Pa ne navodis ti Maverika bas kompletno sam sve do cilja,vec hvatas smer a glava tera na zakljucan cilj.Potrebno je neko vreme da se navodi dok projektil ne krene u zahvat,posle toga samo ima kabuuuummmmm.

Cuo sam skoro da Rumuni nikad nisu usli u serijsku proizvodnju svoje verzije. Jel zna neko da li je to istina?
Ima li neko podatak da li su Maverici koristeni u ratovima u bivsoj YU i kako su se pokazali?

Pogresno si cuo.Proizvodili su se i to u po prilicnom broju.Model IAR-93A je proizveden u 36 primeraka, a model IAR-93B je proizveden u 165 primeraka (po nekim zvanicnim podacima).

IAR-93A: A simple yet effective light attack and tactical reconnaissance warplane well suited to the operational requirements and capabilities of the two sponsor nations, this type was designed from 1970 as a shoulder-wing monoplane of all-metal construction with swept flying surfaces and tricycle landing gear. The type is known to the Yugoslavs as the SOKO J-22A Orao 1 and to the Romanians as the CNIAR (later Iav Craiova and now Avioane) IAR-93A. Each country built two prototypes (one single-seater and one two-seater), the single-seaters making their first flight on the same day in October 30, 1974 and two-seat prototypes following in January 1977. Next came 30 pre-production aircraft (15 each in Romania and Yugoslavia) that flew during 1978 and through a successful development program paved the way for the type to enter full production in Romania during 1979 and in Yugoslavia during 1980. The first model to enter in service, in 1981, was the IAR-93A produced in single-seat form purely for the operational role and in two-seat form for the conversion and armament training roles. Both variants have provision for a maximum disposable load of 1500 kg on five hardpoints (one under the fuselage rated at 500 kg and four under the wings with the inner two units each rated at 500 kg and the outer two units each at 300 kg). In other respects, the IAR-93A differs from J-22B Orao 2 in details such as the accommodation of its one or two crew members on one or two Martin-Baker Mk RU10J zero/zero ejector seats, a non-afterburning powerplant of two Turbomecanica/Orao (Rolls-Royce/Bristol Siddeley) Viper Mk 632-41R turbojets each rated at 17.79 kN dry and supplied with fuel from an internal capacity of 2950 liters in single-seat model or 2700 liters in the two-seat model, length of 14.90 m including probe for the single-seat model or 15.38 m including probe for the two-seat model, wheel base of 5.40 m for the single-seat model or 5.88 m for the two-seat model, empty equipped, normal take-off and maximum take-off weights of 6150, 8826 and 10326 kg respectively, maximum level speed ‘clean’ of 1070 km/h at sea level, maximum cruising speed of 730 km/h at 7000 m, ferry range of 1900 km with tree drop tanks, radius of 260 km on a lo-lo-lo attack mission with four rocket launchers, or 380 km on a hi-hi-hi patrol with tree drop tanks, or 450 km on a lo-lo-hi attack mission with two rocket launchers, six 100 kg bombs and one drop tank, or 530 km on a hi-hi-hi attack mission with four 250 kg bombs and one drop tank, maximum rate of climb at sea level of 2040 m per minute, and service ceiling of 10500 m. Production of this Romanian version was completed by the delivery of 26 single-seaters and 10 two-seaters.[/b][/u]


IAR-93B: This is the upgraded Romanian version first flown in 1985 and produced in single-seat and two-seats forms
 to a total of 165 aircraft. The variant has integral fuel tankage rather than rubber fuel cells in the wings for a maximum fuel capacity of 3120 liters, can carry a maximum disposable load of 2800 kg on uprated hardpoints, and is fitted with an afterburning powerplant of two Viper Mk 633-41 turbojets each rated at 17.79 kN dry and 22.24 kN with afterburning. In other respects, the IAR-93B differs from the J-22B Orao 2 in details such as its empty equipped, normal take-off and maximum take-off weights of 5700, 8400 and 11200 kg respectively, maximum level speed ‘clean’ of 1160 km/h at sea level, maximum cruising speed of 1089 km/h at 5000 m, maximum rate of climb at sea level of 4500 m per minute, and service ceiling of 13200 m. Some IAR-93s are configured for the low-level air defense role with a twin-rail unit on each underwing hardpoint for a total of eight AAMs.[b][u]

Zaboravih da odgovorim. Rakete AGM-65B Maverick kao ni domace rakete tipa "Grom B" (inace zamena za AGM-65B) nisu jos koriscene kao operativne.Jos uvek se rade ispitivanja, do duse jako sporo sve to tece ali.........trenutno sluze samo za fotografisanje

nanishaniti cilj uopshte nije lako . avion se krece i vidno polje kamere se stalno pomera (igrachi simulacija to dobro znaju ) . obichno se ili avion dovede u stabilan let pomocu autopilota (ali tad je laka meta za pvo) ili se kamera usmeri tako da "prati nos" - kao kad gadjash topom - nishani se celim avionom

p.s. grom mora da se navodi direktno do cilja (radio-veza ,shta cesh ) . agm-65 b su koriscene 1991 da potope jednu korvetu marke rade konchar koja je "ostala" hrvatima ....