British know that Germans are buying Kestrel, since their 600 HP engine is late. How late is the next generation of engines?
At 5 km, the HS 12Y will do 20-25% less power than Merlin I/II/III in mid 1930s.
Once again, timing has a lot to do with it. Germans bought (or were loaned?) 1 or 2 Kestrels which were loaned around (each Kestrel powered more than one prototype). R-R got a He 70 as an engine test bed ( room for observers/instruments in the cabin).
However the DB 600 made a very public debut at the Zurich air meet of 1937 and Flight Magazine had a short write up in the Sept 2 1937 issue.
1937 | 2418 | Flight Archive
This would have caught any long range British single engine fighter designed in 1935-36 thinking the Germans were going to use 650-700hp engines with it's proverbial pants down. From then on it is a race between the different engines.
HS 12Y engine/s were several hundred pounds lighter in weight than a Merlin. This puts them in hunt in the mid 30s but fading. They are too light to stand up to higher rpm or higher boost when better fuels come along but in the mid/late 30s it is possible to design a working fighter using one.
Defender has to match the power, since, especially in era where radar coverage is spotty or non-existant, it will do the climb in order to match the position, altitude and speed that esort already has. And in case it suceeeded, ie. the escort somehow failed to take advantage of it's speed & altitude advantage, it has the choice to either get the bombers, or to tangle with escorts thus leaving bombers free.
The Defender needs to match the power to weight ratio of the complete fighter and needs to match the thrust to drag. Using a smaller/lighter plane means either a lower powered engine can be used for equal performance or a similar powered engine will give the defender better performance. And that was the problem in the 1930s.
A Spitfire I that had an all up weight of 5,875lbs had a powerplant weight of 2,035lbs (engine cowl 86lbs and engine mount 58lbs are included in structure) , a structure weight of 1890lbs and a "payload" of 1585lbs. The "payload" includes pilot and parachute (200lbs) armament (685lbs) fuel (646lbs) oil (54lbs), please note that this for a plane with no armor, no BP glass, unprotected tanks and a wooden two blade prop (96lbs + 36lb prop hub).
Adding another 500-600lbs of fuel even in unprotected tanks is a substantial increase in weight when looked at as a percentage.
Engine section of a P-51B/C was 2912lbs not including cowl/mount or fuel tanks (since they are selfsealing it tends to distort the picture, as does the propeller. 483lbs worth of prop on the P-51.
P-51 without rear tank went around 9600lbs clean so adding 500lbs of fuel is a much smaller percentage increase.
Engine installation in the P-51 was about 30% heavier (including two stage supercharger, after cooler and bigger radiators and coolant) for about 45-58% more power (61in boost/67in boost).
It was this increase in the power to weight ratio for the engines/powerplant that opened up the escort fighter.
The DB 601N in 1940 can do that power (1160 BHP) for 1 (one) minute, vs. Merlin XX five minutes, 2500 ft higher.
There may be some dispute about the time limit. Germans stumbled in development of the DB 601E/605 engines. Allies knew what kind of progress they were making, they were guessing at German progress and had to rely on captured equipment/documents to confirm German progress. We know now using the rectrospectroscope that the Germans had trouble for a considerable period of time in matching the Merlin progress.
The reason I've mentioned multiple LMGs is to avoid the low ammo carried for cannons in 1940 by UK and Germany.
The point was that from a weight/performance standpoint it doesn't make any difference. The Bf 110 wasn't a poor performer because it carried a pair of MG/FF cannon. It was a poor performer because of it's size.
I don't think that Ki 61 was any more advanced in aerodynamics than Spitfire or P-39. Internal fuel was some 750 L (around 200 US gals; double checked; self-sealing tanks), plus external fuel - two drop tanks of 200 L. Later it was 650 liters of internal fuel, together with introduction of 20 mm cannons, comparable internal fuel as the Typhoon with almost the twice the power.
So I'd repeat that it was doctrine, not technology that interfered with RAF acquiring the long range fighter early on.
Do you have a good source for the fuel capacity?
Some sources are all over the place (as low as 550 liters internal) and in general, when something is too good to be true, it often isn't true. Ranges are also all over the place but since the ranges almost never mention either speed or fuel capacity (external tanks or not) one is left with a lot of guess work.
The two different reports/charts on Spitfire Performance disagree with each other on both fuel capacity and weight.