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Prithvi-II Missile

Prithvi-II Missile
  • Guidance System Strap-down Inertial Navigation System (INS) with maneuvering capability
  • Maximum Speed Supersonic (Mach 3+ terminal phase)
  • Launch Compatibility Mobile Transporter Erector Launcher (TEL), ground-based
  • Warhead Technology Conventional HE/fragmentation or nuclear-capable (up to 1,000 kg payload)

Full Specifications

1. General Information

Name / Designation Prithvi-II (SS-250)
Type / Role Short-Range Ballistic Missile (SRBM), Surface-to-Surface, Tactical Strike
Country of Origin India
Manufacturer DRDO (Defence Research and Development Organisation)
Service Entry / Year Introduced 2003
Operational Status Active

2. Performance & Range

Range 250โ€“350 km
Speed Supersonic
Ceiling / Altitude Limit ~43 km peak altitude
Accuracy (CEP) ~50 m (up to <10 m in upgraded variants)
Warhead Type High Explosive, Fragmentation, Nuclear-capable

3. Guidance & Targeting

Guidance System Strap-down INS with advanced navigation
Targeting Mode Pre-programmed ballistic trajectory
Launch Platform Compatibility Mobile Ground Launcher (TEL)
Seeker Type Inertial (no terminal seeker in standard configuration)

4. Physical Characteristics

Length 8.56 m
Diameter 1.1 m
Wingspan N/A (ballistic)
Launch Weight ~4,600 kg
Propulsion Single-stage liquid rocket

5. Warhead & Payload

Warhead Weight 500โ€“1,000 kg
Explosive Type HE / Nuclear
Detonation Mechanism Impact / Proximity
Payload Options Conventional or Nuclear

6. Operational Use & Capabilities

Operational Range Type Short
Deployment Platform Ground (Mobile)
Target Types Military installations, troop concentrations, infrastructure
Combat Proven No (extensive testing)
Users / Operators India (Strategic Forces Command, Indian Army/Air Force)

Our Rating

The overall rating is based on review by our experts

7.8
  • Technology 8 / 10
  • Performance 7 / 10
  • Maintenance Efficiency 8 / 10
  • Range & Endurance 8 / 10

PROS

  1. High mobility via road-mobile launchers for rapid repositioning and survivability.
  2. Proven nuclear and conventional payload flexibility supporting strategic deterrence.
  3. Reliable liquid propulsion with extensive flight testing history.
  4. Good accuracy for a short-range ballistic missile in its class.
  5. Indigenous development reduces reliance on foreign suppliers.

CONS

  1. Liquid fueling requires pre-launch preparation, limiting response time compared to solid-fuel alternatives.
  2. Relatively shorter range restricts deep-strike options against distant targets.
  3. Accuracy can degrade under operational conditions without satellite augmentation.
  4. Maintenance of liquid propellants poses logistical challenges in field deployments.
  5. Older technology base compared to modern solid-fuel or hypersonic systems.

Prithvi-II Missile: India’s Precision Short-Range Ballistic Weapon

The Prithvi-II stands as a cornerstone of India’s tactical ballistic missile arsenal, representing a significant achievement in indigenous defense technology. Developed as part of the Integrated Guided Missile Development Programme (IGMDP), this single-stage, liquid-fueled surface-to-surface missile provides rapid, accurate strike options against high-value targets. Designed primarily for the Indian Air Force and later adopted by the Army under the Strategic Forces Command, it enhances India’s credible minimum deterrence posture in a complex regional security environment.

Manufacturer

The Prithvi-II was developed by India’s Defence Research and Development Organisation (DRDO). Production involves collaboration with Indian defense public sector undertakings. It draws on liquid propulsion expertise refined through extensive testing since the mid-1990s.

Speed and Range

The missile achieves supersonic speeds, reaching a peak velocity consistent with short-range ballistic trajectories (typically exceeding Mach 3+ during re-entry phases in similar systems). Its operational range extends up to 350 km with a 500 kg payload, offering flexibility for shorter distances with heavier loads up to 1,000 kg. It follows a ballistic trajectory with a reported peak altitude around 43 km in maximum range tests.

Cost/Price

Exact unit costs are not publicly disclosed by the Indian government, but estimates for Prithvi-series missiles place it in the range of approximately $1.5–2 million per unit based on historical production data and comparative analyses. This reflects the economics of liquid-fueled systems with mobile launch capabilities.

The Prithvi-II features robust countermeasures against anti-ballistic missile defenses through trajectory maneuvering. It uses a strap-down inertial navigation system with upgrades for improved accuracy, reported at around 50 m CEP or better in enhanced variants. It is nuclear-capable and can carry conventional high-explosive or fragmentation warheads. Launched from mobile transporter-erector-launchers (TELs), it offers high mobility and rapid deployment. Inducted in 2003, it has undergone numerous successful user trials, including night tests, validating its reliability.

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