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جستار: Air to Air missiles

  1. #1
    Aviation Storekeeper
    تاریخ عضویت
    Aug 2006
    محل سکونت
    تهران
    نوشته ها
    47
    سپاسگزاری
    1
    سپاسگزاری شده : 8 بار در 5 پست
    قدرت امتیازدهی
    0
    Array

    پیش فرض Air to Air missiles

    Name AIM-120A AMRAAM

    Country USA

    Manafacturer Hughes Missile Systems Division

    Date Deployed 1992

    Range 39.1 nm 45 miles (72 km)

    Speed Mach 4

    Propulsion One solid-propellant rocket motor

    Guidance Nortronics strapdown inertial and Hughes active radar.

    Warhead 45 lb ( 20.4 kg ) proximity and impact delay fused blast/fragmentation

    Launch Weight 335.2lb ( 152.05 kg )

    Length 11 ft, 11.9 in ( 3.655 m )

    Diameter 7 inches ( 0.178 m )

    Fin Span 2 ft, 0.7 in ( 0.63 m )

    us.gif (192 bytes)





    Name AIM-54A/C Phoenix

    Country USA

    Manafacturer Hughes Missiles Systems

    Date Deployed 1973

    Range 110 nm 126.7 ( 203.8 km )

    Speed Mach 4.3+

    Propulsion One Aerojet Mk 60 Mod 0 or Rocketdyne Mk 47 Mod 0 solid-propellant rocket motor

    Guidance Hughes DSQ-26 system using inertial, semi-active and active radar

    Warhead 132 lb ( 59.9 kg ) Bendix IR and Downey Mk 334 radar proximity and impact delay fused continuous rod blast/fragmentation

    Launch Weight 985 lb ( 446.8 kg )

    Length 13 ft, 1.8 in ( 4.01 m )

    Diameter 1 ft, 3 in ( 0.38 m )

    Fin Span 3 ft, 0.4 in ( 0.925 m )







    Name AIM-7F/M Sparrow

    Country USA

    Manafacturer Raytheon Co.

    Date Deployed July 1956

    Range 53.8 nm 62 miles (100 km)

    Speed Mach 3.7

    Propulsion One Hercules Mk 58 Mod 0 or Aerojet Mk 65 Mod 0 dual-thrust solid-propellant rocket motor

    Guidance Raytheon Advanced Monopulse Seeker inverse-monopulse semi-active radar homing

    Warhead 88 lb ( 39.9 kg ) proximity and impact delay fused Mk 71 continuous- rod blast/fragmetation

    Launch Weight 503 lb ( 228.2 kg )

    Length 12 ft, 1 in ( 3.68 m )

    Diameter 8 inches ( 0.203 m )

    Fin Span 3ft, 4 inches ( 1.02 m )





    Name AIM-9L/M Sidewinder

    Country USA

    Manafacturer Raytheon Co. and Ford Aerospace and Communications Co.

    Date Deployed 1976 for L 1983 for M

    Range 15.67 nm 18.04 miles ( 29.03 km )

    Speed Mach 2.5

    Propulsion One Thiokol or Bermite Mk 36 Model 7/8 solid-propellant rocket motor or ( later ) One reduced-smoke Thiokol Mk 36 Mod 9 ( TX-683 ) solid-propellant rocket motor

    Guidance DSQ-29 IR homing

    Warhead 22.5 lb ( 10.2 kg ) Hughes DSU-15/B active laser-fused WDU-17 annular blast/fragmentation

    Launch Weight 188 lb ( 85.3 kg )

    Length 9 ft, 4.2 in ( 2.85 m )

    Diameter 5 inches ( 0.127 m )

    Fin Span 2 ft, 0.8 in ( 0.63 m )









    Name Skyflash

    Country UK

    Manafacturer British Aerospace

    Date Deployed 1978

    Range 28 miles (45 km)

    Speed Mach 4

    Propulsion One Aerojet Mk52 Mod 2 or Rocketdyne Mk38 Mod 4 solid-propellant rocket motor

    Guidance Marconi XJ521 monopulse Semi-Active Radar Homing

    Warhead 87 lb ( 39.5-kg ) HE fragmentation with contact, delay action fuses.

    Launch Weight 425lb ( 192.8 kg )

    Length 12 ft, 1 in ( 3.68 m )

    Diameter 8 in ( 0.203 m )

    Fin Span 3 ft, 4 in ( 1.02 m )





    Name AIM-132 ASRAAM

    Country UK, Germany and Norway

    Manafacturer British Aerospace

    Date Deployed 1998 ?

    Range 8 nm ( 300 m to 15 km )

    Speed Mach 3+

    Propulsion One dual-thrust solid-propellant rocket motor

    Guidance strapdown inertial and Imaging Infrared

    Warhead 22.05 lb (10 kg) blast/fragmentation

    Launch Weight 220.5 lb (100 kg)

    Length 8 ft, 11.5 in ( 2.73 m )

    Diameter 6.6 in ( 0.168 m )

    Fin Span 17.7 inches (45 cm)









    Name MICA

    Country France

    Manafacturer Matra

    Date Deployed 1996 ?

    Range 27 nm 31.1 miles (50 km)

    Speed Mach 4

    Propulsion One SNPE solid-propellant rocket motor

    Guidance Inertial with ESD Actif 4A active/semi-active radar or SAT IR on final approach.

    Warhead Thomson Brandt blast/fragmentation 26.5 lb (12 kg)

    Launch Weight 242.5 lb (110 kg)

    Length 10 ft, 2.1 in ( 3.10 m )

    Diameter 6 in (150 mm)

    Fin Span ( 0.56 m )







    Name Mistral (ATAM)

    Country France

    Manafacturer ?

    Date Deployed 1988?

    Range 5 km ( at 4 km effective against helicopters )

    Speed 1492 knots

    Propulsion two stage solid propellant boost motor

    Guidance All-aspect Infra-red

    Warhead 3 kg HE tungsten ball

    Fuze Laser proximity

    Launch Weight 18 kg

    Length 1.80 m

    Diameter 90mm

    Fin Span 180mm

    25 km 40 km







    Name Super 530F/D

    Country France

    Manafacturer Matra

    Date Deployed 19?? / 1979

    Range 18.9 nm 21.75 miles (15 km)

    Speed Mach 3.7

    Guidance EMD Super AD26 semi-active radar homing

    Warhead 66.1 lb (30 kg) HE fragmentation with radar proximity fuze ( active radar fuzeing for D model)

    Launch Weight 551.1 lb (245 kg) 270 kg active radar fuze

    Length 11 ft, 7.4 in ( 3.54 m ) 3.80 m

    Diameter 10.35 in ( 263mm )

    Tailspan 2 ft, 1.2 in ( 0.64 m ) forward fins

    2 ft 11.4 in ( 0.88 m ) aft fin





    Name R.550 Magic

    Country France

    Manafacturer Matra

    Date Deployed 1975

    Range 5 nm

    Speed 1147 knots Mach 2.7

    Propulsion SNPE Romeo single-stage composite-DB rocket

    Guidance Infra-red ( not all-aspect )

    Warhead 27.6lb ( 12.5 kg ) high explosive

    Launch Weight 198lb ( 89.8 kg )

    Length 109 in ( 2.77 m )

    Diameter 6.2 in ( 157mm )

    Fin Span 26 in ( 660mm )





    Name R550 Magic 2 MK2

    Country France

    Manafacturer Matra S.A.

    Date Deployed 1985

    Range 320m minimum to 5,400m maximum

    Speed Mach 2.7

    Propulsion Advanced SNPE Richard rocket motor

    Guidance Infra-red homing all aspect

    Warhead 27.6 lb ( 12.5 kg ) Blast fragmentation with radar proximity fuze

    Launch Weight 198 lb ( 89.8 kg )

    Length 9 ft, 1.1 in ( 2.75 m )

    Diameter 6.18 in ( 157mm )

    Fin Span 2 ft, 2.3 in ( 0.66 m )







    Name Aspide Mk1/Mk2

    Country Italy

    Manafacturer Selenia

    Date Deployed ?

    Range 0.5 - 35 miles ( ? km ) 50 miles

    Speed Mach 4

    Propulsion One SNIA-Viscosa solid-propellant rocket motor

    Guidance Selenia monopulse semi-active radar homing

    Warhead 72.75 lb (33 kg) SNIA Difesa e Spazio blast/fragmentation

    Launch Weight 485 lb (220 kg) 230 kg

    Length 12 ft, 1.67 in ( 3.70 m ) 3.65 m

    Diameter 8 in (203 mm) 210 mm

    Fin Span 3 ft, 3.4 in ( 1.00 m ) same







    Name Python 3

    Country Israel

    Manafacturer Raytheon Armament Development Authority

    Date Deployed Mid 1980's

    Range 0.5 km to 15 km

    Speed Mach 3.5

    Propulsion One Rafael Armaments Development Authority double-base solid propellant rocket motor

    Guidance IR homing

    Warhead 24.25 lb (11 kg)

    Launch Weight 264.6 lb (120 kg)

    Length 9 ft, 10.1 in ( 3.00 m )

    Diameter 6.3 in (160 mm)

    Fin Span 2 ft, 9.9 in ( 0.86 m )



    This missile is credited with 50 kills in the Beka Valley in 1982. The Python can be fitted to F-15, F-16, all types of Mirage, F-5, F-4 Phantom and Kfir C-2 and C-7 aircraft





    Name Python 4

    Country Israel

    Manafacturer Raytheon Armament Development Authority

    Date Deployed Mid 1980's

    Range 0.5 km to 15 km

    Speed Mach 3.5

    Propulsion One Rafael Armaments Development Authority double-base solid propellant rocket motor

    Guidance IR homing

    Warhead 24.25 lb (11 kg)

    Launch Weight 264.6 lb (120 kg)

    Length 9 ft, 10.1 in ( 3.00 m )

    Diameter 6.3 in (160 mm)

    Fin Span 2 ft, 9.9 in ( 0.86 m )







    Name R-40R/T ( AA-6A/B Acrid )

    Country Russia

    Manafacturer -

    Date Deployed Late 60s

    Range 30 km (R-40) 50 km (R-40TD and R-40RD)

    Speed Mach 4.5

    Propulsion One solid-propellant rocket motor

    Fuze Radar and active laser

    Guidance Command, inertial and semi-active radar (R-40R) Command, inertial and IR (R-40T)

    Warhead 70 kg HE fragmentation

    Launch Weight 475 kg

    Length 6.2 m

    Diameter 355 mm

    Fin Span 1.8 m

    Platforms Mig-25





    Name R-60 ( AA-8 Aphid )

    Country Russia

    Manafacturer ?

    Date Deployed 1975

    Range 3 km, 5 km 10 km

    Speed Mach 2+

    Propulsion One solid-propellant rocket motor

    Fuze Two active radar fuze aerials located aft of the moving control fins, and a single strake running down the forward half of the body. Active laser in R-60M

    Guidance All aspect Infrared

    Warhead 6 kg ( 1.6 kg of which is uranium ) HE fragmentation

    Launch Weight 65 kg

    Length 2.08 m

    Diameter 130 mm

    Fin Span 0.43 m

    Platforms Su-24, Su-25, Mig-23, Mig-27



    Name R-33E ( AA-9 Amos )

    Country Russia

    Manafacturer Vympel

    Date Deployed 1985?

    Range 160 km

    Speed Mach 4.5

    Propulsion solid rocket

    Fuze Active radar

    Guidance Inertial, command updates and semi-active radar

    Warhead 47 kg HE fragmentation

    Launch Weight 490 kg

    Length 4.15 m

    Diameter 380mm

    Fin Span 1.18 m ( 0.9 m wingspan )

    Platforms Mig-31, up to 6 can be carried



    Name R-27R/T ( AA-10 Alamo A/B/C/D )

    Country Russia

    Manafacturer Vympel

    Date Deployed 1982

    Range 2 - 80 km R-27R 70 km R-27T 130 km R-27RE 120 km R-27TE

    Speed Mach 4

    Propulsion One solid-propellant rocket motor

    Guidance SARH R-27R, R-27E All-aspect Infrared R-27T, R-27TE

    Warhead 39 kg expanding rod

    Launch Weight 253 kg R-27R 254 kg R-27T 350 kg R-27RE 343 kg R-27TE

    Length 3.70 m

    Diameter 230 mm

    Fin Span 0.77 m

    Platforms Mig-29, Su-27, Su-35



    Name R-73 ( AA-11 Archer )

    Country Russia

    Manafacturer Vympel

    Date Deployed 1980s

    Range 20 km (R-73M1) 30 km (R-73M2) 40 km

    Speed Mach 2.5

    Propulsion One solid-propellant rocket motor

    Guidance All aspect Infrared

    Warhead 7.4 kg HE expanding rod warhead

    Launch Weight 105 kg (R-73M1) 115 kg (R-73M2)

    Length 2.9 m

    Diameter 170 mm

    Fin Span 0.51 m

    Platforms Mig-29, Mig-31, Su-24, Su-25, Su-27, Su-35



    Name R-77 ( AA-12 Adder )

    Country Russia

    Manafacturer Vympel

    Date Deployed 1992

    Range 50 km 90 km 150 km

    Speed Mach 4.5

    Propulsion solid rocket

    Fuze Active radar

    Guidance Radio Command + active radar homing on terminal phase (<20 km)

    Warhead 30 kg HE fragmentation

    Launch Weight 175 kg

    Length 3.60 m

    Diameter 200 mm

    Fin Span 0.35 m

    Platforms Mig-29, Mig-31, Su-25, Su-27, Su-35





    ch-t.gif (921 bytes)

    Name PL-7

    Country China

    Manafacturer China National Aero-Technology Import and Export Corporation

    Date Deployed Mid 1980's

    Range 500m minimum to 14.4 km (5 miles)

    Speed Mach 2.5

    Propulsion One solid-propellant rocket motor

    Guidance IR, all aspect homing

    Warhead 28.7 lb (13 kg) HE fragmentation

    Launch Weight 196.25lb (89 kg)

    Length 8 ft, 11.1 in ( 2.72 m )

    Diameter 6.18 in (160 mm)

    Wingspan 2 ft, 2 in ( 0.66 m )





    Name PL-10

    Country China

    Manafacturer China National Aero-Technology Import and Export Corporation

    Date Deployed Mid 1980's

    Range 37 miles

    Speed Mach 4

    Propulsion One solid-propellant rocket motor

    Guidance Radar guided, Semi-active terminal

    Warhead 73lb ( ? kg ) HE fragmentation

    Launch Weight 484lb ( ? kg )

    Length 12 ft ( ? m )

    Diameter ?

    Wingspan ?
    جهان سوم جایی است که اگر بخواهی کشورت را بسازی خانه ات خراب میشود...
    و آنان که کشور خراب کردند کومه ی دیروزشان
    امروز چه بزرگ است کاخ است
    خانه من اکنون
    خاطره است

  2. #2
    Aerographer's Mate
    تاریخ عضویت
    Jan 2006
    نوشته ها
    398
    سپاسگزاری
    0
    سپاسگزاری شده : 523 بار در 142 پست
    قدرت امتیازدهی
    19
    Array

    پیش فرض

    I have to delete posts which arent in English

    sorry friends :)
    ...آن ها که بر فراز آسمان درس پرواز آموخته بودند ، دیگر زیستن بر خاک زمین میسرشان نبود و جنگ بهانه ای بود تا مشق نیمه کاره ی آسمانی بودنشان را کامل کنند ....

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