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  • Publish Date:2026-08-26
NYCU Rocket Team Marks Two Milestones With Record Solid-Rocket Launch and Taiwan’s First Liquid-Propellant Rocket Flight
Members of the SST3 and FARCX-1 teams pose for a group photo. (Photo credit: TASA)
Members of the SST3 and FARCX-1 teams pose for a group photo. (Photo credit: TASA)
 
Edited by Chance Lai
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At daybreak on August 24, two very different rockets rose from Taiwan’s southern coast. The SST3 and FARCX-1 launches marked two major milestones for National Yang Ming Chiao Tung University (NYCU) and Taiwan’s emerging academic rocket program.

The SST3 was the largest solid-propellant rocket launched in Taiwan under a university-led project since the Taiwan Space Agency (TASA) began supporting collegiate rocket initiatives. The FARCX-1, meanwhile, demonstrated a locally developed liquid-propulsion system — a far more complex technology rarely attempted by student teams.

For the team, the twin launches were about more than sending rockets into the sky. They were a test of whether Taiwan’s university researchers and students could design, build and integrate two fundamentally different propulsion systems — and operate them in parallel.
 
The 3.5-meter-long SST3 soared to an altitude of 8.3 kilometers, becoming the largest solid-propellant sounding rocket launched in Taiwan to date by a university-led team. (Photo credit: TASA)
The 3.5-meter-long SST3 soared to an altitude of 8.3 kilometers, becoming the largest solid-propellant sounding rocket launched in Taiwan to date by a university-led team. (Photo credit: TASA)

SST3 Reaches 8.3 Kilometers and Sets a New Benchmark

The SST3 stood 3.5 meters tall and measured 16.3 centimeters in diameter. Its target was ambitious: 9 kilometers, roughly three times the altitude pursued in the team’s earlier test program. The rocket was developed to validate the performance and system specifications needed to compete in the 30,000-foot category of the Intercollegiate Rocket Engineering Competition (IREC) in the United States.

Earlier rockets in the SST series focused on flights in the 3-kilometer range. Reaching for 9 kilometers meant the team needed more thrust, longer burn time and stronger protection against heat and structural stress. At the heart of the upgraded rocket was the Pioneer-50K RNX, a solid-propellant propulsion system developed under the leadership of the Advanced Rocket Research Center (ARRC) at NYCU.

Although SST3 fell short of its 9-kilometer target, the flight represented a dramatic leap from the team’s earlier 3-kilometer tests and set a new record for a solid-rocket launch led by Taiwan’s academic community and conducted in the country. The rocket also successfully transmitted critical flight data to the ground. The flight data gave the team a detailed record of the rocket’s performance and will serve as a foundation for improving the recovery system ahead of future launches and international competitions.

For the students behind the rocket, the successful liftoff followed months of testing and redesign. “To withstand higher temperatures and sustain thrust for a longer period, we had to set much stricter thermal-protection requirements,” said Dan-Ying Cao, a first-year doctoral student in NYCU’s Department of Mechanical Engineering. “That meant conducting many more tests. Seeing the rocket lift off successfully made all that work worthwhile.”

The higher total impulse also placed greater stress on the rocket’s fins. “The structural strength of the fins became a major challenge,” said Yung-Ching Cheng, a second-year master’s student. “It was one of the areas where the team invested the most time and effort.”

One was built to fly higher than any comparable solid rocket launched by Taiwan’s academic community. It reached 8.3 kilometers. The other climbed only 532 meters. But altitude told just part of its story: It became the first rocket launched in Taiwan using a liquid-propellant system.

 

Both rockets were led by NYCU’s Institute of Space Systems Engineering (iSSE) and ARRC. Faculty members and students worked across every stage of development, from initial design and manufacturing to testing, systems integration and launch operations.

FARCX-1 Takes a Crucial Step toward Liquid Propulsion

The FARCX-1 measures 16.3 centimeters in diameter and 4 meters in length. Its primary mission was to validate the propulsion technology, rocket-system specifications and integration capabilities required for IREC’s Student Researched and Developed (SRAD) category. Unlike most student rockets, which use solid propellants, the FARCX-1 is equipped with a liquid-propellant system developed under the leadership of ARRC. The system uses high-concentration hydrogen peroxide as its oxidizer and kerosene as its fuel.

Liquid-propellant rockets require systems for fuel delivery, ignition, combustion control and multiple layers of safety protection. Their complexity and integration requirements are considerably greater than those of solid-propellant rockets. The FARCX-1 successfully lifted off, reached an altitude of 532 meters and transmitted critical flight data.

The launch achieved Taiwan’s first flight of a rocket powered by a liquid-propellant system. More than the completion of a single rocket, the achievement represents an important step for Taiwanese students and academic researchers developing liquid-propulsion technology independently. The results will provide a foundation for increasing thrust and flight altitude while improving system reliability in future missions.

Kao-San Lin, a fourth-year student in NYCU’s Department of Mechanical Engineering and a member of the FARCX-1 team, said building the liquid engine required the team to make the internal piping as compact as possible while carefully determining the location of each valve. “Every modification had to be followed by another ground test,” Lin said. “Altogether, we conducted five or six rounds of ground testing.”

Assistant Professor Shih-Sin Wei, who teaches NYCU’s Space Systems Integration course, said completing two rockets with different propulsion systems within a single semester was an enormous undertaking.

The 4.1-meter-long FARCX-1 reached an altitude of 532 meters, becoming Taiwan’s first student-developed liquid-propellant sounding rocket to successfully complete a flight test. (Photo credit: TASA)The 4.1-meter-long FARCX-1 reached an altitude of 532 meters, becoming Taiwan’s first student-developed liquid-propellant sounding rocket to successfully complete a flight test.

Building Experience for Future Competitions

As the Taiwan Cup Rocket Competition grows and its launch missions become increasingly complex, teams must do more than solve engineering and manufacturing problems. They must also use systems-engineering methods to coordinate technologies and resources across universities, academic disciplines and student teams — while, in this case, carrying out two fundamentally different launch missions at the same time.

NYCU hopes the technical demonstrations and results from the two launches will help teams competing in future Taiwan Cup and international rocket competitions build greater expertise in rocket design, propulsion, flight control and systems integration. The project is also expected to advance academic research on rockets in Taiwan and support the development of the country’s next generation of space-engineering professionals.
文/ARRC前瞻火箭研究中心、公關組
圖/國家太空中心、公關組


火箭再度升空!火箭團隊24日清晨在屏東旭海發射SST3「9公里挑戰組固態火箭」及FARCX-1「自製推進組液態火箭」。這是國內大專校院執行國家太空中心(TASA)計畫以來最大規模的固態火箭發射,也是國內首次採用液態火箭推進系統,寫下兩項重要里程碑。

這兩支火箭均由國立陽明交通大學太空系統工程研究所與ARRC前瞻火箭研究中心共同主導,從設計、製造、測試到系統整合,皆由師生團隊實際參與。此次任務不僅挑戰更高飛行高度,也同步驗證自製液態推進技術,展現國內學界在火箭研發與系統整合上的進展。

從3公里級驗證邁向9公里挑戰 SST3飛抵8.3公里

SST3固態火箭直徑16.3公分、全長3.5公尺,主要目標是驗證參加美國大專校際火箭工程競賽(Intercollegiate Rocket Engineering Competition, IREC)30,000英尺組別所需的火箭性能與系統規格。

SSTT火箭以3公里級火箭技術規格及系統驗證為重點,今年SST3則進一步挑戰9公里高度,推進系統也升級採用由前瞻火箭研究中心主導研製的Pioneer-50K RNX固態燃料推進系統。

本次SST3順利達到8.3公里飛行高度,較前一階段的3公里級驗證大幅提升,並成功回傳火箭飛行的關鍵數據。雖然降落傘未能依計畫開啟,團隊仍取得完整的重要飛行資料,可作為後續改善回收系統及參與國際競賽的重要依據。此次任務也創下由國內學界主導、並在國內執行的最大規模固態火箭發射紀錄。

SST3成員機械工程學系博士班一年級學生曹丹穎表示,為了使火箭能承受更高溫度、推進更久,他們為火箭定義更嚴苛的隔熱條件,也因此增加很多測試,很高興能看到火箭順利發射。碩士二年級的程永靖則說,為了挑戰更大總衝,尾翼的設計結構強度也面臨挑戰,團隊在這裡下了很多苦工。

FARCX-1首度升空 跨出液態火箭推進關鍵一步

另一支FARCX-1液態火箭直徑16.3公分、全長4公尺,主要任務是驗證參與IREC「學生自行研發推進系統組」(Student Researched and Developed, SRAD)所需的推進技術、火箭系統規格與整合能力。
 



不同於一般學生火箭採用的固態燃料,FARCX-1搭載由前瞻火箭研究中心主導研製的液態火箭推進系統,以高濃度雙氧水為氧化劑、煤油為燃料。液態火箭涉及燃料供應、點火、燃燒控制及各項安全機制,系統複雜度與整合難度均高於固態火箭。

本次FARCX-1順利升空,達到532公尺飛行高度,並成功回傳關鍵飛行數據,實現國內首次使用液態火箭推進系統的火箭發射目標。這不只是一支火箭完成,更代表國內學生及學研團隊跨出自主研發液態推進系統的重要一步,為後續提高推力、飛行高度及系統可靠度奠定基礎。

液態火箭FARCX-1團隊成員機械工程學系四年級林誥三則說,團隊在打造液態引擎的過程中,努力縮小管路及確認閥件的位置,每次修改都要進行地面測試,總計執行了五、六次地面測試。開設「太空系統整合」課程的魏世昕助理教授指出,要在一學期內完成兩支不同推進系統火箭的設計、製造、測試與發射,極具挑戰。

隨著台灣盃火箭競賽規模擴大、發射任務日益複雜,團隊除了克服工程設計與製造問題,也必須運用系統工程方法,整合跨校、跨領域及不同學生團隊的技術與資源,並同步執行兩項性質不同的發射任務。期盼此次表演組的技術示範與成果,能為未來參與台灣盃及國際火箭競賽的團隊累積更多火箭設計、推進、飛行控制與系統整合經驗,持續推動國內學界火箭研發與太空工程人才培育。

補充說明:
本次兩支火箭由陽明交大太空系統工程研究所與ARRC前瞻火箭研究中心共同主導,結合「太空系統整合」課程、前瞻火箭研究中心實習生及校內外學生火箭團隊,共同完成設計、製造、測試與系統整合。

  • SST3參與單位及團隊:陽明交大ARRC前瞻火箭研究中心、iSSE太空系統工程研究所、機械工程學系、ASARe Lab航太系統與流體力學實驗室,以及國立成功大學機械工程學系。
  • FARCX-1參與單位及團隊:陽明交大ARRC前瞻火箭研究中心、iSSE太空系統工程研究所、機械工程學系、Formosan Fox陽明交大學生火箭隊、國立中央大學AT Lab學生火箭團隊。