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Hsiung Feng IIE

The Hsiung Feng IIE is a surface-to-surface land-attack cruise missile system developed by the National Chung-Shan Institute of Science and Technology (NCSIST) in Taiwan.

Development
According to the Taiwan Defense Review (TDR), the HF-2E land attack cruise missile is not a derivative of the Hsiung Feng 2 HF-2 anti-ship missile as it is often incorrectly reported. The use of the "HF-2E" designation is the primary cause of this confusion and was intentional misinformation done to divert attention away from the true nature of the project, which is that of a long range offensive cruise missile. The HF-2E is actually a completely different design and is said to serve a similar function in Taiwan's military as the US Navy's Tomahawk cruise missile. Its launch weight is reported to be in the range, including its solid rocket booster. It is essentially a tactical land attack cruise missile designed for use against military target sets, particularly air-defense fire units and command-and-control facilities, and its relatively small warhead size and the rather limited number of missiles planned for procurement clearly suggest that this is not a "first strike" weapon. The project was first announced in 2001. Following several test firings in 2004 and early 2005 at the Jiu Peng Missile Range in southeastern Taiwan, the baseline HF-2E (Block I) completed its operational evaluation (OPEVAL) in 2005, the missile flying a low-altitude circuit off Taiwan's southeastern coastline between Pingtung and Lanyu Island. An improved HF-2E missile was reportedly tested by CSIST at Jui Peng Missile Range on 2 February 2007. In 2017 the missiles received an extensive upgrade to increase their effectiveness against naval targets. ==Description==
Description
The baseline HF-2E Block I land attack cruise missile (LACM) is said to be powered by an indigenously-developed Taiwanese turbofan engine believed to be rated in the thrust range and developed by CSIST partially based on technology and experience from the Microturbo 078 turbojet engine used on Hsiung Feng 2 (HF-2) anti-ship cruise missiles. When equipped with a standard unitary high-explosive -class warhead, it is said to have a maximum range of 700 km. Other types of warhead are said to be in development, such as cluster submunitions and a hard target penetrator warhead. TDR also reported that through modification of the existing engine and combined with the redesign and reduction of the missile's control and electronic systems, CSIST was able to free up enough internal space/weight in the missile to allow it to carry additional fuel and extend its range to over 2,000 km, == Production and fielding ==
Production and fielding
The low-rate production of the Block I missile was to have started in July 2005 and using funds originally allocated for its R&D, at least five missiles were built. The unit cost per missile was estimated to be at US$3.08 million (2003 US$ dollar value). The HF-2E began low volume production in the Project ChiChun (戟隼, jǐ zhǔn, lance hawk). A Taipei Times news report claimed that President Ma Ying Jeou ordered the production of 500 to 1000 HF-2E missiles in 2008. It was approved and cleared to enter full volume/serial production in 2011. It supposedly can deliver a unitary warhead to a range of . The Associated Press has reported a range of 1,500 km. In 2022 annual combined production of the HF-2E and Hsiung Sheng was 81 units, the two missiles share a production line. In 2025 it was reported that the navy planned to upgrade the Kee Lung-class destroyers with HF-2E missiles. == Hsiung Sheng ==
Hsiung Sheng
The improved variant has been designated the Hsiung Sheng (). It is designed to be able to strike critical targets in distant Chinese cities like Wuhan and Qingdao. The Hsiung Sheng carries either a unitary or fragmentation warhead. ==General characteristics==
General characteristics
• Primary Function: Land-attack cruise missile • Power Plant: turbofan engine 1,500 km, and 2,000 km. • Top Speed: • Guidance: Inertial navigation system and commercial GPS with in-flight waypoints and corrected by terrain contour matching and forward-looking imaging infrared (IIR) seeker with automatic target recognition for terminal guidance • Launch Weight: including solid rocket booster • Accuracy: Within 10 m • Warhead: • Date deployed: Unknown ==See also==
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