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AIM-9B Sidewinder


First generation Sidewinder missile


Overview


AIM-9B Sidewinder

AIM-9B Sidewinder missile on display at the Royal Military Museum Brussels.
Source: Marcelloo - © CC BY-SA 3.0

Origin
United States
Type
Short range air to air missile
Entered service
1956 (AIM-9B)
1969 (AIM-9F)
Status
Limited service
Development
1950 - Mid 1950's
Developer
United States - NOTS (Naval Ordnance Test Station)
Production
1955 - 1962 (AIM-9B)
Producer
United States - Ford Aerospace (Philco Ford)
United States - General Electric
Germany - Bodensee Gerätetechnik (AIM-9F)
Number produced
240 AIM-9A
Over 80.000 AIM-9B
15.000 AIM-9B/F in Germany
Designations
AAM-N-7 Sidewinder I (AIM-9A)
GAR-8 (AIM-9B)
AAM-N-7 Sidewinder I (AIM-9B)
AIM-9B FGW.2 (AIM-9F)
Rb 24B (Swedish service)

Description


Introduction

The AIM-9B Sidewinder is an early Cold War era short range air to air missile of American origin. The AIM-9B was the first operational missile in what would become a family of many generations of infrared guided missile used and developed till present day. Originally it was known as the AAM-N-7 Sidewinder IA in US Navy service and GAR-8 in US Air Force service until renamed AIM-9B in 1963.

Design

The AIM-9B has a classic layout with the passive infrared homing sensor in the nose, followed by the guidance and warhead sections and the rear half is made up of the rocket motor. There are four swept wings at the front and larger clipped wings at the rear. This early model Sidewinder had limited maneuverability and the seeker required the pilot to position the launch aircraft within strict parameters for a successful launch.

Guidance

The AIM-9B uses a passive infrared homing seeker. This early model seeker was uncooled and could only lock on to the exhaust of a jet aircraft, making it a rear aspect only missile. Ground clutter and the sun also interfered with the seeker, and flares could easily fool the seeker. The limited tracking rate could not keep up with sharp evasive maneuvers of target aircraft. Despite all this the AIM-9B was used successfully against various Soviet produced aircraft during the Vietnam war.

Firepower

The blast-fragmentation warhead has a 4.5 kg explosive charge and lethal radius of several meters. A passive infrared proximity fuse detonates the warhead. Early model Sidewinders did sometimes fly into the tailpipe of the target aircraft, severing the rear fuselage upon detonation. In other occasions the warhead did not detonate. One missile was recovered and sent to the Soviet Union for testing and reverse engineering after getting stuck in the fuselage of a Chinese MiG-17 during the Second Taiwan Strait Crisis in 1958.

Platforms

The relatively small size of the AIM-9B and placing no requirements on the aircraft's radar set made the AIM-9B easy to integrate into many existing and new fighter aircraft. First operational use was on US Navy FJ-3M Fury and F9F-8 Cougar. Several export models of the F-86 Sabre included the ability to launch the AIM-9B. The most notable platforms during the Vietnam were the F-8 Crusader and F-4 Phantom II. These were armed with the AIM-9B and the US Navy and US Air Force specific successors such as AIM-9D and E.

Users

The main user of the AIM-9B was the US military. It was developed by the US Navy, but also adopted by the US Air Force. Both used it actively during the Vietnam war. The AIM-9B was also exported in quantity to US allies in Europe and around the world. Tens of thousands of these missiles were produced, including license production of the baseline and improved AIM-9B in Germany. The AIM-9B was developed in many other variants, which often relegated the AIM-9B to reserve use.

Variants


AIM-9B Sidewinder

AIM-9B Sidewinder air to air missile on display at the Phillippine Air Force Aerospace Museum.
Source: RoyKabanlit - © CC BY-SA 4.0

List of AIM-9B variants

AIM-9A
The AAM-N-7 Sidewinder I was used for testing purposed and only 240 were ever built. These were built from 1955 and formally entered service in 1956 but was never actively used. In 1963 this early model was renamed AIM-9A.
AIM-9B
The main production model was the AAM-N-7 Sidewinder IA, known as GAR-8 to the US Air Force. This was renamed to AIM-9B in 1963. Over 80.000 of the AIM-9B were produced.
AIM-9F
The West German production line for the AIM-9B was updated to the AIM-9B FGW.2 model to improve performance. This retained the wide cylindrical nose of the AIM-9B while adding a cooled seeker, improved nose dome and solid-state electronics. The FGW.2 was also known as AIM-9F.

Details


Facts AIM-9B Sidewinder AIM-9F Sidewinder
General
Origin
United States
Type
Short range air to air missile
Dimensions
Length
2.83 m
Diameter
127 mm
Wingspan
0.56 m
Weight
70.4 kg
Guidance
Guidance mode
Passive infrared homing
Cooling
Uncooled seeker
Field of view
25°
Track rate
8 to 11 °/s
Lock range
About 4 km
Aspect
Rear aspect only
Warhead
Type
Blast fragmentation
Weight
4.7 kg HBX
Fuse
Proximity and impact
Propulsion
Type
Solid propellant rocket motor
Model
Thiokol MK 17
Thrust
17.8 kN for 2.2 seconds
Engagement envelope
Speed
Mach 1.7
Range
4.8 km maximum (practical range due to lock range and 20 s of guidance)
0.9 km minimum
G force
2 G at launch
10 G overload

Media


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