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HN-5A (SA-3) Chinese Man Portable Surface-to-Air Missile (MANPAD)

HN-5A

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Basic Information
Name
HN-5A (SA-3) Chinese Man Portable Surface-to-Air Missile (MANPAD)
Designation
HN-5A
Alternate Designation
Equipment Type
Manufacturer
Date of Introduction
1972
Description

The HN-5A (SA-3) Chinese Man-Portable Surface-to-Air Missile (MANPAD) is designed to engage propeller-driven aircraft and helicopters. It originated as a copy of the Soviet SA-7 Grail but has since been updated to the HN-5A. The original HN-5 guidance technology was relatively primitive, using an uncooled lead sulfide (PbS) infrared (IR) seeker and following the target's flight path until intercept. The uncooled IR seeker proved very susceptible to homing on the hottest object in its field of view, which was often something other than an aircraft. The HN-5A features a cooled seeker with a background noise rejection filter, an extended detection range, and proportional navigation, which steers the missile onto an interception course. It also has a heavier warhead. The HN-5A has replaced the HN-5 in production and is now available for export. The launch tube has simple sights. The power supply is under the tube. The missile has a long pipe-like body with very small foreplanes and angled steering vanes extending to the rear. The launch procedure for the HN-5 was nearly identical to the SA-7.

Ground Specifications
Crew 1
Max Speed 1850.4 km/h
Range 4.4 km
Variants
LHN-5A The HN-5A has a greater detection range for the IR seeker and a reduced susceptibility IR background noise.
HN-5B The HN-5B has an increased maximum altitude of 8,202 ft (2,500 m).
HN-5C This is a mobile launcher system. There is one four-tube box on either side of unmanned pedestal. A laser rangefinder, thermal imager and TV camera for fire control are in a mount atop the pedestal. Eight reload missiles are in the vehicle body. Total mounted weight is 4,409 lb. (2,000 kg). This version has been displayed on a small flat-bed truck and a scale model of 6 x 6 wheeled armored reconnaissance vehicle. Originally, it was shown on the HRB-230 cross-country vehicle. During the 1997 Paris Air Show, a model of the WZ551 APC was on display with the HN-5C system mounted on the ve hicle's roof. The WZ551 version has a turret elevation limitation of -2/+80 degrees. The HN-5C is operated by a two-man crew and has a maximum effective range of 13,779 ft. (4,200 m) between an altitude limits of 164 ft (50 m) and 7,545 ft (2,300 m). The maximum target speed is 492 ft/s (150 m/s) for head-on intercept and 853 ft/s (260 m/s) for tail-on engagement. It is available f or export; the current production status of this HN-5C is unreported.
System
Alternative Designations HN-5A; NATO: SA-3; Red Cherry 5; Red Cherry 5A
Target Rotary wing aircraft
Crew Can be fired by one however, a second crew member assists with identification of the target
Reaction Time <5 secs
Family HN-5
Dimensions
Weight 16 kg
Length 1.44 m
Diameter 72 mm
Armament (Missile)
Engine 1 x 2-stage solid-propellant rocket
Max Speed Mach 1.5
Maximum Slant Range 4.4 km
Minimum Slant Range 800 m
Maximum Altitude 2,300 m
Minimum Altitude 80 m
Maximum Target Speed (Head On) 550 kph
Maximum Target Speed (Tail Chase) 950 kph
Warhead HE / Frag
Counter-Counter Measures Missile has a filter to reduce chances of missile being diverted by flares
Details
Country of Origin China
Category Man-Portable Air-Defense Systems (MANPADS)
Land > Air Defense > Man-Portable Air-Defense Systems (MANPADS)
Filter Label
H
Classification
Domain
Ground
Equipment Status
Active
Dimensions
Length
1.44 m
Width
0.07 m
Height
Weight
16 kg
Operators (9)
China
North Korea
Pakistan
Afghanistan
Albania
Bangladesh
Burkina Faso
Cambodia
Thailand
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