The AR176 is an Electronic Point Detonating fuze for artillery
rocket systems that is widely compatible with all calibers.
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ResheFuze AR176
Artillery Rocket Electronic Point Detonating Fuze
TECHNICAL SPECIFICATIONS
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COMPATIBILITY
With artillery rockets having high explosive (HE) warheads;
with calibers of 2.75”, 110mm - 300mm.
OPERATION MODES
N\A
TIME DELAY SETTING
N\A
SETTING SYSTEM
N\A
ACCURACY
N\A
POWER SUPPLY
Air driven (turbine) alternator.
ARMING
Arming of the fuze occurs only after two independent conditions
are sensed:
• Set back forces for a minimum duration.
• Sustained air flow through the fuze.
BACK-UP
N\A
FUZE INITIATION
N\A
SAFETY
Set-back: Acceleration of 20g minimum for a duration
of 1.2 seconds minimum.
Air Flow: 200m/s minimum.
Arming distance: 500m from muzzle, minimum.
Safety pull wire: There is no use of a safety pull wire.
HUMAN ENGINEERING
N\A
EXPLOSIVE OUTPUT
Booster pellet: 21g of CH-6.
TEMPERATURE LIMITS
Operation: From -40°c to +63°c
Storage: From -46°c to +71°c
PHYSICAL DESCRIPTION
Overall length: 183.5mm
Intrustion depth: 55.0mm
Cross section diameter: 64.0mm
Standard thread size: M45 x 2-6g
Weight: 0.82kg
Note: The dimensions given here are for the 122m rocket version.
MILITARY STANDARDS
MIL-STD-331: Environmental and performance tests for fuze
and fuze components.
MIL-STD-1316: Fuze design, safety criteria.
STANAG 4187: Fuzing system - safety design requirements.
HEIGHT OF BURST
N\A
IMMUNITY
N\A
POINT DETONATING
N\A
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