercury while lower performing and the only advantage being smaller frontal area)When licence production of GR 14K was possible in Polish high command there were no interest in high power engine for the fighters. Till 1938 the PZL.38 Wilk was under development with pair of Foka engines - both should produce no less power as one powerful engine (2 x 420HP). Moreover, the Foka engines could be used solely for other types: P.39 lightweight fighter and LWS-3 Mewa reconnaissance aircraft. After the Foka fiasco a new engine was necessary. For the classic pursuit fighter (P.50) the Mercury VIII was chosen, as well GR 14M for other types (PZL.45 Sokół lightweight fighter, LWS-3 Mewa, PZL.48 Lampart two engine destroyer).
The PZL.39 itself did lead to the later PZL.45 project, and something close to that but using the older 645 hp Mercury engine from the start might have shown up soon enough to make a difference. Either developing a new, light fighter around the Mercury VI.S2 engine or using the PZL.11C (or possibly P.24) fuselage but using a smaller, low wing with fixed landing gear instead as an interim 'light' fighter. (faster but less maneuverable than the P.11) Climb rate would still be a problem with that older engine, though and tended to be a problem for most 'light' fighters in general. Though I guess a small, but thick wing would make for useful lift at low speeds and better take-off, turning ability, and better space for guns.
Continuing to use the old Mercury VI.S2 with the light fighter concept would mean similar forward fuselage structure could be used from the P.11 as well, keeping weight down and simplifying production. (it would limit further development, but that's where the P.50 would come in anyway) If the P.24 fuselage was used, and the new wing was designed with at least a little more power in mind, it shouldn't have been difficult to adapt the Mercury VIII when it was ready. (or for the Romanians to install 14k engines)
Yes yes, but I'm thinking of developments starting back around 1934/35, including interim fighter projects or light fighters and the PZL.38 and 39 projects specifically. Going with the old Mercury VI for the interim wouldn't be that big a step from the planned air cooled V-8 and V-12 engines. Development plans potentially following the pace of the PZL.37 bomber project.OK, but again Pegasus engines was not suitable for a fighters. Mercury VI was not considered any more for the future aircraft due an obsolete construction. On summer 1939 a licence production of Mercury VIII has begun and few dozen engines were produced before the war broke (captured engines Germans sold to Finland). After the summer tests of the P.50 prototype, this aircraft was found underpowered and PZL started looking for another powerplant. All Mercury VIII production was directed to P.11g "emergency fighter program".
I guess a better idea might have been to design the PZL.37 around Mercury VIII engines instead (more like the Blenheim) with more of a fast-bomber approach with somewhat reduced maximum load and then have a new, powerful engine with good altitude performance useful for a new generation of fighters and bombers.
One final thought on the Gnome Rhone engine topic: did Romania's license for the 14k not allow for them to export engines? With France being unreliable, it seems like importing Romanian manufactured 14ks would be much more attractive.