Bueno, si quieren confirmar que esto es un chiste lean esto.
http://www.mehrnews.com/en/NewsDetail.aspx?NewsID=1808201
1) como el f-35? pero esas no son DSI y estan puestas de otra manera... no pensaron en altos AOA para la comparacion?
2) Me vas a decir que por eso no necesita proteccion termina la salida? Yo no te creo que los gases salgan a temperatura ambiente
3) Claro, la madera balsa es jodida de detectar... bue madera balsa no, pero casi
4) Así que le vas a poner 6 R-17/PL-12 o 2 bombas de 2000 libras. Claro que si, seguramente le sacas el motor y hay espacio para todo eso
5) Bueno, por que no.
6) Bueno si, despues de todo, el unico medio de deteccion que tienen es el viejo y fiable Eyeball Mk 1
7) Parecido a una M, como una W. Clarisimo. Es el mejor diseño por eso ellos lo usan. Y nadie mas puedo usarlo correctamente.
8) Claro, necesitabamos una prueba de que es liviano..... Tan liviano como un F-16 para los pesos cargados y maximos que dan. Y con dimensiones similares. Y vienen las preguntas de nuevo. Si el F-16 alcanza el peso maximo cargando de todo bajo las alas, como este bicho lo logra? Además si comparamos el tamaño de toma de aire del F-16 con este "coso" como hacemos para que con pesos y tamaños similares pero con un motor mucho mas chico tenga una performance decente?
En este punto muchachos, es cuando se va todo al carajo, la fisica es la fisica y con eso no hay suposiciones que valgan.
9) Ojo te destacan los instrumentos analogos... no cualquiera.
10) Esto es genial, es hidraulico, no FBW!!! Aca quedan 2 caminos
a) Consiguieron hacer un bicho como el bird of prey, pero estable para que no requiera FBW, cerramos todo, northrop, boeing, Dassault, NASA, todo y que se pongan un bar en la playa. No? No, es poco creible.
b) Este avion no vuela como un caza.
En fin, lean y disfruten........
Buzones, buzones, se venden buzones....
Alguno seguro compra
Top 10 F-313 most important features
TEHRAN, Feb. 4 (MNA) – In the anniversary of Iran's 1979 Revolution, Iranian president unveils indigenous Qaher 313 (Conquer) fighter jet, developed by Ministry of Defense and Armed Forces Logistics.
The top 10 technical characteristics of the F-313 fighter jet and some of the related data on its features and appearance:
1- Using Two inlets and inlet ducts make up the air induction system to deliver air to the engine. Due to an indirect angle of the engine to the air inlets, the radar reflectivity is reduced, and it makes angled design of inlet ducts to the surface to get radar energy wave, just like in F35.
2- The hot exhaust gas mixes with cold air through the inlet ducts, and gets cooler before it gets out of the exhaust system, to reduce heat effects on the surface of the aircraft.
3- Use of radar-absorbent materials in the body, to absorb wave energy and reduce radar reflection, for greater stealth effect of Qaher F-313 fighter.
4- Considering the estimated length and height of the aircraft is less than 16 and 4 meter, the two compartments with payload capacity of carrying two 2000 pound bombs, or greater number of smaller smart guided missiles, or at least 6 air-to-air missiles in the category of R-17 or PL-12.
5- Relatively large vertical tail surface has created favorable directional stability and with canted vertical tails create aerodynamic benefits as well specific appropriate lateral maneuvering capabilities.
6- The very large canopy gives a 360 degree visibility, which is essential for low altitude fly-by flights, especially helps ground mission attacks, and it is also very useful in close dog-fights.
7- The angled wings is perfect example of indigenous design for aircrafts, which gives a side profile like M, and similar to a W profile, is the best form to use in aircrafts.
8- Single-cycle landing gear is another proof that F-313 is a light weight aircraft, with minimum flying weight of 12 to 14 ton, and maximum flying weight of 20 ton.
9- There are 8 analog displays in the cockpit, which shows Multi-Function Display (MFD) technology has more room to improve in F-313, Qaher fighter jet.
10- Considering F-313 normal steering lever, the control systems, with the wing movable surfaces, rudder, and vertical stabilizer are hydraulics, and not fly-by-wire (FBW) system, since many today’s aircraft use “side-steering lever” control.
The advance computer designing software (CATIA) were used for designing F-313, and aerodynamic analysis methods such as computational fluid dynamics (CFD) also were used, with the help of numerical grid generation software (GAMBIT), flow analysis software (FLUENT) and other design computation software, which shows a complete scientific work in various areas of indigenous scientific and technology was used for F-313.