Dongfeng DF-4 vs Jericho
Dongfeng DF-4 vs Jericho at a glance — range 5,500 vs 6,500 km, speed 22,000 vs 20,000 km/h, warhead 2,190 vs 400 kg, launch weight 82,000 vs 6,500 kg.
| Dongfeng DF-4 | Jericho | |
|---|---|---|
| Origin | 🇨🇳 China | 🇮🇱 Israel |
| Category | Ballistic | Ballistic |
| Type | Intercontinental Ballistic Missile | Medium range ballistic missile |
| Manufacturer | Factory 211 (Capital Astronautics Co.) | IDF |
| Service year | 1975 | 2011 |
| Number produced | -- units | -- units |
| Estimated unit price | NA | NA |
| Range | 5,500.0 km | 6,500.0 km |
| Maximum speed | Mach 17.8 | Mach 16.2 |
| Weight | 82,000 kg | 6,500 kg |
| Warhead | 2190.0 kg | 400.0 kg |
| Length | 28.05 m | 13.40 m |
| Diameter | 2250 mm | 800 mm |
| Guidance | Astro-inertial guidance | Inertial with terminal guidance |
| Warhead type | Nuclear | TNT or nuclear |
Detailed Comparison
The Chinese Dongfeng DF-4 (CH-SS-3) and the Israeli Jericho series are primary nuclear delivery vectors for their respective operators. The DF-4 is a first-generation, liquid-fueled intermediate-to-intercontinental platform developed in the 1960s, while the Jericho represents an evolving family of solid-fueled missiles scaling from early medium-range ballistic missiles (MRBMs) to modern multi-stage systems.
Development and Design
Initiated in 1965 by Factory 211 to target United States bases in Guam, the DF-4 is a two-stage liquid-propellant missile utilizing nitric acid and unsymmetrical dimethylhydrazine (UDMH). This volatile fuel combination mandates a delayed pre-launch preparation phase. The Jericho program began in 1963 through a contract with French aerospace manufacturer Dassault. Following a 1968 arms embargo, Israel forced the program into domestic production. The Israelis immediately standardized on solid-propellant motors, sharing technical commonality with their Shavit space launch vehicle, eliminating the fueling delays that characterize the DF-4.
Performance and Capabilities
The DF-4 is an 82,000 kg system delivering a 2,190 kg, 3.3-megaton warhead (or three warheads in the DF-4A variant) out to 5,500 km at Mach 18.0. The baseline Jericho I weighed 6,500 kg, carrying a 400 kg warhead over a 500 km range at Mach 16.3. Later variants, specifically the Jericho II and III, scaled up to multi-stage designs capable of delivering high-explosive, fragmentation, or nuclear payloads at intermediate and intercontinental ranges. The 2011-era Jericho III incorporates multiple independently targetable reentry vehicles (MIRVs) to defeat ballistic missile defense systems.
Guidance and Technology
The DF-4 utilizes a 1970s-era astro-inertial guidance system yielding a 1.5 kilometer circular error probable (CEP). This low accuracy restricts the DF-4 exclusively to counter-value area targeting against cities or massive installations. The Jericho series utilizes inertial guidance, but later variants integrate active radar homing and terminal guidance. This terminal phase adjustment allows for high-precision counter-force targeting against hardened military sites.
Deployment and Combat Record
Neither missile has been fired in combat, but both dictate regional nuclear posturing. The PLARF deploys the DF-4 in underground silos or cave-based roll-out garages. Its lengthy liquid fueling process makes it highly vulnerable to preemptive strikes. The Israel Defense Forces deploy the Jericho deep in hardened facilities, notably Sdot Micha Airbase. During the 1973 Yom Kippur War, Jericho I missiles were armed with nuclear physics packages and placed on launch alert in response to ground losses. The Jericho II design saw export to South Africa as the licensed RSA series before Pretoria dismantled its nuclear program in 1994. Israel deploys the system across silos, road-mobile trucks, and rail cars.
Conclusion
The Jericho series holds a strict tactical and strategic edge over the DF-4. The DF-4's reliance on liquid UDMH propellant requires an operationally unviable launch sequence, rendering it vulnerable to first-strike destruction by modern precision munitions. Its 1.5 km CEP restricts it to a rigid counter-value role. The Jericho's solid-fuel architecture guarantees near-instantaneous launch authority, while its terminal radar guidance enables precision counter-force strikes. Israel’s system provides a survivable, rapid-response deterrent, whereas the DF-4 is an obsolete platform retained primarily for volume until the solid-fueled DF-31 completely absorbs its mission profile.