The Fattah-1 is Iran's first-generation hypersonic weapon, while the Fattah-2 represents a significant technological step forward by incorporating a true Hypersonic Glide Vehicle (HGV) that allows for far greater maneuverability and a more unpredictable flight path.
In other words, Fattah-2 is the more advanced, and more capable missile. Fattah-1 and Fattah-2 are probably Iran's most advanced publicly unveiled hypersonic-class missile systems.
Which is Better?
Depends on what is prioritized — penetration or destructive power. Fattah-1 has greater destructive force whereas Fattah-2 has superior ability to penetrate defenses.
| Feature | Fattah‑1 | Fattah‑2 |
|---|---|---|
| Unveiled | June 2023 | November 2023 |
| Type | MRBM with Maneuverable Reentry Vehicle (MaRV) — maneuvers only in the terminal phase | True Hypersonic Glide Vehicle (HGV) — sustained mid‑course + terminal maneuvering |
| Range | ~1,400 km | ~1,400–1,500 km |
| Speed (claimed) | Mach 13–15 | Mach 13–15 |
| Warhead | 500 kg — larger, heavier | 200 kg — smaller due to HGV mass constraints |
| Maneuverability | Limited — mostly last ~100 km before impact via thrust‑vectoring | Superior — continuous, unpredictable lateral & altitude changes throughout glide; harder to detect/track |
| Trajectory | Mostly ballistic; predictable until late reentry | Boost‑glide: flatter, lower, highly variable; can approach from unexpected directions |
| Propulsion (upper) | Solid‑fuel TVC motor in RV | Liquid‑fuel or aerodynamic HGV; sustains maneuvering |
| Precision (CEP) | ~10–25 m | Comparable or slightly improved |
| Cost / Complexity | Lower (~$0.8–1.5M) | Higher (~$1.5–3M) |
| Defense Penetration | Very good — but defenses can still model a ballistic‑style approach | Far superior — current air/anti‑missile systems (Arrow, Patriot, THAAD) struggle with HGV trajectories |
The key difference is how they maneuver.
Fattah-1:
It is essentially a ballistic missile with a maneuverable warhead. The warhead can change its trajectory, including with a small rocket motor. The International Institute for Strategic Studies classifies this type of system as a MaRV, rather than a true hypersonic glide vehicle.
Fattah-2:
Iran presented a substantially different second stage shaped more like a hypersonic glide vehicle. In principle, after being boosted upward, the glide vehicle can use aerodynamic lift to maneuver through the atmosphere rather than simply following the descending portion of a ballistic trajectory.
How Fattah Missile Works
The easiest way to understand it is that Fattah is not simply a missile that flies straight toward the target. Its important feature is the ability of the terminal vehicle to maneuver, making its final trajectory less predictable.
Fattah-1, step by step
Think of the flight in four stages:
1. Launch 🚀
A solid-fuel rocket booster launches Fattah upward at very high speed.
2. Boost phase
The main rocket accelerates the missile and gives it most of its speed. Once the booster has done its job, the propulsion configuration changes and the missile continues on its ballistic trajectory.
3. High-altitude flight
The missile travels on a trajectory that is broadly similar to other ballistic missiles: it goes high into the atmosphere and then begins descending toward the target.
4. Maneuvering terminal phase
This is the unusual part. The maneuverable reentry vehicle (MaRV) can use its own small propulsion system to alter its trajectory while approaching the target.
So rather than:
⬆️ → 🛰️ → ⬇️ → 🎯
it is more like:
⬆️ → 🛰️ → ↘️ ↗️ ↘️ → 🎯
The changes in direction make its final path harder for a defender to predict.
What about Fattah-2?
Fattah-2 is designed differently.
Its booster first accelerates the vehicle to very high speed. The second-stage vehicle is intended to behave more like a hypersonic glide vehicle (HGV):
🚀 Booster → high speed → glide vehicle separates → ↘️ maneuvering glide → 🎯
Instead of relying primarily on a predictable ballistic arc, the glide vehicle is intended to generate aerodynamic lift and maneuver inside the atmosphere.
That's why Fattah-2 is potentially more difficult to intercept than a conventional ballistic missile—but its publicly demonstrated operational capabilities are much less certain than the Iranian claims.
One important point
“Hypersonic” doesn't mean Fattah is necessarily faster than every other ballistic missile. Many conventional ballistic missiles already travel at hypersonic speeds during parts of their flight.
The important question is how the missile moves while traveling at those speeds:
- Conventional ballistic missile: mostly predictable ballistic trajectory.
- Fattah-1: ballistic trajectory + maneuverable terminal vehicle.
- Fattah-2: intended ballistic boost + maneuvering hypersonic glide vehicle.
That's the basic principle behind Fattah.
Fattah-1 has actually been used
Iran used it during the October 2024 attack on Israel, although the exact number of Fattah missiles and how many successfully reached their targets is uncertain.
Fattah-2 is a different story. There isn't good public evidence that Iran has used Fattah-2 operationally. Recent analysis specifically notes that Fattah-2 and Qassem Basir appear not to have been deployed, despite their much-publicized capabilities.
Fattah‑1 = MaRV (terminal maneuver only); Fattah‑2 = true HGV (mid‑course glide + full lateral maneuver). Both are often called "hypersonic" interchangeably in media, causing confusion.
The most widely cited Fattah‑1 successful impact is the Dimona nuclear site perimeter strike in early March 2026. Other reported hits include parts of the US Navy 5th Fleet support complex in Bahrain, Nevatim Airbase, and IDF headquarters area in Tel Aviv.
However — all these are primary claims from Iran, regional media, or sympathetic outlets. There is no official Western confirmation that these impacts were specifically Fattah‑1 rather than other Iranian ballistic missiles (Kheibar, Emad, Sejjil, etc.).
| Feature | Fattah‑2 (Iran) | DF‑17 (China) | LRHW Dark Eagle (US) | Kinzhal (Russia) | Zircon (Russia) |
|---|---|---|---|---|---|
| Category | Theater HGV | Theater HGV | Theater HGV | Air‑launched ballistic‑type | Scramjet cruise |
| Launch | Ground TEL | Ground TEL | Ground TEL | MiG‑31K / Tu‑22M | Ships / submarines |
| Range | 1,400–1,500 km | 1,800–2,500 km | ~2,775 km | ~1,500–2,000 km | ~900–1,000 km |
| Speed | Mach 13–15 | Mach 5–10 glide / Mach 15+ peak | Mach 8–12 glide / Mach 17 peak | Mach 9–12 | Mach 8–9 |
| Type | Boost‑glide HGV | Boost‑glide HGV | Boost‑glide HGV | Ballistic + terminal maneuver | Airbreathing scramjet |
| Warhead | ~200 kg conventional | 500–800 kg conv/nuclear | Conventional | Nuclear‑capable (~500 kg) | Nuclear/conventional |
| Maneuver | Mid‑course + terminal | Full glide, large lateral | Full glide | Terminal only | Continuous (lower altitude) |
| Status 2026 | Claimed operational | Operational (mass deployed) | Initial fielding | Operational since 2017 | Operational since 2023 |
| Primary Role | Regional strike ME | Pacific theater / anti‑ship | Global conventional deterrence | Quick‑strike / anti‑ship | Naval / coastal |
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