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Sky Bow
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The Sky Bow, or Tien Kung (Chinese: 天弓; pinyin: Tiān gōng), are a series of surface-to-air anti-ballistic missile and anti-aircraft defense systems developed by Taiwan's National Chung-Shan Institute of Science and Technology (NCSIST). Development of the TK-1 was completed in 1986 and this system is now retired. The TK-2 and TK-3 are in service with the Military of the Republic of China.[1] TK-4 is in development.
Development
[edit]Research into what became the Sky Bow project began after the United States ended bilateral relations with the Republic of China in 1979. Other names proposed by chief engineer Chen Chuan-hao for the project included Sky Horse (Pegasus) and Flying Horse. Upon formal approval of the project in October 1980, it became known as Sky Bow. Under the influence of aerospace engineer and rocket scientist Huang Hsiao-tsung the project expanded to include testing of ramjet motors. In 1981 the project received increased support from minister of defense Sung Chang-chih and was expanded into a general purpose air defense project benchmarked to the American Patriot and Soviet 2K12 Kub. Sung set a seven year deadline for the project. The first test flight in 1982 ended in failure as did other early test flights. Huang left the project in 1982 for an executive role at NCSIST.[2]
In 1984 Taiwan gained the cooperation of Raytheon and was allowed to examine semi-obsolete missiles in detail. NCSIST experts traveled to the United States studied the technology, but they were not allowed to ask any questions and quickly came to the conclusion that many of the missiles they had been allowed to examine were old and had been damaged while in storage.[3] Dedicated facilities needed to be constructed to support the development of the TK-1 including Taiwan's first hypersonic wind tunnel. In 1986 the 12th flight test ended in a successful intercept of a target aircraft, the system's first. The system was officially unveiled in 1986 at a large ceremony presided over by premier Yu Kuo-hua. Its designation it was given, Zhongzheng 100/Sky Bow 1, referred to its 100km range.[2]
Missiles initially used a semi-active radar homing seeker. A passive infrared homing terminal seeker was also developed as a secondary seeker for the TK-1, this was successfully tested against a HAWK missile target but was never put into production. NCSIST also developed a large multifunction, phased-array radar known as Chang Bai (long white) for use with the Tien Kung (Sky Bow) series surface-to-air missile systems with 120 degree coverage and a maximum range of 450 km. Two versions of the phased array radar exist, a towed trailer radar and fixed "hardened" radar sites.[4][5] The Chang Bai radar system is reported to be based on the Lockheed Martin's ADAR-HP (Air Defense Array Radar-High Power) design and operates in the 2–4 GHz range (S-band). At least seven systems were said to be in service in 2006.[4] The system performance specifications remain classified, but its effective detection range against a 1m2 target is reported to be around 400 km.[4]
There was also a mobile version of the phased array radar developed in the late 1990s which could provide all-round radar cover with four separate faces but with a much decreased detection range. This version only appeared in public once but was never put into service. The development of Sky Bow 2 started around 1986, this added a tandem boost motor and an active radar homing terminal seeker. Proposals were reported to develop Sky Bow 2 into a surface-to-surface missile; unconfirmed reports suggest that this missile is known as Tien Chi. Modifications have been developed for Sky Bow 2, changing it into a single-stage rocket and to provide it with a limited capability against shorter-range ballistic missiles; the first test firing against a ballistic missile target was reported in September 2008.[6] Seven batteries were in service in 2006.[4] In 2010 TK-1/2 SAMs were in service and deployed throughout Taiwan, on the Pescadores, and Dong Ying island.[7]
Chen claims that the Sky Bow I project was completed in less time and using less money than any comparable air defense system. The project was NCSIST's first ambitious weapons project and its success would have a large influence on the organization.[2]
Sky Bow I
[edit]
The Sky Bow I (TK-1) (天弓一, Tien Kung I) is a surface-to-air missile (SAM) system developed by the NCSIST in Taiwan. Originally based on the aerodynamics of the MIM-23 Hawk missile, the original missile design resembled a scaled-up Raytheon AIM-54 Phoenix.[8] The TK-1 missile was subsequently redesigned and eventually became very similar in appearance to the US Patriot missile after the US government allowed Raytheon to transfer 85 percent of the MIM-104 Patriot missile technology.[8] There is no track-via-missile (TVM) homing capability as this technology was not included in the technology package licensed to Taiwan; the TK-1 system operates in a similar manner to the US Standard SM2 missile, requiring an illuminating radar during the terminal phase.[8]
The TK-1 is designed primarily to target low and medium altitude attacks. Each TK-1 battery has one Change Bai 1 (Long White 1) S-Band phased-array radar for search and target tracking and two CS/MPG-25[5] target illuminator radars that operates in the X-Band (18–32 GHz) range for the terminal phase, servicing three or four 4-round missile launchers.[8] The combination of inertial/autopilot and mid-course command guidance with a terminal semi-active radar seeker allows the TK-1 missile to fly an energy-efficient flight path to the vicinity of the target where the seeker's semi-active radar would then receive target illumination for the final seconds of the engagement, giving the target minimum amount of time either to evade or commence electronic countermeasure (ECM).[8]
Two versions of the missile launcher exist, one is housed in underground shelters designed to survive an intensive attack. The other is a towed mobile version, and is an integral part of Taiwan's dense air defense network. In addition to bases on Taiwan proper, the TK-1 has also been deployed by the ROC Army on the outlying islands of Penghu and Dong Ying, bringing all of the Taiwan Strait and parts of the PRC's Fujian, Zhejiang and Guangdong Provinces within range.[8]
It was reported in Jane's Missiles and Rockets, August 2006's issue, that the Tien Kung 1 surface-to-air missile (SAM) system would be retired. The TK-1 missiles would be replaced with TK-2 missile rounds and the existing TK-1 system would be upgraded with radar and training simulator to the Tien Kung II standard.[9]
CS/MPG-25 target illuminator radars
[edit]The CS/MPG-25 X-band target illuminator radar entered service in the late 1980s. It has a reported maximum range of 222km and a ceiling of 30,480m.[10] The CS/MPG-25 is a continuous wave disk antenna illuminator radar that was indigenously developed by NCSIST, and was derived from the I-HAWK AN/MPQ-46 High-Power Illuminator (HPI) radar but is estimated to be 60 percent more powerful in output with improved EW, ECM, and IFF capabilities.[8] It is tied into the main phased-array radar on a time-share basis similar to that employ by the US Navy's AEGIS air defence system, allowing the TK-1 surface-to-air missile system multiple target engagement capability.[4]
General characteristics
[edit]- Primary Function: surface-to-air missile
- Power Plant: Single-stage dual-thrust solid-fuel rocket motor
- Launch platform: Towed quad launchers and underground silos
- Length: 5.3 m[8]
- Diameter: 0.41 m[8]
- Weight: 915 kg[8]
- Top Speed: Mach 4.0[8]
- Range: 70 km
- Guidance: Inertial with mid-course guidance update from ground-based phased array radar, Semi-active radar homing (SARH) for terminal guidance
- Date Deployed: 1986
Sky Bow II
[edit]

The Sky Bow II (TK-2) (天弓二, Tien Kung II) is a SAM system also developed by the NCSIST. Originally a TK-1 with a first-stage booster, the system became a slightly-enlarged modified version of the Sky Bow I (TK-1) missile using an X-Band active-radar seeker,[11] with a longer range and limited anti-missile capability. The TK-2 active radar seeker operates in the 28–32 GHz frequency range and provides reasonably good performance against air-breathing targets of typical aircraft size. The X-Band active radar seeker used on the TK-2 SAM system was developed from licensed radar technology that NCSIST purchased from the U.S. in the 1980s.[11] The system uses the improved Change Bai 2 (Long White 2) multifunction radar which entered service in the late 1990s.[12] The first public test of the TK-2, codenamed Magic Arrow 43, occurred on May 10, 2002 during the Han kuang 18 exercise.[13]
The TK-2 also has the added benefit of being able to use the same box launcher as the TK-1. Internal components were replaced with miniaturized parts to take advantage of modern electronics technologies, yielding extra room within the missile for more fuel and a more powerful main rocket motor.[14] The TK-2 possesses only modest capabilities against ballistic missiles but is highly effective against aircraft.[13]
General characteristics
[edit]- Primary Function: surface-to-air missile
- Power Plant: Single-stage dual-thrust solid-fuel rocket motor
- Launch platform: Underground silos and mobile launch vehicles
- Length: 5.673 m[15]
- Diameter: 0.42 m[15]
- Weight: 1,135 kg[15]
- Top Speed: Mach 4.5[16]
- Warhead: 90 kg[16]
- Range: 150 km
- Guidance: Inertial with mid-course guidance update from ground-based phased array radar, Active radar homing (ARH) for terminal guidance
- Date Deployed: 1997
Variants
[edit]
Sky Spear
[edit]Sounding rocket
[edit]The TK-2 has also been modified for use as a sounding rocket to perform upper atmospheric research for the civilian space program.[18] The sounding rocket test vehicle launched on December 24, 2003, measures 7.7m in overall length and 1,680 kg in launch weight.[14] It reached a maximum altitude of almost 270 km and splashed 142 km down range around 8 minutes after launch into the Pacific.[19] The science mission payload was in the 220 pounds (100 kg) weight class and the rocket reached a burnout velocity of 2,000 m/s.[19] According to the report from Taiwan Defense Review, depending on its payload and launch parameters, the rocket can be converted to attain a horizontal maximum range of up to 500 km.[19]
| Mission | Date | Payload | Result |
|---|---|---|---|
| SR-I | 15 December 1998 | None | Successful first test flight[20] |
| SR-II | 24 October 2001 | Tri-Methyl Aluminum (TMA) release experiment | Second stage ignition failure, mission lost[20] |
| SR-III | 24 December 2003 | Tri-Methyl Aluminum (TMA) | Mission successful[20] |
| SR-IV | 14 December 2004 | Airglow photometer, GPS receiver | Mission successful[20] |
| SR-V | 15 January 2006 | Ion probe, 3-axis magnetometer | Mission successful[20] |
| SR-VI | 13 September 2007 | Hydrazine-fueled reaction control system, recovery capsule | Mission successful, capsule lost in the sea due to bad weather conditions[20] |
| SR-VII | 10 May 2010 | Ion probe | Mission successful[20][21] |
| SR-VIII | 5 June 2013 | Hydrogen peroxide reaction control system, recovery capsule | Mission successful[22] |
| SR-IX | 26 March 2014 | Ion probe | Mission successful[22] |
| SR-X | 7 October 2014 | Ion probe | Mission successful[22] |
Sky Bow III
[edit]



Sky Bow III (TK-3) (天弓三, Tien Kung III) is the third generation of the missile system. Taiwan had initially sought and even proposed a joint development effort to co-produce a missile defense interceptor with the U.S.[23] Taiwan officials asked for U.S. technical support for Taiwan's indigenous anti-tactical ballistic missile (ATBM) effort, including the transfer of Hit-to-Kill (HTK) technologies, specifically those related to an active radar Ka-band seeker and precision attitude control. NCSIST was reported to had sought the release of the associated traveling-wave tube (TWT) transmitter of the Ka-band active radar seeker technology. However, U.S. refusal of the export release of a complete Ka-band active radar seeker without tamper protection or to provide the TWT on a stand-alone basis forced NCSIST to use a different active radar seeker technology with a little European content.[24]
The TK-3 (formerly known as TK-2 ATBM) was conceived as a lower-tier missile defense system based on the TK-2 missile that uses an imported Ku-Band (12–18 GHz) active radar seeker, a directed fragmentation warhead,[24] and improved precision controls for engaging high-speed, low radar cross-section (RCS) targets such as tactical ballistic missiles.[25] It is designed with greater mobility in mind than the original TK-1/2 systems, with an integrated battle management system, and uses an upgraded Chang Bai phased array radar or with the new mobile phased-array radar that is reportedly called the Mobile 3-Dimensional (3D) Air Defense Fire Control Phased Array Radar (Mobile 3D ADFCPAR).[4]
The new mobile radar reportedly called Chang-Shan ("Long Mountain") radar system, like the Patriot's Raytheon AN/MPQ-65 radar system, is reported to operate on the C-Band (4–8 GHz) frequency range, and like the AN/MPQ-65 system, it is trailer-mounted with a rectangular planar array radar of approximately similar size. However, it does not appear to have any identifiable missile guidance sub-array like those found below the main array on the AN/MPQ-65 system and it is therefore not clear if this new radar can provide target guidance illumination function in support of TK-1 SARH missiles. However, this should not present any problem for the new radar to be utilized on both TK-2 missile (X-Band) and TK-3 missile (Ku-Band) active radar seekers, as these missile systems do not require target illumination. The new radar enhances the survivability and operational flexibility of the TK2/3 missile systems by allowing a TK surface-air-missile battery to be deployed rapidly to a previously unprepared site.[4] The TK-3 incorporates advanced ceramics and carbon fiber in its construction. The missile's nose cone can resist temperatures in excess of 1,000 °C.[3] The TK-3 is capable of both midcourse and terminal defense against ballistic missiles.[26]
Production of the Tien Kung 3 SAM commenced in 2014 with an initial production run of 12 batteries.[27] With the retirement of the HAWK batteries and the Sky Bow II becoming more obsolete, another twelve batteries of Sky Bow IIIs were ordered to replace these older systems. Conversion of six older batteries to Sky Bow IIIs began in 2022 and is to be completed by 2025. Work on the remaining six batteries began in early 2023 and is to be completed by 2026.[28] Previously, the United States had given Taiwan the options of upgrading the Hawk, buying the NASAMS system, and/or buying the THAAD missile system to replace their Hawks. The Ministry of National Defense ultimately decided to pursue the development of indigenous weapons to meet the need.[29]
In 2019 Taiwanese President Tsai Ing-wen ordered the NCSIST to accelerate mass production of the TK-3 in response to increasing Chinese military power and bellicosity.[30] In response to President Tsai’s request NCSIST completed their quota for TK-3 missile production ahead of schedule in 2021.[31]
In 2023 the Taiwanese MOD announced plans to build twelve new bases to host TK-3 batteries, six expected to complete before the end of 2025 and six more expected to complete before the end of 2026.[32]
Variants
[edit]In late 2016, NCSIST launched a ship-based variant of the Sky Bow III BMD interceptor. According to NCSIST, the test was conducted from a land-based launcher and "was successful and the data was satisfactory".[33] The ship-based version has a folding tail to fit in Mark 41 vertical launch system or Huayang Vertical Launching System and is planned to be deployed on the ROCN's next-generation general-purpose frigates and air defense destroyers as well as possibly retrofitted onto existing vessels.[34]
General characteristics
[edit]- Primary Function: surface-to-air missile
- Power Plant: Solid-fuel rocket motor
- Launch platform: Towed quad launchers
- Length: 5.498 m[8]
- Diameter: 0.4 m[8]
- Weight: 870 kg[8]
- Top Speed: Mach 7.0[8][35]
- Range: 200 km[36]
Export
[edit]The TK-3 has seen interest from foreign buyers but as of November 2019 none were confirmed.[3]
Sky Bow IV
[edit]
See also
[edit]- Sky Spear – (Taiwan)
- Sky Sword I/Antelope air defence system/Sea Oryx – (Taiwan)
- MIM-104 Patriot – (United States)
- Aster_(missile_family) – (France, Italy)
- Sayyad-2 – (Iran)
- Pongae-5 – (North Korea)
- KM-SAM – (South Korea)
- L-SAM – (South Korea)
- HQ-9 – (China)
- S-300 missile system – (Soviet Union, Russia)
- Defense industry of Taiwan
- Comparison of anti-ballistic missile systems
References
[edit]Notes
[edit]- ^ Everington, Keoni (2016-12-15). "Taiwan test fires Sky Bow air defense missiles amid tensions with Beijing". Taiwan News. Archived from the original on 2017-02-11. Retrieved 2017-02-10.
- ^ a b c Han Cheung (29 October 2023). "Taiwan in Time: The homegrown 'sky bow' project". Taipei Times. Retrieved 29 October 2023.
- ^ a b c Strong, Matthew (27 November 2019). "Foreign arms buyers show interest in Taiwan's Sky Bow III missile". www.taiwannews.com.tw. Taiwan News. Archived from the original on 3 December 2019. Retrieved 3 December 2019.
- ^ a b c d e f g Mei, Fu S. "Medium Range Air Defense Radar," Taiwan Defense Review, June 19, 2006.
- ^ a b "Tien Kung Weapon System" Archived 2011-07-22 at the Wayback Machine Chungshan Institute of Science and Technology
- ^ Mei, Fu S. "Taiwan Tests TK-2A ATBM," Taiwan Defense Review, September 18, 1998.
- ^ "The Balance of Air Power in the Taiwan Strait" Archived 2011-09-28 at the Wayback Machine US-Taiwan Business Council, May 2010.
- ^ a b c d e f g h i j k l m n o O'Halloran, James C. "Tien Kung I low-to-medium-altitude surface-to-air-missile system, pages 299-300," Jane's Land-Based Air Defense, 2002-2003 Edition.
- ^ Richardson, Doug "Taiwan switches from Tien Kung I to Tien Kung II," Jane's Missiles and Rockets, August, 2006.
- ^ "CS/MPG-25 (Sky Bow Illuminator)". cmano-db.com. CMANO. Archived from the original on 1 August 2019. Retrieved 1 August 2019.
- ^ a b Mei, Fu S. "CSIST Seeks New Seeker," Taiwan Defense Review, January 15, 2002.
- ^ "Long White 2 (Sky Bow 2 MFR)". cmano-db.com. CMANO. Archived from the original on 1 August 2019. Retrieved 1 August 2019.
- ^ a b "Taiwan: U.S. Ties Squeeze Missile Development". worldview.stratfor.com. STRATFOR. Archived from the original on 9 August 2019. Retrieved 8 August 2019.
- ^ a b Mei, Fu S. "Taiwan Forming Missile Command," Taiwan Defense Review, February 16, 2004.
- ^ a b c Fu S. Mei. "More Sounding Rocket Missions," Taiwan Defense Review, February 11, 2003.
- ^ a b O'Halloran, James C. "Tien Kung II, pages 298-299," Jane's Land-Based Air Defense, 2002-2003 Edition.
- ^ Minnick, Wendell: A better indigenous missile defense, Taipei Times, July 13, 2001.
- ^ Chern, Jeng-Shing; Wu, Bill; Chen, Yen-Sen; Wu, An-Ming (2012). "Suborbital and low-thermospheric experiments using sounding rockets in Taiwan". Acta Astronautica. 70: 159–164. doi:10.1016/j.actaastro.2011.07.030. ISSN 0094-5765.
- ^ a b c Mei, Fu S. "Satellite Prospects," Taiwan Defense Review, October 20, 2004.
- ^ a b c d e f g Chern, Jeng-Shing; Wu, Bill; Chen, Yen-Sen; Wu, An-Ming (2012). "Suborbital and low-thermospheric experiments using sounding rockets in Taiwan". Acta Astronautica. 70: 159–164. doi:10.1016/j.actaastro.2011.07.030. ISSN 0094-5765.
- ^ "美寶落格 MEPO Log - 文章在 週一, 五月 10. 2010". Mepopedia.com. Archived from the original on February 20, 2019. Retrieved August 1, 2017.
- ^ a b c McDowell, Jonathan C. (13 November 2024). "Launch List - By Family - NSPOB". www.planet4589.org. Retrieved 2024-11-14.
- ^ Stokes, Mark A. "Taiwan's Security - Beyond the Special Budget," Archived 2011-04-26 at the Wayback Machine American Enterprise Institute for Public Policy Research, March 2006.
- ^ a b Mei, Fu S. "Retaining Missile Defense Focus," Taiwan Defense Review, March 27, 2006.
- ^ Minnick, Wendell "Taiwan Proceeds on LACM," Defense News, September 15, 2008.
- ^ Freeman, Cameron (December 2019). "China's Next Generation Missile: The DF-17 in Pacific Conflict and Great Power Competition" (PDF). Institute for National Defense and Security Research. 8 (4): 35–54. Archived (PDF) from the original on 31 May 2021. Retrieved 17 February 2020.
- ^ 呂, 昭隆 (December 3, 2014). "國軍將採購12套天弓三飛彈". 中國時報. Archived from the original on May 28, 2022. Retrieved December 20, 2023.
- ^ "DEFENSE/Taiwan to build 12 new domestic TK III missile sites by 2026". Focus Taiwan CNA News. October 23, 2023. Archived from the original on November 2, 2023. Retrieved December 20, 2023.
- ^ Taiwan Retires Hawk Missiles - Defensenews.com, 15 September 2014
- ^ Wen Kuei-hsiang and, FLor Wang. "Taiwan president urges faster mass production of missiles". focustaiwan.tw. Focus Taiwan. Archived from the original on 18 May 2019. Retrieved 18 May 2019.
- ^ Chen, Kelvin (31 March 2021). "Sky Bow III missiles completed ahead of schedule: Taiwan's defense ministry". www.taiwannews.com.tw. Taiwan News. Archived from the original on 31 March 2021. Retrieved 30 May 2021.
- ^ Strong, Matthew. "Taiwan to station Sky Bow III missiles at 12 new bases". taiwannews.com.tw. Taiwan News. Retrieved 29 April 2024.
- ^ Taiwan's NCSIST Successfully Tested a Ship-based Variant of Tien Kung III BMD Interceptor Archived 2017-01-03 at the Wayback Machine - Navyrecognition.com, 2 January 2017
- ^ and Liao Yen-Fan, Michal Thim (25 March 2016). "Taiwan Navy Emphasizing Domestic Shipbuilding Program in Ongoing Maritime Restructure". news.usni.org. USNI. Archived from the original on 3 December 2019. Retrieved 3 December 2019.
- ^ "tw.news". 6 December 2018. Archived from the original on 2019-04-17. Retrieved 2019-04-17.
- ^ "Tien-Kung III (Sky Bow III) Surface-to-Air Missile System". Archived from the original on 2019-04-17. Retrieved 2019-04-17.
- ^ "國防產業發展條例列管軍品清單" (PDF). Ministry of National Defense official website. Archived from the original (PDF) on Feb 1, 2025. Retrieved July 30, 2024.
- ^ 羅添斌. "天弓四型飛彈傳115年度量產 攔截高度達70公里成為反飛彈最前線" [Tien Kung IV missile reportedly goes into mass production in 2015, interception altitude reaches 70 kilometers, becoming the forefront of anti-missile defense]. 自由時報電子報-軍武. Archived from the original on 2024-08-16. Retrieved 2024-08-16.
- ^ 劉宇捷. "台灣極機密飛彈有多少款?大盤點神秘雄昇、天弓四、雲峰一次看懂" [How many types of top-secret missiles does Taiwan have? A comprehensive review of the mysterious Xiongsheng, Tiangong IV, and Yunfeng]. 自由時報電子報-軍武. Archived from the original on 2024-08-16. Retrieved 2024-08-21.
External links
[edit]- Sky Bow I article on GlobalSecurity
- Sky Bow II article on GlobalSecurity
- Manufactures' videos [1][2][3]
Sky Bow
View on GrokipediaOrigins and Development
Initial Conception and Influences
The development of the Sky Bow (Tien Kung) surface-to-air missile system was conceived in response to Taiwan's shifting geopolitical and defense landscape following the United States' severance of diplomatic relations in 1979 and the subsequent 1982 "Six Assurances" and arms sales limitations, which underscored the need for indigenous capabilities to counter aerial threats from the People's Republic of China, estimated at around 4,000 MiG aircraft at the time.[10] In February 1980, engineer Chen Chuan-hao proposed a self-reliant missile design incorporating a ramjet engine for cost-effective airspace defense, securing approval from propulsion expert Huang Hsiao-tsung in coordination with the Ministry of National Defense.[10] The project formally commenced in October 1980 under the National Chung-Shan Institute of Science and Technology (NCSIST), aiming to produce a domestically engineered system within a compressed timeline.[10] Influences on the initial design drew from foreign benchmarks to inform performance goals, including the U.S. Patriot system's advanced guidance and the Soviet SA-6's mobility, while incorporating some imported overseas instrumentation for testing; however, the core aerodynamics were adapted from the U.S. MIM-23 Hawk missile, with the Sky Bow I prototype resembling a scaled-up version of the AIM-54 Phoenix in configuration to leverage proven semi-active radar homing principles.[10] [11] This hybrid approach prioritized empirical adaptations over direct replication, driven by Taiwan's expertise in wind tunnel testing and ramjet propulsion developed locally by figures like Chen and Huang, reflecting a first-principles emphasis on achieving interception ranges suitable for defending against massed low- to medium-altitude incursions without full dependence on embargo-prone foreign suppliers.[10] The program's rapid six-year cycle to operational readiness by late 1986 demonstrated the feasibility of indigenous innovation amid external constraints.[10]Early Prototypes and Testing (1980s–1990s)
The Sky Bow (Tien Kung) I program originated in October 1980 at the National Chung-Shan Institute of Science and Technology (NCSIST), following approval after consultations in February 1980, with the goal of developing a cost-effective surface-to-air missile to counter threats from Chinese MiG aircraft.[10] Initial prototypes adopted a wingless body design with four control fins powered by a ramjet engine, which was later modified to use a solid-propellant motor and large tail wings, bearing resemblance to the U.S. HAWK missile.[3] The first test flight occurred in 1982 but failed due to the missile sliding off the launcher, with subsequent early attempts also experiencing technical setbacks.[10] In the mid-1980s, NCSIST tested a Tien Kung I prototype fitted with an infrared seeker to explore alternative guidance options, though this configuration was not advanced to production in favor of semi-active radar homing.[3] A breakthrough came in March 1986, when the 12th test successfully intercepted a mock target aircraft, validating the system's capability after six years of development ahead of an initial seven-year timeline.[10] Designated Zhongzheng 100, the missile achieved a range of 100 km and was deemed operational by December 1986, enabling engagement of multiple targets.[10] Development of the Tien Kung II variant began in the late 1980s to extend range and improve performance, starting with prototypes that augmented the Tien Kung I airframe with a solid-propellant booster before evolving to a single-stage rocket motor and lighter structure.[3] Tien Kung I entered full deployment in 1993, supported by CS/MPG-25 illuminator radars and Chang Bai phased-array radar for semi-active homing at up to 70 km.[2] Tien Kung II progressed to batch production in 1997 after 1990s testing, incorporating active radar homing for 150 km engagements and deployment by 1998.[3][2]System Architecture
Radar and Guidance Systems
The Sky Bow surface-to-air missile system employs multifunction phased-array radars for target acquisition, tracking, and midcourse guidance across its variants, with the Chang Bai S-band radar serving as the primary search and acquisition component for Sky Bow I and II, offering detection ranges exceeding 300 km and capabilities for multiple target tracking, identification friend-or-foe (IFF) interrogation, and electronic counter-countermeasures (ECCM).[2][12] Sky Bow I relies on semi-active radar homing for terminal guidance, supported by two CS/MPG-25 X-band target illuminator radars to provide continuous illumination of incoming threats.[2] Sky Bow II introduces an X-band active radar seeker for autonomous terminal homing, reducing dependence on ground-based illumination and enhancing resistance to jamming, while retaining the Chang Bai radar for initial detection and midcourse updates via data links.[2] Sky Bow III features an upgraded Chang Bai or mobile Chang-Shan C-band phased-array radar with improved phase shifters for finer beam control, enabling tracking of low-radar-cross-section targets such as ballistic missiles; it integrates inertial navigation for midcourse phase with radar uplinks/downlinks for real-time corrections, transitioning to a Ku-band active radar seeker and microwave terminal seeker for precision intercept at hypersonic speeds.[2][4][1] These systems support networked operations through engagement control stations that handle threat evaluation, weapon assignment, and fire sequencing, allowing integration of Sky Bow I, II, and III missiles in mixed-mode searches for aircraft, cruise missiles, and tactical ballistic threats.[1] The phased-array radars provide simultaneous multi-target engagement, with ECCM features to counter electronic warfare, though operational effectiveness depends on terrain masking and integration with broader air defense networks.[4]Launch Platforms and Propulsion
The Sky Bow series employs various launch platforms tailored to its variants, transitioning from towed and fixed installations to more mobile vertical launch systems. Early models, such as Sky Bow I, utilize towed quad launchers capable of deploying four missiles, often integrated with underground silos for hardened protection at fixed sites.[13] Sky Bow II shares similar towed launchers with its predecessor but benefits from enhanced integration for rapid deployment.[2] In contrast, Sky Bow III features road-mobile vertical launchers, each containing four canisters compatible with both Sky Bow II and III missiles, enabling flexibility in response to dynamic threats.[1] [4] Propulsion across the Sky Bow family relies on solid-fuel rocket motors, providing reliable boost and maneuverability. Sky Bow I is powered by a single-stage dual-thrust solid propellant motor, optimizing initial acceleration and sustained flight.[13] Sky Bow II incorporates a second-stage solid propellant booster attached to the Sky Bow I airframe, extending range and velocity.[12] For Sky Bow III, a single-stage solid propellant system delivers hypersonic speeds and high specific impulse for rapid target engagement up to 200 km.[4] [1] These designs emphasize simplicity and storability, with vertical launch configurations in later variants reducing setup time and improving survivability.[2]Sky Bow I
Design and Specifications
The Sky Bow I, designated Tien Kung I, is a single-stage solid-propellant surface-to-air missile engineered by Taiwan's National Chung-Shan Institute of Science and Technology for medium-range air defense against aircraft incursions.[14] Its design emphasizes a wingless cylindrical fuselage with four rear-mounted control fins to facilitate aerodynamic stability and high-maneuverability intercepts.[3] The propulsion system utilizes a dual-thrust solid rocket motor, enabling rapid acceleration for engaging low- to medium-altitude targets.[13] Guidance employs semi-active radar homing in the terminal phase, with mid-course autopilot corrections directed by ground-based radar commands, supported by a multifunction phased-array radar for target acquisition and tracking, alongside a continuous wave illuminator for illumination.[3][14] The system incorporates electronic counter-countermeasures (ECCM) features to resist jamming, enhancing reliability in contested environments. Launch platforms include mobile quad-canister erector-launchers for tactical flexibility or hardened underground silos for strategic fixed-site defense.[3][14] Key specifications are as follows:| Parameter | Value |
|---|---|
| Launch Weight | 870 kg |
| Effective Range | 5–80 km (reports up to 100 km) |
| Interception Altitude | 0.03–23 km |
| Propulsion | Single-stage solid rocket motor |
| Guidance | Semi-active radar homing (terminal); command/radar correction (mid-course) |
Deployment and Phase-Out
The Sky Bow I (Tien Kung I) entered operational service with the Republic of China Air Force in 1993, representing Taiwan's initial indigenous long-range surface-to-air missile deployment.[2] The system's fixed-site batteries were integrated into the national air defense network, primarily for intercepting aircraft at ranges up to approximately 100 kilometers.[3] By 1996, Sky Bow I batteries had contributed to the full replacement of the obsolete U.S.-supplied Nike Hercules systems, enhancing Taiwan's layered air defense architecture with domestically produced assets.[3] At its peak, up to six battalions were operational, stationed at strategic locations including outlying islands such as Kinmen and Matsu.[16][13] As the more capable Sky Bow II variant achieved initial operational capability in the late 1990s, Taiwan initiated a transition away from Sky Bow I, with procurement and deployment shifting toward the upgraded model by the mid-2000s. This phase-out reflected improvements in range, guidance, and anti-ballistic potential in successors, though select Sky Bow I units persisted in reserve or supplementary roles into the 2020s to maintain defense depth amid evolving threats.[3]Sky Bow II
Improvements and Specifications
The Sky Bow II, designated Tien Kung II, featured a command active radar homing guidance system, replacing the semi-active homing of the Sky Bow I, which enabled terminal-phase autonomy without ground radar illumination.[2][3] This shift improved resistance to electronic countermeasures and allowed engagement of multiple targets more efficiently.[2] Structural modifications included a slightly enlarged airframe and a two-stage solid-fuel rocket motor, extending operational range beyond the Sky Bow I's maximum of approximately 100 km to reported figures of 150-160 km against aerodynamic targets.[3][12] The system integrated with the Chang Bai phased-array radar for target acquisition and mid-course guidance, providing a search range of up to 300 km.[12] Key specifications include a missile length of 9.1 meters, diameter of 0.57 meters, and launch weight of 1,100 kg.[12] Deployment occurred via fixed single-rail or silo launchers, optimized for static defense roles.[14] These enhancements positioned the Sky Bow II as a medium- to long-range surface-to-air capability suited for intercepting aircraft and cruise missiles.Variants and Adaptations
The Sky Bow II missile has been adapted primarily for enhanced anti-aircraft and limited anti-ballistic roles through modifications to its propulsion, warhead, and guidance systems. A key variant developed in the late 1990s focused on intercepting tactical ballistic missiles, featuring an enlarged solid-propellant booster for increased velocity and range, alongside a specialized kinetic or proximity-fused warhead optimized for high-speed targets.[12] This adaptation retained the active radar homing seeker of the baseline model but incorporated modifications for terminal-phase engagement of reentering projectiles.[18] In the fall of 1998, Taiwan conducted a successful live-fire test of this anti-missile interceptor variant against a ballistic missile surrogate, demonstrating its potential to counter short-range threats despite earlier technical challenges that had temporarily deferred such capabilities in 1997.[12][18] The test validated the variant's radar-guided acquisition and homing under realistic conditions, though operational deployment remained limited compared to the standard surface-to-air configuration, which prioritizes aircraft, cruise missiles, and anti-radiation threats.[2] Launch platform adaptations for Sky Bow II include both single-rail erector-launchers and silo-based vertical launch systems, with the latter integrated into fixed defense sites for rapid response and survivability.[19] By the early 2000s, several sites featured multi-canister vertical silos housing up to 20 rounds per battery, enabling cold-launch or hot-launch sequences compatible with the two-stage design.[3] More recent modernization efforts, initiated around 2022, have involved retrofitting select batteries with upgraded vertical launch infrastructure to extend service life and integrate with layered defenses, replacing older components while maintaining compatibility with existing Chang Bai radars.[20] These adaptations emphasize modularity, allowing phased upgrades without full system replacement.[19]Sky Bow III
Advanced Features and Specifications
The Sky Bow III missile system incorporates a vertically launched interceptor designed for both anti-aircraft and anti-ballistic missile roles, with a reported maximum engagement range of 200 km and altitude ceiling of 45 km.[7][4] The missile achieves hypersonic velocities to intercept high-speed threats, including ballistic missiles, enabling rapid response to incoming projectiles.[4] Central to the system's advanced capabilities is the Chang Bai (Long White) mobile phased-array radar, which supports simultaneous tracking of multiple targets and provides mid-course guidance updates to the missile via datalink.[21] This radar features electronic counter-countermeasures (ECCM) for jamming resistance, identification friend-or-foe (IFF) interrogation, and the ability to detect low-radar-cross-section targets such as stealth aircraft or ballistic warheads.[2][4] The launchers are compatible with both Sky Bow II and III missiles, allowing mixed-battery configurations for flexible deployment.[2] Guidance combines inertial navigation with command updates from the ground-based radar during the mid-course phase, transitioning to terminal-phase autonomy for precision intercept.[14] The system's fire control integrates automated threat evaluation and prioritization, supporting salvo launches against saturated attacks. Overall performance is stated to approximate that of the U.S. Patriot system in engagement envelope and reliability.[21]| Component | Key Specifications |
|---|---|
| Missile Range | Up to 200 km[4] |
| Maximum Altitude | 45 km[7] |
| Speed | Hypersonic (Mach 5+)[4] |
| Radar Type | Mobile phased-array with multi-target tracking[21][2] |