Jokosuka MXY6

Yokosuka MXY6 / 空廠 実験用小型滑空機 [MXY6]
     
Název:
Name:
Jokosuka MXY6 Yokosuka MXY6
Originální název:
Original Name:
空廠 実験用小型滑空機(MXY6)
Kategorie:
Category:
experimentální letoun experimental aeroplane
Výrobce:
Producer:
DD.MM.1943-DD.MM.1943 Chigasaki Manufacturing Co., Ltd., Chigasaki /
Období výroby:
Production Period:
DD.MM.1943-DD.MM.1943
Vyrobeno kusů:
Number of Produced:
3 (1 byl motorizovaný)
První vzlet:
Maiden Flight:
DD.09.1943
Osádka:
Crew:
1
Základní charakteristika:
Basic Characteristics:
 
Vzlet a přistání:
Take-off and Landing:
CTOL - konvenční vzlet a přistání CTOL - conventional take-off and landing
Uspořádání křídla:
Arrangement of Wing:
jednoplošník monoplane
Uspořádání letounu:
Aircraft Concept:
kachna canard
Podvozek:
Undercarriage:
pevný fixed
Přistávací zařízení:
Landing Gear:
kola wheels
Technické údaje:
Technical Data:
 
Hmotnost prázdného letounu:
Empty Weight:
490 kg 1080 lb
Vzletová hmotnost:
Take-off Weight:
640 kg 1411 lb
Maximální vzletová hmotnost:
Maximum Take-off Weight:
? kg ? lb
Rozpětí:
Wingspan:
11.142 m 36ft 6,66in
Délka:
Length:
9.660 m 31ft 8,31in
Výška:
Height:
4.212 m 13ft 9,83in
Plocha křídla:
Wing Area:
22.50 m2 242.19 ft2
Plošné zatížení:
Wing Loading:
28.444 kg/m2 5.83 lb/ft2
Pohon:
Propulsion:
 
Kategorie:
Category:
pístový piston
Počet motorů:
Number of Engines:
1
Typ:
Type:
Semi Nainenki Ha-90-11 vzduchem chlazený čtyřválcový motor s protilehlými válci v o výkonu 16.4 - 18,6 kW při 2 250 ot/min.
Vrtule dvoulistá dřevěná tlačná.
Semi Nainenki Ha-90-11 four-cylinder air-cooled boxer with engine rated at 22~25 hp at 2.250 rpm,
driving a two-blade wooden propeller a pusher configuration.
Objem palivových nádrží:
Fuel Tank Capacity:
? ?
Výkony:
Performance:
 
Maximální rychlost:
Maximum Speed:
320 km/h v ? m 198.8 mph in ? ft
Cestovní rychlost:
Cruise Speed:
? km/h v ? m ? mph in ? ft
Rychlost stoupání:
Climb Rate:
? m/s ? ft/min
Čas výstupu na výšku:
Time to Climb to:
? min do ? m ? min to ? ft
Operační dostup:
Service Ceiling:
? m ? ft
Dolet:
Range:
? km ? mi
Maximální dolet:
Maximum Range:
? km ? mi
Výzbroj:
Armament:
žádná None
Uživatelské státy:
User States:
Poznámka:
Note:
空廠 実験用小型滑空機 [MXY4] - Kūšō jikken-jo kogata kakkū-ki (MXY6) - Experimentální malý kluzák typu kachna (MXY6).
空廠 実験用小型滑空機 [MXY4]- Kūshō jikken-yō kogata kakkū-ki (MXY6) - Navy Experimental Canard-type Glider (MXY6)


Dai-Ichi Kaigun Koku Gijitsusho in April 1943, by designing three gliders with the canard layout, designated Yokosuka MXY6, and built by Chigasaki Seizo KK, one of the gliders later being fitted with a 22 hp Semi 11 (Ha-90-11) four-cylinder air cooled engine.
Zdroje:
Sources:
Tadeusz Januszewski a Kryzysztof Zalewski, Japońskie samoloty marynarski 1912-1945, tiel 2, Lampart, rok 2000, ISBN 83-86776-00-05
www.geocities.jp
archiv autora
URL : https://www.valka.cz/Jokosuka-MXY6-t41517#161558 Version : 0

Brief history:



Japanese naval air force from the beginning of the year 1943 seriously addressed in the proposal of captain Masaoki Tsuruna, who proposed the assault fighter duck concept, later known as the Kjushu J7W1 Shinden. In Japan, with still no plane duck the concept of the build and behavior of such aircraft was the great unknown. The technical staff of the naval air force was divided between supporters and opponents of this fighter aircraft. Eventually, a solution was found – in jokosuckém naval arsenal was commissioned the construction of three small gliders duck concept.

Gliders were allocated the designation MXY6, it was a very simple aircraft should have the approximate dimensions of the Shindenu, the designers even at the end of the airplane created a spinner, although it was a glider, different was also the design of the glider, that was in the glider wood. Kites gliders were re-built by Chigasaki Seizo K. To. The final mounting and assembly of the glider conducted a naval arsenal. This was the aircraft that was supposed to bring knowledge about the behavior of the aircraft in flight in all kinds of situations, therefore, was a glider equipped with hinges of the wings and horizontal surfaces, which allow for different settings of these areas. To the adjustment elements of the techs should get the help of the covers and the glass-enclosed nose of the plane is enabled to view on this device, in a glazed bow was still signalling light used for the communication with the towing aircraft. For the campaign used the trainer Yokosuka K5Y1 Willow. The behavior of the aircraft depending on the different surface of the device, it was possible to test using a variable load. Load simulate the mass of the propulsion unit. The chassis was tall, solid, bow-type with relatively small wheels in the front undercarriage legs was a tow hook. One of the gliders was rebuilt on a motorized glider, to the rear was mounted a weak four-cylinder engine Ha-90 power of 22 horses. The engine was probably installed to make it possible to extend the flight time, take-off your performance not be sufficient.

At the end of 1943 they flew the planes at the air base Oppama, their use of acquired designers the necessary experience, which they used during the construction of the overflow tank Shinden. Duck glider so he fulfilled the task for which it was built.


Used springs:
Tadeusz Januszewski and Kryzysztof Zalewski, Japońskie samoloty marynarski 1912-1945, tiel 2, Lampart, 2000, ISBN 83-86776-00-05
www.geocities.jp
author archive
.
URL : https://www.valka.cz/Jokosuka-MXY6-t41517#506641 Version : 0

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Jokosuka MXY6 -


Jokosuka MXY6 -


Jokosuka MXY6 -


Jokosuka MXY6 -


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