kool kitty89
Senior Master Sergeant
Wouldn't that 'rugged' design philosophy just put it in line with most (or all) operational American fighters during the war (including the Mustang)? Granted, that would inevitably have meant increasing the wing area over what the V1 prototype initially used, mostly likely to similar dimensions the A-1 and late A-0 variants used but with lower overall weight.
And SpicyJuan, the best alternate engine (of those actually in production) might have been the Jumo 211F. It was available sooner than the DB 601E and had better all-around performance than the 601N while using B4 fuel. If the 1 minute limit could have been successfully extended to a full 5 minute fighter emergency rating (remember this was historically a bomber engine) it would have had fairly competitive power to the DB 601E but at slightly lower critical altitudes or significantly better power while the 601E remained restricted. The larger/heavier 190 airframe also might have benefited enough from the added power and altitude performance the intercooled 211J offered to make the added drag worthwhile. (I forget the exact dates, but I believe the 211J was in production before the DB 605A -otherwise the 605A would have been more attractive performance wise, but perhaps not in terms of ruggedness and reliability)
The Fw 190C would still be a better heavy-fighter/interceptor 190 derivative, had the RLM allocated DB 603A engines for that project. (it isn't something that should have been affected one way or the other by the 211 vs 801 powered 190)
We've been over this before, but the turbocharged DB 603 arrangements really weren't worthwhile, the added weight and drag made for worse performance at most useful altitudes and the turbocharger added cost and complexity (assuming it could even be produced reliably).
And SpicyJuan, the best alternate engine (of those actually in production) might have been the Jumo 211F. It was available sooner than the DB 601E and had better all-around performance than the 601N while using B4 fuel. If the 1 minute limit could have been successfully extended to a full 5 minute fighter emergency rating (remember this was historically a bomber engine) it would have had fairly competitive power to the DB 601E but at slightly lower critical altitudes or significantly better power while the 601E remained restricted. The larger/heavier 190 airframe also might have benefited enough from the added power and altitude performance the intercooled 211J offered to make the added drag worthwhile. (I forget the exact dates, but I believe the 211J was in production before the DB 605A -otherwise the 605A would have been more attractive performance wise, but perhaps not in terms of ruggedness and reliability)
The Fw 190C would still be a better heavy-fighter/interceptor 190 derivative, had the RLM allocated DB 603A engines for that project. (it isn't something that should have been affected one way or the other by the 211 vs 801 powered 190)
We've been over this before, but the turbocharged DB 603 arrangements really weren't worthwhile, the added weight and drag made for worse performance at most useful altitudes and the turbocharger added cost and complexity (assuming it could even be produced reliably).