Generated by DeepSeek V3.2| Henschel Hs 293 | |
|---|---|
| Name | Henschel Hs 293 |
| Caption | An Hs 293 glide bomb on display. |
| Type | Air-to-surface missile |
| Origin | Nazi Germany |
| Service | 1943–1945 |
| Used by | Luftwaffe |
| Wars | World War II |
| Designer | Herbert A. Wagner |
| Manufacturer | Henschel |
| Variants | Hs 293A, B, C, D, V, W |
| Weight | 1,045 kg (2,304 lb) |
| Length | 3.82 m (12 ft 6 in) |
| Width | 3.10 m (10 ft 2 in) wingspan |
| Primary armament | 295 kg (650 lb) warhead |
| Engine | Walter HWK 109-507 liquid-fuel rocket |
| Engine power | 5.9 kN (1,300 lbf) for 10 seconds |
| Vehicle range | 12 km (7.5 mi) |
| Speed | 260 m/s (580 mph) |
| Guidance | Kehl-Straßburg MCLOS radio command |
Henschel Hs 293. The Henschel Hs 293 was a pioneering World War II-era German guided anti-ship missile, representing a significant technological leap in stand-off weaponry. Developed by Henschel under Professor Herbert A. Wagner, it was designed to be launched from medium bombers like the Heinkel He 111 and Dornier Do 217 to attack Allied shipping without exposing the aircraft to intense anti-aircraft warfare. Its operational use, primarily in the Mediterranean Sea and the Atlantic Ocean, marked one of the first successful combat deployments of a precision-guided munition against naval targets.
The development of the Hs 293 stemmed from pre-war experiments with remote-controlled glide bombs, notably the earlier Fritz X. Professor Herbert A. Wagner and his team at Henschel began work in 1940, focusing on a weapon that could be launched from beyond the range of a ship's defensive guns. The design utilized a standard SC 500 general-purpose bomb as its core, fitted with a lightweight alloy frame, wings, and a tail unit. For propulsion, it was equipped with a Walter HWK 109-507 liquid-fuel rocket motor slung beneath its fuselage, providing a short thrust phase after release. Guidance was achieved through the sophisticated Kehl-Straßburg radio command link, where an operator in the launching aircraft used a joystick to send control signals, visually tracking the missile's path via a bright flare in its tail. This MCLOS system required the pilot to maintain a steady course, making the aircraft vulnerable during the terminal attack phase, a critical tactical limitation.
The Hs 293 entered service with the Luftwaffe in mid-1943, with KG 100 being the primary operator. Its first major success occurred on August 25, 1943, when aircraft from II./KG 100 severely damaged the British sloop HMS Bideford and sank the corvette HMS Egret in the Bay of Biscay during the Battle of the Bay of Biscay. The weapon saw extensive use in the Mediterranean Sea, where it was deployed against Allied invasion forces during the Allied invasion of Sicily and the Allied invasion of Italy. Notable victims included the destroyer HMCS Athabaskan and the hospital ship HMHS Newfoundland, which was tragically sunk off the coast of Salerno. However, effective Allied countermeasures, particularly jamming of the Kehl-Straßburg radio frequencies and aggressive fighter aircraft patrols from carriers like HMS Chaser, increasingly degraded its effectiveness. By 1944, the threat had largely been neutralized, though sporadic attacks continued until the end of the war in Europe.
Several variants of the Hs 293 were developed to overcome operational shortcomings or to serve specialized roles. The basic **Hs 293A** was the initial production model. The **Hs 293B** was intended to use wire-guidance to avoid radio jamming, but it did not enter service. The **Hs 293C** featured a modified warhead for different target types, while the **Hs 293D** was an experimental television-guided version to improve accuracy. The **Hs 293V** series encompassed various test models used during development. Perhaps the most significant development was the **Hs 293W**, which was designed as an anti-aircraft warfare weapon, theoretically to be launched from ground installations or aircraft against United States Army Air Forces bomber formations, though it remained a prototype.
* **Length:** 3.82 m (12 ft 6 in) * **Wingspan:** 3.10 m (10 ft 2 in) * **Launch Weight:** 1,045 kg (2,304 lb) * **Warhead:** 295 kg (650 lb) TNT explosive * **Engine:** Walter HWK 109-507 liquid-fuel rocket * **Thrust:** 5.9 kN (1,300 lbf) for 10 seconds * **Maximum Speed:** Approximately 260 m/s (580 mph) * **Operational Range:** Up to 12 km (7.5 mi) from launch point * **Guidance System:** Kehl-Straßburg MCLOS radio command link * **Launch Platform:** Typically carried by Heinkel He 111, Dornier Do 217, and Focke-Wulf Fw 200 aircraft.
Category:World War II guided missiles of Germany Category:Anti-ship missiles of Germany Category:Henschel aircraft