***Left To Right***.





1. AIM-7F Sparrow.
Type Medium-range, semi-active radar homing air-to-air missile
Place of origin United States
Service history
Used by Australia, Canada, Egypt, Greece, Iran, Israel, Italy, Japan, Jordan, Kuwait, Malaysia, Saudi Arabia, Singapore, South Korea, Spain, Taiwan, Turkey, United Kingdom, United States
Production history
Manufacturer Raytheon
Unit cost $125,000
Produced AIM-7D: 1959
AIM-7F: 1976
AIM-7M: 1982
Variants Sparrow I: AIM-7A
Sparrow II: AIM-7B
Sparrow III: AIM-7C, AIM-7D, AIM-7E, AIM-7E2/Skyflash/Aspide, AIM-7F, AIM-7M, AIM-7P, RIM-7M
Specifications
Weight 510 lb (230 kg)
Length 12 ft (3.7 m)
Diameter 8 in (200 mm)
Warhead High explosive blast-fragmentation
AIM-7F/M: 88 pounds (40 kg)
Engine Hercules MK-58 solid-propellant rocket motor
Wingspan 2 ft 8 in (0.81 m) (AIM-7A/B)
Operational
range
AIM-7C/D: 32 kilometres (20 mi)
AIM-7E/E2: 45 kilometres (28 mi)
AIM-7F/M: 50 kilometres (31 mi)
Speed AIM-7A/B: Mach 2.5
AIM-7C/E/F: Mach 4[1]
Guidance
system
semi-active radar
Launch
platform
Aircraft:

McDonnell Douglas F-4 Phantom II
McDonnell Douglas F-15 Eagle
General Dynamics F-16 Fighting Falcon
Grumman F-14 Tomcat
F/A-18 Hornet
JA-37 Viggen
F-104S Starfighter
Tornado F.3 ADV
F/A-18E/F Super Hornet
Mitsubishi F-2





2. AIM-54 Phoenix.
Type Long-range air-to-air missile
Place of origin United States
Service history
In service 1974–2004
Used by United States Navy (former)
Iranian Air Force
Production history
Manufacturer Hughes Aircraft Company
Raytheon Corporation
Unit cost US$477,131
Produced 1966
Specifications
Weight 1,000–1,040 lb (450–470 kg)
Length 13 ft (4.0 m)
Diameter 15 in (380 mm)
Warhead 135 lb (61 kg), high explosive
Detonation
mechanism
Proximity fuze
Engine Solid propellant rocket motor
Wingspan 3 ft (910 mm)
Operational
range
100 nmi (190 km)
Flight ceiling 100,000 ft (30 km)
Flight altitude 80,000 ft (24 km)
Speed Mach 5[1]
Guidance
system
Semi-active radar homing and terminal phase active radar homing
Launch
platform
Grumman F-14 Tomcat
General Dynamics-Grumman F-111B





3. AIM-120A/B AMRAAM (Kinda)
Type Medium-range, active radar homing air-to-air missile
Place of origin United States
Service history
In service September 1991–present
Used by See operators
Production history
Manufacturer
• Hughes: 1991–97

• Raytheon: 1997–present
Unit cost
• $300,000–$400,000 for 120C variants

• $1,786,000(FY2014) for 120D[1]
Variants AIM-120A, AIM-120B, AIM-120C, AIM-120C-4/5/6/7, AIM-120D
Specifications
Weight 335 pounds (152 kg)
Length 12 feet (3.7 m)
Diameter 7 inches (180 mm)
Warhead
High explosive blast-fragmentation
• AIM-120A/B: WDU-33/B, 50 pounds (22.7 kg)

• AIM-120C-5: WDU-41/B, 40 pounds (18.1 kg)
Detonation
mechanism
Active RADAR Target Detection Device (TDD)

Quadrant Target Detection Device (QTDD) in AIM-120C-6 – lots 13+.[2]
Engine Solid-fuel rocket motor
Wingspan 20.7 inches (530 mm) (AIM-120A/B)
Operational
range
• AIM-120A/B: 55–75 km (30–40 nmi)[3][4]
• AIM-120C-5: >105 km (>57 nmi)[5]

• AIM-120D (C-8): >180 km (>97 nmi)[6]
Speed Mach 4 (4,900 km/h; 3,045 mph; 1.3612 km/s)
Guidance
system
inertial guidance, terminal active radar homing
Launch
platform
Aircraft:

Boeing F/A-18E/F Super Hornet
Eurofighter Typhoon
General Dynamics F-16 Fighting Falcon
Lockheed Martin F-22 Raptor
Lockheed Martin F-35 Lightning II
McDonnell Douglas AV-8B+ Harrier II
McDonnell Douglas F-15 Eagle
McDonnell Douglas F-15E Strike Eagle
McDonnell Douglas F/A-18 Hornet
Northrop F-5S/T
Panavia Tornado ADV
Saab JAS 39 Gripen
Surface-launched:

NASAMS and others

Source: https://en.m.wikipedia.org