KNACKSAT * : A Thai Educational Satellite

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Transcription:

KNACKSAT * : A Thai Educational Satellite Suwat Kuntanapreeda, Pongsatorn Saisutjarit, Suramate Chalermwisutkul King Mongkut s University of Technology North Bangkok (KMUTNB) Bangkok, Thailand *KNACKSAT: KMUTNB Academic Challenge of Knowledge SATellite

History KNACKSAT Introduction Missions Requirements Subsystems Integration Test Etc. Outline

History ThaiSat, 1988. Proposed by Dr. Suthee Aksornkit http://www.thaiscience.info/journals/article/tjkm/10469766.pdf

History ThaiCom 1, 1993 (Note. The latest one is ThaiCom 8) Operated by Thaicom Public Company Limited http://www.thaicom.net

History TM-Sat (Thai Micro-SATellite) or Thaipat, 1998 Designed and developed by Mahanakorn University of Technology and University of Surrey http://www.space.mict.go.th/knowledge.php?id=thaipat

History SMMS (Small Multi-Mission Satellite), 2008 Joint project of China, Iran, Republic of Korea, Mongolia, Pakistan and Thailand. Kasetsart University involved in design and development of the Ka-Band communication subsystem. http://wwwku.ac.th/e magazine/jan52/it/engineers.htm

History THEOS (Thailand Earth Observation System) or Thaichote, 2008 Operated by Geo-Informatics and Space Technology Development Agency (GISTDA) http://www.gistda.or.th/main/th/node/90

History In 1998, King Mongkut s University of Technology North Bangkok (KMUTNB) started offering an undergraduate program in Aerospace Engineering. KMUTNB Satellite Attitude Dynamic and Control Simulator, 2000

History KMUTNB CanSat Project started in 2012.

History KMUTNB CubeSat Project started in 2012. First prototype 2012 BBM 2013 EM 2014 EM* 2015 * EM2015 is a joint project between KMUTNB and GISTDA.

History I wrote this article introducing CubeSat to Thai society 10 years ago. However, no attention was drawn at that time. http://www.space.mict.go.th/knowledge.php?id=cubesat

History We are not alone! Other CubeSat activities going on in Thailand include: JAISAT (Joint Academy for Intelligent Satellites for Amateur Radio of Thailand, The Radio Amateur Society of Thailand. SpaceBox, King Mongkut s Institute of Technology Ladkrabang (KMITL) and King Mongkut's University of Technology Thonburi (KMUTT) LESASAT, Learning Center for Earth Science and Astronomy

KNACKSAT: Introduction KNACKSAT is a 1U CubeSat satellite. (KmutNb Academic Challenge of Knowledge SATellite) 270k USD granted from NBTC Thailand in OCT 2015 (National Broadcasting and Telecommunications Commission) Fully in-house developed satellite in Thailand.

KNACKSAT: Missions Main Missions To acquire basic space technologies by demonstrating : Remote sensing technology (Earth Imaging) Active attitude control Communication via HAM radio

KNACKSAT: Requirements Satellite design requirements Modular design Size 10 x 10 x 10 cm Weight less than 1.33 kg Internal Bus : I2C interface Communication : GFSK 9600 and FSK 1200 bps Image size : QQVGA FULL HD

KNACKSAT: Subsystems 1. Structure Subsystem, STR 2. Communication Subsystem, COM 3. Electrical Power Subsystem, EPS 4. Command and Data Handling Subsystem, CDH 5. Attitude Determination and Control Subsystem, ADCS 6. Camera Subsystem (or Payload), CAM

KNACKSAT: Integration Test PC Command TableSat Model PC Monitor

KNACKSAT: Integration Test https://www3.nhk.or.jp/nhkworld/en/news/editors/1/thailandsaerospacehopes/

KNACKSAT: Engineering Model Ready for Environment Tests

KNACKSAT: How to get to this point? 5 + teaching staff 15 + students Many valuable supports from friends around the world

KNACKSAT: How to get to this point? Team Discussion

KNACKSAT: How to get to this point? Soldering and Inspection

KNACKSAT: How to get to this point? Software Development and Testing

KNACKSAT: How to get to this point? Ground Station Installation

KNACKSAT: How to get to this point? Preliminary Design Review Thanks to Mr. Masanobu Tsuji, Prof. Shinichi Nakamura and Prof. Shinichi Nakasuka

KNACKSAT: Future Works Environment testing (27 Feb 7 March 2017, Center for Nanosatellite Testing Laboratory of Spacecraft Environment Interaction Engineering, Kyushu Institute of Technology ) Critical Design Review (CDR) Flight Model (FM) Fabrication Software Fine Testing and Validation Launch (550-600km, SSO, Q4/2017) Ground Operation and Control

Thank you For your attention