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The He-162 was a way better fighter than any version of the Ta-152, proposed or buildt.
So was the P80 when introduced (beeing grounded twice due to high accident rate when introduced). To be fair, all high performance, 1st generation jet fighters experienced serious safety records. Still they were better than piston props. Accident rate of the He-162 in JG1 during 1945 was lower than for the Me-262 in EKdo-262 and Kdo. Nowotny in 1944.It was way better at killing its pilots, even the experienced hands of JG 1.
We will have to agree to disagree then, because everything I have ever read about the He 162 points to the contrary. They were a dead end design born out of desperation, with no hope of ever fullfilling its intended role. No amount of Hitler Youth with minimal glider training could have made an impact on allied air superiority using this aircraft. Post war testing saw the design relegated to the historical scrap bin of aviation curiosities. Smith and Creeks' excellent hardcover on this aircraft is the most comprehensive text written, and objectively points out the failure of this plane both technically and operationally. It took valuable resources away from the already battle proven Me 262 and Arado Ar234, and achieved absolutely nothing in return. With properly trained and experienced pilots ( which they were), the Ta 152 was more than a match for any allied fighter, whereas the He 162 came off second best every time. The Ta 152 had superior range, reliability and manouverability, could operate at all altitudes, and was a more developed and intrinsically well thought out design. The He 162 fell apart, fell out of the sky, and quite quickly fell from favour with its pilots. The pilots of the Ta 152, on the other hand, spoke in volumes, praising the quality and performance of their aircraft. Adolf Galland and Willy Messerschmitt were opposed to the production and deployment of the He 162 with good reason. It really was an inferior design.I am not sure that I can agree. The He-162 was a way better fighter than any version of the Ta-152, proposed or buildt. It also offered a more efficient fighter platform in terms of ressources and manhour investment. Performancewise, the future was in the jet age. The only aspect where I can see operational advantages for the Ta-152 /late Fw-190D is in (a) the low altitude range due to their better endurance and (b) their operational reliability due to the quircks which had yet to be worked out completely. Otherwise the jet own the prop driven fighter in every aspect, most notably survivability.
Ad. Dickfeld´s 136th victory was credited while flying a He-162A. Similarely, the 2nd TAF last ww2 europe loss is credited by british sources to be caused by a He-162A. Accounts differ but You go so far to claim that they were refuted which is not the case. Similar doubts exist for Ta-152 kill claims. Data is simply not sufficient to jump to conclusions.No Kills were ever credited to the He 162. The one possible exception was awarded to the AA battery, and the He 162 was incidentally in the area, by all accounts.
It is. Contrary to Your interpretation, crit Mach was the best justification for a new design. The He-162A could maneuvre at speeds where the Vampire, Meteor or P80 would already been rendered immaneuverable due to Mach tuck. That´s a rather serious advantage.The Meteor was never cleared for any acrobatics, unlike the He-162a.A higher critical Mach figure is irrelevant on an aircraft which breaks up in flight or in high G manouvres.
According to an US evaluation, the He-162 was attested to have the highest tactically useful Mach speed of all ww2 fighter. As the -262 had a crit Mach speed of M=0.86, I suppose the figure would be around M=0.87. The Baubeschreibung of the He-162 gives a limiting V-gleit figure at 1000 m of 1000 Km/h, which would resemble a safe max. dive speed of Mach= 0.826 at this altitude. The lim. Mach speed therefore would be M=0.83 lowest, with a corresponding crit. Mach speed of M=0.86. A slight bow snaking will be approached at very high speeds.
(...)
At the upper end of the speed range, the Vampire behaved in singular fashion with the onset of compressibility, and from M=0.71 up to 0.76 the aircraft displayed increasing porpoising and wing buffet until at M0.79 the aircraft would suddenly "break" up or down with the likelihood of a wing drop, giving the sensation of an "incipient" flick roll.
Roll-rate has really nothing to do with stall speed.I have read his reports, and the roll rate with such short wings is a given. This was as big a drawback as an advantage, with the He 162 displaying the "falling leaf" stall characteristics which were an inherant flaw in the design.
VAMPIRE:
Charackteristics of maneuverability:
Low wingload, mass concentrated, finely balanced ailerons. Light Stick (very sensitive), good roll charackteristics through the entire speed regime.
Elevator very sensitive, pulling to hard will give no stall warnings. Pilots have to be careful, not to enter unintended spins, esspeccially at lower speeds.
Rudder not very sensitive, demanded coarse movement to be of much consequence.
The aeroplane was agile within the 600-800km/h speed range at low level. At lower speeds, however, steep turns required coarse use of rudder to maintain height, and it was uncomfortably simple to stall in relatively shallow turns.
Stall charackteristics:
The stall was accompanied by quite a sharp wing-drop, but a surprising amount of aileron control existed right down to the stall, albeit with marked control buffet. One was advised to recover quickly while use of the most effective elevator could be maintained. Though by no means dangerous, the spin could be embarrassing owing to blanking of the diminutive rudders and the necessity to use coarse elevator control resulted in the aircraft pointing at terra firma for an uncomfortable length of time while speed built up.
HE-162A:
Charackteristics of maneuverability:
Very light stick throughout the entire speed regime. Aileron controll is good with a resulting roll rate considered to be superior to everything by US and RAF postwar tests (The US concluded that the X-1 approaches the roll rate figures of the He-162). Rudder controll is average.
Elevator controll is to sensitive, accompanied with latent instability at certain conditions. Max. turnrate is inferior to Meteor MK IV and Vampire MK III but sustained turn rate is very good.
Stall charackteristics:
The stall is approached on high angles of attack with prestalling warnings, particularely on the stick. The stall itselfe is quite comfortable, a nose down with full aileron controll.
The nacelle confined vision backwards. So be it, but remember, it had the highest tactical speed so this would be an issue in approach and take off conditions, which is where the TEMPEST "bested" the He-162a (contrary to the He-162a which went into aerial dogfight with the Tempest not beeing at take off condition). The stability problem is well documented in the sources, however it was adressed by various means like wingtip changes, though that still left a lot to be desired. The agility of the He-162a was excellent and basically superior to the Fw-190 which already had a poor turnrate but an excellent roll rate. The He-162 just emphasized this approach.The large nacelle hampered both vision and longtitudinal stability and the aircraft was simply not known for its agility or dog fighting prowess.
Yes. But why not putting it in perspective with the 1st operational Me-262a squadron? Kdo. Nowotny with 3 Staffeln strength suffered 26 Me-262 lost in one month. It suffered a worse attrition rate but had the benefit of beeing active in mid 1944 not spring 1945, with all it´s associated benefits in care, controll and thread environment.JG1 lost thirteen He 162s and 10 pilots. Only 2 were shot down by the enemy so the He 162 was doing a good job of killing its pilots without any help from the RAF or USAAF.
. The engine was still unreliable and prone to flame out and structural failures of the air frame still occurred, just as one famously did on V1 during a demonstration flight, killing test pilot Gotthard Peter. 3 He 162 test pilots were killed, Wedemeyer, Full and Peter, and yet the plan was for pilots with only ground training with the BMW engine and flights in a glider conversion to fly the type in combat!
Half an hour, yes. But remember thats referring to Sea level and max. permissable thrust after allowances for warming up the engines, acceleration and take off. In this condition, the VAMPIRE MKI´s endurance was 36 minutes, better by six minutes while the P80A on internal fuel could cover 49.5 minutes at SL.The fundamental problem of a lack of fuel was never addressed either. The He 162's half hour endurance makes a Bf 109 E look like a long range fighter.
#4b--------Lt. R. Schmitt-----3.5.45-------North Germ------------2nd TAF loss lists, but probably identical to 4b
Generally spoken, none of the claims could be confirmed or refuted with the present state of data aviability.
Thats what my books say too.Except this one which was awarded, by the Germans, to a flak unit, not Schmitt.
Cheers
Steve
No. It was not "awarded" at all. Schmitt notes in his flight log that he has "Feindflugzeug effektiv beschossen", which meant he fired at and observed strikes on the enemy a/c, the base for a claim. The 20mm AAA also observed effective hits on the Tempest and filed it´s own claim.
Czech built Me 262 (Avia S92 and S199) flew till 1957Allied jets like the Meteor and P80 went on to have very long careers, while the German jets can be measured in months.