- Thread starter
- #101
BarnOwlLover
Staff Sergeant
As far as my original post, it seems that it wasn't really 100% practical for a single seat, let alone single engine, escort fighter anywhere until at least 1942. That was mostly because the allies could have access to 1500-2000+hp engines to lift the fuel armament, armor and such required of such an aircraft, as well as improvements in aero and such. And the big thing that helped there was two stage supercharging and everything that made that possible.
However, I should note that going from single stage to two stage usually wasn't a simple drop in job. Why did the Spitfire IX/VII/VIII run symmetrical underwing radiators? Why did the two stage Mosquitoes grow under propeller intakes similar to the Merlin P-51's supercharger intake? Speaking of which, why did the Merlin P-51s get a deeper, more pronounced radiator intake vs the Allison powered versions? Two stage supercharging makes more power, but needs more cooling to handle/use that power. Probably an oversimplification, but that's the simple crux of it.
Hence, even if the Mustang used the Merlin from the start, it would've needed a similar redesign to make the most of the two stage Merlins.
As far as something that did get made, what about maybe the Martin-Baker MB5 as a possible British escort fighter? It had the range and performance, but it wasn't a reality until 1944-45, by which time there was the Merlin Mustangs, the Hawker Tempest, and the Hawker Fury/Sea Fury and DH Hornet. Not to mention that though I like it overall, the MB5 was a bit outdated as far as construction (tube frame instead of a monocoque) and, like the Merlin Mustangs that were most produced/used, a bit heavy for the engine power being used. Of course, for the Mustang that was due mostly to outdated US stress and loading standards, for the MB5, I'd argue that using a monocoque fuselage would've saved weight due to better strength to weight ratio.
However, I should note that going from single stage to two stage usually wasn't a simple drop in job. Why did the Spitfire IX/VII/VIII run symmetrical underwing radiators? Why did the two stage Mosquitoes grow under propeller intakes similar to the Merlin P-51's supercharger intake? Speaking of which, why did the Merlin P-51s get a deeper, more pronounced radiator intake vs the Allison powered versions? Two stage supercharging makes more power, but needs more cooling to handle/use that power. Probably an oversimplification, but that's the simple crux of it.
Hence, even if the Mustang used the Merlin from the start, it would've needed a similar redesign to make the most of the two stage Merlins.
As far as something that did get made, what about maybe the Martin-Baker MB5 as a possible British escort fighter? It had the range and performance, but it wasn't a reality until 1944-45, by which time there was the Merlin Mustangs, the Hawker Tempest, and the Hawker Fury/Sea Fury and DH Hornet. Not to mention that though I like it overall, the MB5 was a bit outdated as far as construction (tube frame instead of a monocoque) and, like the Merlin Mustangs that were most produced/used, a bit heavy for the engine power being used. Of course, for the Mustang that was due mostly to outdated US stress and loading standards, for the MB5, I'd argue that using a monocoque fuselage would've saved weight due to better strength to weight ratio.