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Well the numbers should not be a problem as we are using the ones IOTL used on the 580 Bothas. The benefits of higher boost and/or compression ratio that 100 octane could permit would be nice but twin Perseus gives you a solid 1,800bhp as a base.A big problem with both of your engine swap schemes is that the Perseus engine used the same cylinders as the contemporary Hercules. Larger Perseus production means fewer Hercules engines. Granted you are only proposing to use the engines used in the Botha. Perseus development practically stopped with the outbreak of WW II. While the Perseus was allowed to be run on 100 octane fuel (with suitable notations in the log books) I don't believe it was ever approved for increased boost/power ratings. Welcome corrections?
The Perseus used much less fuel than the Hercules (after all twin Hercules are four Perseus) so the range would not be directly comparable to a Beaufighter's tankage.
The Blenheim was a gnat's slower than even a Beaufort. With an external torpedo (is there room for the tail on take off?) it must drop drastically to that of a Blackburn Roc on a bad day. Barely a third faster than a Vickers Vildebeest. Sidney Cotton tried putting lipstick on the pig but could not get even a stripped down smoothed out Blenheim up to a speed to evade anything. The torpedo is 167% of the Blenheim warload.
Which version of the Perseus are you using? The one/s most quoted for the Bothas offered either 750hp for take-off or (with a cropped impeller) 880hp for take-off. the first engine could give 880hp at 15,500ft but cropping the impeller gave 950hp at 5,500ft. 100 oct, if used, gave 950hp for take-off in the cropped impeller engines, it was good for about an extra 70hp at continuous climb rating down low (like 2750ft). Power is no better than either the Peregrine or Taurus and the Taurus has more power and less drag.
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Pom pom HV? Does this have a name?
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The 2nd part is trying to replace a torpedo plane/recon machine with an endurance of around 5 hours with a fighter?/recon/whatever with an endurance of around 2-3 hours.
The F.9/37 was a large plane physically (50 ft wing span, 37ft length and 386sq ft wing) but was actually a "light" airplane being about 90% of the weight of P-47 when empty and about 80-82% of the weight of the YP-38 (unarmed) empty. You have room (volume) to "add" all kinds of stuff. Do you have the strength? or do you need stronger spars, frames, landing gear etc if you add several thousand pounds to the aircraft.
Looking at the Blenheim would the F.9/37 using essential the same power engines be enough better performing due to smaller wing and fuselage (lower drag) to be worth making?