Mauricio escribió:Para blancos de 5 m^2, según un piloto RAF que lo vuela, el alcance de detección es 185 Km. Date cuenta que esto lo pone al nivel del APG-80, el radar del F-16E/F, no al nivel del APG-79.
“Según” piloto italiano el Captor tiene “varias veces” mas alcance que el Foxhunter del Tornado.
Tambien “según” pilotos españoles el Captor hace cosas que se creían solo al alcance de un AESA. Y a la hora de compararlo con el alcance del APG-65, les da la risa. Varias veces...
Y otra vez “según” San Google al que el amigo de nombre ireproducible alude constantemente, el APG-68 blocaría blancos de 5 m² de RCS a 80 Km, el APG-80 a 130 km y el Captor a mas de 160 Km...
¿A quien creer?
xanthippos escribió:
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Ay Don Carlo. Impagable su articulo “Demon or Lemon” sobre el Tifón. Denota lo que le gusta e interesa y lo que no. Lo tiene ahí “abandonado” sin renovarlo hace un porrón de años...
Quizás le convendría hacerlo y cambiar algunas tonterías.
O también podría tirarlo a la basura, claro. Que creo que es lo que debería hacer...
Alguna muestra de la retahíla de gilipolleces que suelta:
The combined delta canard configuration and 538 ft2 wing size confer very low wing loading on 50% internal fuel, and are optimised for transonic manoeuvre and supersonic dash performance. The combination of sweep angle and unstable aft CoG is clearly intended for minimising supersonic drag, and is comparable to a classical supersonic interceptor like the Mirage series, but is more modest than the “supercruiser” 72° swept inboard wing section of the F-16XL/E.
Toma ya...
Eurofighter claim the engine has a supercruise capability, although the duration of possible supercruise has not been disclosed. As the engine is technologically of the same generation as evolved teen series engines, expectations that it can deliver the kind of supercruise performance provided by uniquely designed supercruising powerplants like the US F119 and F120 are difficult to accept.
Se nota que el tipo no ha vuelto a interesarse por el tema...
In an OCA/DCA combat configuration, clean, at 50% internal fuel (~6,500 lb), the Typhoon delivers a nominal sea level dry thrust/weight ratio of 0.82:1 and reheated thrust/weight ratio of 1.22:1 with a wing loading of 60.8 lb/ft2. Both are in the class of the F-15A/C, F-16A/C, MiG-29 and Su-27SK.
The overall impression resulting from a review of the aircraft's basic configuration, propulsion and fuel package is of a fighter with F-15 class transonic and supersonic agility at optimal weight, instantaneous manoeuvre performance slightly exceeding the teen series, all packaged into an F/A-18 sized airframe with installed thrust comparable to late build F/A-18 models. This reflects very closely the initial EFA design objectives.
The Typhoon's avionic package is built essentially upon the technology base used in the teen series fighters, but employs a higher level of integration against established in service teen series types.
The comparative advantages of the Typhoon over the Su-27/30 family exhibit similar sensitivities to technology upgrades in the Sukhoi fighters. Fitted with a phased array, longwave IRS&T, carrying ramjet R-77M missiles, supported by SuAWACS, and using growth engines we must seriously question how great a lethality margin the Typhoon would hold against such a fighter. The Sukhoi, inevitably, exhibits the same thrust/weight ratio advantages the F-15 does in extended range combat, which was a design objective for this type as it was for the F-15
Ho-ho-ho. Este no se ha coscado de los Cope India o los últimos DACT Canarios.
Ni supercrucero, ni fusión de sensores, ni leches...
Está bien como resumen general de lo que pensaba el amigo...








