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My observation is that the Luftwaffe's greatest foe, was the RLM.
There were a great many aircraft that held potential, but the RLM's insistence that everything be able to carry bombs and/or be dive-bomb capable either delayed or killed projects.
Another stellar example is the political infighting within the RLM that hobbled many projects.
To be fair the invasion, had it worked, would have give them enough oil. Remember training hours were only cut in September of 1942, so Barbarossa, while long term causing some fuel issues, was not immediately limiting on training. The bigger problem was the mobilizing of training staff to fight instead of train, which if Barbarossa worked out (Moscow instead of Kiev) then it would have solved the material and oil problems.Dive bomber infatuation condemned only the He 177?
Decisions of Hitler's clique - 1st and foremost decision to attack Soviet Union - meant that Germany/RLM does not have enough of fuel to train it's aircrews, and that there is no cushion for mistakes. Those were not RLM's faults and even a working 4-engined bomber cannot help them now. Not having enough of chromium, nickel, copper and rubber was also not a fault of RLM.
In the case of the Fw187 they only added the dive requirement after it was abandoned as a single seat long range fighter and were trying to find other roles for it so the investment in design wasn't wasted and once the Bf110 proved vulnerable as an aircraft due to low performance.Amongst the brilliant ideas the RLM had for the Fw187 (instead of being the long range single seat fighter it was intended to be) was a dive-bomber.
The Me210 was required to be dive-bomb capable.
The Do217 was required to be dive-bomb capable.
The Ju88 was required to be dive-bomb capable (which it actually excelled at).
The Ju188 was required to be dive-bomb capable.
The list goes on, but it seems that Udet was the main force behind this, as he was a huge proponent of dive-bombers.
90 degree is a dive. 60 or less is a glide. A true dive stressed the airframe too much so they largely did steeper glides, but that even had to be changed to 45 degrees or less:Ju88s were used as dive-bombers in France, Norway and more extensively in the Eastern Front with KG51 and KG54.
In anti-shipping along the Baltic, Ju88s accounted for quite a few Soviet ships with dive-bombing tactics.
despite all the modifications, dive bombing still proved too stressful for the airframe, and in 1943, tactics were changed so that bombs were delivered from a shallower, 45° diving angle. Aircraft and bomb sights were accordingly modified and dive brakes were removed.
So then the SBD, D3A, A-36, Skua and the rest were all glide bombers.90 degree is a dive. 60 or less is a glide. A true dive stressed the airframe too much so they largely did steeper glides, but that even had to be changed to 45 degrees or less:
August Lichte, the Jumo chief engine designer responsible for the 213, regarded the 213 as the "Reinschrift dieser Bauart (Jumo 211)" - that is, the Fair Copy of the 211, so he saw the 213 clearly as a development and refinement of the 211. We can quibble about semantics, but the 213 was clearly not a completely new engine, not in the way that a DB 603 was compared to a 601, or a Merlin compared to a Kestrel. I wonder - would you also regard a C-Series R2800 as a completely new engine compared with the R2800 A?Nope - Jumo 213 was a whole new engine. New crankcase, crankshaft, head, ancillaries (including the cooling and lubricating system), reduction gear, pistons & piston pins, supercharger & it's drive... It weighted 950-1000 kg, vs. ~700 kg for the mid-war 211s.
Bramo developed the 323 from the Bristol Jupiter.
BMW licence built the Pratt & Whitney Hornet, from which the Mitsubishi Kinsei was also developed.
BMW developed the licence built Hornet into the two row 139.
The 801 was developed from both the Bramo 323 and the BMW 139.
Not sure how using a Japanese development of the Hornet would improve the situation with the Hornet development BMW 139, and its successor, the BMW 801.
All hail the one true dive bomberSo then the SBD, D3A, A-36, Skua and the rest were all glide bombers.
Good to know
I think Reinschrift in this context means 'engrossment' or ultimate version.August Lichte, the Jumo chief engine designer responsible for the 213, regarded the 213 as the "Reinschrift dieser Bauart (Jumo 211)" - that is, the Fair Copy of the 211, so he saw the 213 clearly as a development and refinement of the 211. We can quibble about semantics, but the 213 was clearly not a completely new engine, not in the way that a DB 603 was compared to a 601.
Part of the issue is the Kasei was only first run in 1938, a year earlier than the BMW 801. At that point the Germans didn't know how long the BMW would take given that it was supposed to be a rapidly finished and indeed it did enter production in 1940, same year as the Kasei. Their power output was virtually identical. The Kasei really offered no advantages.So if, say, Bramo had got a license for the Kasei in 1938 when the engine was reasonably mature, and had concentrated on getting that engine in production, the timescale might have been shortened, perhaps even with fuel injection from the start. After all, they managed to put fuel injection on the Jupiter
In the case of the Fw187 they only added the dive requirement after it was abandoned as a single seat long range fighter
I wonder - would you also regard a C-Series R2800 as a completely new engine compared with the R2800 A
The Kasei had no advantage in power or weight, but in availability, which is my point; it entered service in the Ki-21-II in December 1940, probably used in combat in China shortly afterwards, while the BMW 801, in December of 1941, a year later, was regarded as not combat worthy; experts expected half a year for the necessary modifications. Kasei-powered aircraft bombed the Prince of Wales and Repulse half a year before the BMW was regarded as safe to use over water for even short periods.Part of the issue is the Kasei was only first run in 1938, a year earlier than the BMW 801. At that point the Germans didn't know how long the BMW would take given that it was supposed to be a rapidly finished and indeed it did enter production in 1940, same year as the Kasei. Their power output was virtually identical. The Kasei really offered no advantages.
Now if the Japanese had shared/developed in conjunction with the Germans the Homare engine in 1940 instead of Germany trying to develop the BMW 802 that might have yielded something valuable, as despite the quality of the BMW 802, it was cancelled as basically irrelevant given the success of the BMW jet engines. Being lighter and higher powered as well as having a vastly better power to weight ratio the Homare could have replaced the BMW 801 in production if they could fix the engine's issues before 1943.
Not any different than the BMW801. Production commenced in 1940. The delay in front line service had to do with the aircraft rather than the engine. The choice of the Germans not to fit the BMW801 to other aircraft like the Japanese did with their bombers wasn't related to the engine AFAIK. After all the Do217E of 1940 used the BMW801 exclusively:The Kasei had no advantage in power or weight, but in availability, which is my point; it entered service in the Ki-21-II in December 1940, probably used in combat in China shortly afterwards, while the BMW 801, in December of 1941, a year later, was regarded as not combat worthy; experts expected half a year for the necessary modifications. Kasei-powered aircraft bombed the Prince of Wales and Repulse half a year before the BMW was regarded as safe to use over water for even short periods.
The Homare was essentially an over-ambitious Nakajima design that always had problems with lacking and inconsistent altitude performance and strong vibrations; it was used in many types because the Navy standardized on it. As a highly-tuned engine it needed high-strength materials and high-octane fuel, both in short supply. The first reliable version, the Homare 12, came out in the spring of 1944, and it took almost another year until problems with unreliable fuel flow were finally eradicated. Essentially, Germany would have been better served even with the Jumo 222, absent interference by Milch.
The Kasei had no advantage in power or weight, but in availability, which is my point;
Not any different than the BMW801. Production commenced in 1940. The delay in front line service had to do with the aircraft rather than the engine. The choice of the Germans not to fit the BMW801 to other aircraft like the Japanese did with their bombers wasn't related to the engine AFAIK.
The D-series engines did yes, but they also had a boost up to 2000hp. The boosted Kasei engine's HP was only 1530. Later higher powered Kasei engines increased in weight, such as the 23 series, which was 860kg and a max boost of 1820hp. Regular HP was 1600hp max vs. the D-series 1700hp. Don't forget the German engine also had the Kommandogerät integrated into the engine, which the Japanese one lacked. The Japanese 23 series engine also apparently had some propellor resonance issues as well. Information is lacking on the Japanese engine, so the limited figures might make it seem better than it really was, while with the BMW 801 we have so much info about it we can see all the warts.BMW 801 weighted about 50% more than Kasei.
In 1940 to the late 1942, BMW 801C/D were as problematic as that was the case for Sabre in the UK in 1941-42, or R-3350 in it's 1st year in service. The BMW 801A used on Do 217 wasn't cleared for the 3 min rating (bar for take off), just the 30 min one and less 'aggressive' ones - probably a reason why their reliability record seem to was decent.