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Reference data current as of March 2026.

Specifications
Classification
Medium-Range Ballistic Missile (MRBM)
Range
1,350–1,950 km (variant-dependent)
Warhead
750 kg
Propulsion
Liquid-fuel, single stage
Guidance
Strap-down INS with GPS correction
CEP
~300 m
Launch Weight
17,000 kg
Length / Diameter
16.0 m / 1.25 m
Basing
Road-mobile (TEL)
Launch Prep
~30 minutes
Variants
Qadr S (1,350 km), Qadr H (1,650 km), Qadr F (1,950 km)
Est. Unit Cost
$200K–$350K
Description

The Ghadr family represents an incremental improvement over the baseline Shahab-3, achieved primarily through stretched fuel tanks that extend range and a distinctive "baby bottle" reentry vehicle nose cone. Multiple variants exist — Qadr S, Qadr H, and Qadr F — offering progressively longer ranges. The system uses strap-down inertial navigation with GPS/GLONASS midcourse corrections, achieving a CEP of approximately 300 m. Its MaRV capability allows limited terminal manoeuvring. First operational around 2007, the Ghadr has been a mainstay of IRGC Aerospace Force inventory for nearly two decades.

Key Features
  • Distinctive "baby bottle" reentry vehicle nose cone
  • 30-minute setup time — faster than the original Shahab-3
  • Road-mobile on wheeled TEL for rapid dispersal and survivability
  • GPS/GLONASS midcourse correction, vulnerable to GNSS denial
  • Multiple variants allow range optimisation for different target sets
Combat Use

The Ghadr's first confirmed combat use was in June 2025 during True Promise 3, where it was employed alongside other Shahab-3 derivatives and newer solid-fuel systems in massed salvo attacks against Israel. As a liquid-fuel missile, it requires longer launch preparation than solid-fuel alternatives like the Kheibar Shekan, making it more vulnerable to pre-emptive strike during fuelling.

Gallery
Sources

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