Heinkel HE-162 EP ARF 36.2 inches - KAV6628
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KAVAN |
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| Specifications | ||
| Wing Span | 36.2 in | 920 mm |
| Wing Area | 225 inē | 14.5 dmē |
| Length | 28.7 in | 730 mm |
| Weight | 19.4 | 550 |
| Wing airfoil | S 7055 mod. | S 7055 mod. |
| Radio Required | 3-channel minimum, Micro receiver, 3 micro servos (.32 oz 9 g or less) | |
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In 1944, Germany's air
defense problems were increasingly worsening; On top of that Hitler's
industrial plants were often the victim of Allied bomber raids always
straining what little resources they had left. Germany needed a new
fighter that was less expensive and also able to be produced faster. From
this thinking the Heinkel HE-162 was brought forward to fill the void.
Pilots were to be recruited largely from the Hitler youth and the initial
production rate at the beginning was to be 1,000 aircraft per month,
rising quickly to 4,000 aircraft per month. Extensive component
sub-contracting as well as underground assembly facilities were to be used
to produce the numbers desired. The specification was issued on September
14th, 1944 and the aircraft was to be ready for mass production by the
January 1st 1945. Production requirements called for a minimum of
strategic materials as well as the use of non-specialist laboring its
manufacture. It also had to weigh less than 4,409 lbs, be able to take off
in no more than 1,640 ft., and carry two 30 mm cannons. The result was an
aircraft with a one-piece wing of wooden construction, a semi-monocoupe
fuselage of duralumin, and a plywood nose and nose wheel doors. In
addition to the 153-gallon fuel tank behind the cockpit, the wing was
sealed between main and auxiliary spars to provide an integral tank with a
39.6-gallon capacity. The supplied BMW 190-003E-1-turbojet engine mounted
on top provided the aircraft with 1,764 lbs. of thrust, simplifying
installation and avoiding problems with intake and tail pipe ducting.
Chief test pilot Flugkapitan Peter flew the prototype on December 6th,
1945, bringing the aircraft to a speed of 522 mph and an altitude of
19,685 ft. On December 10th, before military
and government personnel, the starboard wing leading edges were torn off
during a high-speed pass that resulted in the crash of the aircraft and
the loss of life to the test pilot. The second prototype flew on December
22nd along with other development aircraft in the program that lead to the
findings of some aerodynamic problems. The third and fourth prototype flew
on the 16th of January 1945. Both of these aircraft had a few design
changes to correct the problems from the earlier setbacks. These changes
included wingtip extensions as well as increasing the overall surface area
of the vertical tail. The 30 mm cannons proved to be to heavy for the
lightweight airframe so instead two 20 mm cannons were substituted. A
total of 116 HE 162s were built, and more than 800 were in various stages
of assembly when the underground centers were overrun. |
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This
HE-162 is considered a park flyer. However, because it uses an electric
ducted fan for propulsion, you'll need to give yourself a little more
flying area than with a propeller-powered park flyer. Our test flights were with a 10 mph steady breeze. This is probably the most wind that I would fly the model in. The 300 size EDF moved the plane along at a good rate. I would not call it fast, like you might expect from a jet, but I would not call it a slow-flyer either. Most of the flight was either at full power or very close to it. On high rate ailerons the model rolls pretty well. Several attempts were made at a loop, but the model would keep falling out at the top. Being that this was a scale Warbird and not really designed for aerobatics, no other maneuvers were attempted. The HE-162 feels much like a trainer in the air. It is very stable and controls are soft when setup as the manual directed. There were no bad stall characteristics exhibited. LANDING: CONCLUSION:
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