Event

活動資訊

2025-09-20
學習教育

2025航太展參展

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2025台北航太展

南港一館 太空產業與技術區 K0416

教師 展品名稱 展品說明
張起維 深太空輻射探測儀(Deep Space Radiation Probe)(DSRP) 中大的「深太空輻射探測儀」是台灣第一個探月酬載,已與民間登月公司 ispace 的 Resilience 登月小艇整合,並於 2025/1/15 發射,順利在為期五個月的任務期間探測地球到月球軌道、月球軌道以及月球表面的游離輻射劑量、劑量率、以及單位元翻轉次數,以利後續太空電子及載人太空任務發展。The NCU Deep Space Radiation Probe (DSRP) is Taiwan's first lunar payload and has been integrated with the ispace Resilience lunar lander that was launched on 2025/1/15. During the 5 month mission, DSRP successfully measured the ionizing radiation dose, dose rate, and single event upset rate between the Earth and the Moon, which will benefit the future development of space electronics and crewed missions.
林映岑 星載微型軟體定義無線電收發機(MSDR for CubeSats) 微型軟體定義無線電(MSDR)為一輕巧多功能的衛星通訊酬載,它可被整合致力方衛星上以實現高數據速率傳輸,也可透過程式編寫更改訊號處理方式,執行自適應編碼和調變。The Miniature Software-Defined Radio (MSDR) is a compact communication payload that can be integrated into CubeSats for hight data-rate transmission. It is a versatile device that can also perform adaptive code and modulation.
  小型可攜式GNSS接收機( NavPod) 此系統整合商用接收機晶片與樹梅派小型電腦,採用POE供應系統用電和網路,並具備自動接收及上傳資料的功能,小巧體積及設置的便利性使實驗數據的蒐集更加便利。 NavPod: Compact Portable GNSS Receiver
This receiver system integrates a commercial GNSS receiver chip with a Raspberry Pi single board computer. It uses Power over Ethernet (PoE) for both power supply and network connectivity and features automatic data acquisition and uploading. Its compact size and ease of deployment make the collection of GNSS experimental data much more convenient.
  DIY全天景相機( DIY all-sky camera) 全天景相機使用魚眼鏡頭與 CMOS 模組對整個天空進行拍攝,同時內部的單板電腦可自定義相機參數與拍攝時間並將數據儲存且同步上傳。The all-sky camera uses a fisheye lens and CMOS module to capture the entire sky. The internal single-board computer allows for customizing camera parameters and shooting times, also storing and uploading data.
許藝瓊 微重力系統(Microgravity System) 系統特色:
1.模擬微重力環境(零重力與月球火星重力),採用雙軸360°旋轉技術,重現類太空站(10⁻³ G)條件,實現重力全方位均勻抵銷。
2.超重力環境模擬,透過單軸離心力裝置,模擬2~3G的加速條件,重現火箭發射等極端狀況。
3.重力變化即時監測,內建感測模組,可即時偵測與紀錄實驗中產生的重力變化與動態數據。
4.模擬特殊製程條件,推動高階材料開發。
5.支援衛星與太空艙內部生物模組設計。1.Microgravity Simulation (Zero-G, Lunar, and Martian Gravity)
Equipped with dual-axis 360° rotational technology, the system replicates space station–like conditions (10⁻³ G) by achieving uniform gravity offset across all orientations.
2. Hypergravity Environment Simulation
Utilizes a single-axis centrifugal system to simulate 2–3 G acceleration, enabling reproduction of extreme conditions such as rocket launch dynamics.
3.Real-Time Gravity Variation Monitoring
Intergrated sensor modules allow for continuous detection and recording or gravity changes and dynamic data during experiments.
4.Suooprt for Specialized Manufacturing Conditions
Enables simulation of unique microgravity or hypergravity processes to accelenrate the development of advanced materials.
5.Compatible with Satellite and Space Capsule Biolab Modules
Designed to support biological module intergration for use in satellite payloads or onboard space habititats.
陳彥宏 低軌立方衛星量子光通訊模組(Low-orbit CubeSat Quantum Optical Communication Modules) 全自製量子光通訊光源模組,特點如下:
積體晶片材料: 週期性晶疇極化反轉鈮酸鋰波導。
光子對產生機制: 自發參量下轉換。
光子對產生率: ~107 Hz。
可達成糾纏維度: 偏振、時間、頻率、模態。
Integrated quantum light sources for quantum communications, by NCU:
Substrate: PPLN waveguides.
Photon pair generation: spontaneous parametric down conversion.
Photon pair generation rate: ~107 Hz.
Entanglement dimension: polarization, time, frequency, spatial modes.
張貴雲 星載機密運算平台(Confidential Computing Satellite,CC-Sat) 系統特色: 星載機密運算平台可被整合於衛星以提供多租戶衛星機密運算服務、GPU資訊安全防護,目前有二款可供選擇。 CC-Sat can be integrated into satellites to provide multi-tenant satellite confidential computing services and GPU information security protection.
郭政靈 1U 立方衛星飛行版衛星電腦板
1U 立方衛星飛行版電力系統板
1U 立方衛星教育版
1U 立方衛星教育版地面站

本展示品為由大學自主設計與整合的1U立方衛星飛行版本,旨在運用大學資源製作於近地軌道上之立方衛星。
具備指令與資料處理、姿態控制、通訊系統及電源管理等基本任務功能。透過成本控管與模組化設計,培養與傳承立方衛星設計與系統整合能力之基礎,並可以此為基礎延伸至較高複雜度之衛星系統。

This exhibit showcases a 1U CubeSat flight model independently designed and integrated by the university. It is intended to leverage university resources for the development of a CubeSat capable of operating in low Earth orbit (LEO).
The system includes essential subsystems such as Command and Data Handling (C&DH), Attitude Determination and Control System (ADCS), Communication (COM), and Electrical Power System (EPS). Through cost control and modular design, this project serves as a foundation for cultivating and passing down the knowledge and capabilities required for CubeSat design and system integration, with potential to scale toward more complex satellite systems.

 
 

 

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