The results of Small Satellite technology transfer from JAXA
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1 The results of Small Satellite technology transfer from JAXA Hiroaki Kawara, Naomi Murakami, Yuuta Horikawa, Koji Nakaya, Keiichi Hirako, Hidekazu Hashimoto Japan Aerospace Exploration Agency (JAXA) 24 th ANNUAL CONFERENCE ON SMALL SATELLITES
2 Table of contents Back Ground of Technology Transfer Program Satellite Overview and Objectives On-Orbits Technology Transfer Conclusion
3 Background of SOHLA In Japan, SMEs and universities associate to develop small satellites At Osaka area SOHLA, established in 2003: Space Oriented Higashiosaka Leading Association Object of SOHLA is to develop a small satellites and their commercialization at a low cost SOHLA Osaka JAXA JAXA is required by public to spread our accumulated space technologies to industries and universities
4 JAXA s Tech. Transfer Program Ryukoku Univ. Kinki Univ. Space Technology Transfer Program Osaka Prefecture Univ. System design and analysis SOHLA-1 Satellite Integration Univ. of Tokyo, Osaka Univ. Experimental Components JAXA micro satellite technology SME SME SME SME Component Manufacturing Space systems engineering System design and analysis Space components development System integration and testing Satellite operation General ideas under space environment Quality management Satellite integration and testing techniques System management and interface control Mission analysis Power management analysis Attitude control analysis Structure and thermal analysis Selection of materials and electrical parts High reliability micro soldering techniques Component manufacturing techniques Etc
5 Difference of purpose towarads space. Main member of SOHLA To Cheer-Up Higashi-Osaka Area, whose main industry is decline. Satellite development is the one of its ways. Member of JAXA To spread space technologies to industries and universities Satellite development is the main way to achieve the JAXA s goal.
6 Satellite objective? SOHLA To complete satellite development Launch Satellite to space JAXA Transfer technology to SMES and Univercity, through satellite development To complete satellite development in peace SME & Univercity To develop satellite components and to be operate on the space.
7 Satellite Overview(named MAIDO) Item Size Weight Power Attitude Control Orbit Comm. Specifications Octagonal prism (500 x 500 x 500) Approx. 50 kg over 30 W Spin stabilized SSO S-band/Amateur band Spin rate : 3rpm TSA :0-85deg, deg Solar cells are placed on the surface of MAIDO to generate enough electric power.
8 MAIDO System Block Diagram
9 On-orbit Demonstration 8 experiments in 50kg class micro satellite 1. COTS based small GPS receiver demonstration (JAXA) 2. High accuracy geomagnetic observation and on-orbit radiation monitoring (JAXA) 3. Deployable boom demonstration (Ryukoku Univ.) 4. Small monitor camera demonstration (SOHLA/JAXA) 5. Sun sensor demonstration (Osaka Prefecture Univ.) 6. For thunderstorm observation, demonstration of component for broadband measurement of waveform for VHF lightning impulses (Osaka Univ.) 7. CIGS solar cells demonstration experiment (JAXA) 8. Demonstration of 64bit MPU with 200 MIPS level (JAXA)
10 Thunderstorm Observation Ground System(in-service) Space system (planed) Direction estimation using phase difference of radio waves Data record Universities plans to develop a component to observe thunderstorm from low Earth orbit using small satellites
11 Broadband Measurement for Waveforms of VHF Lightning Impulses (BMW) Osaka university develops a component to measure VHF broadband waveform of lightning impulses. Functional verification of BMW in space Understanding features of VHF radio wave from thunderstorms BMW Antenna for BMW
12 Launch of MAIDO Tanegashima Space Center Jan. 23, H-IIA Lift off! GOSAT MAIDO SDS-1 MAIDO was successfully launched as one of the seven piggyback satellites with GOSAT (Green-house gasses observation satellite) on January 23rd 2009 with H-2A LV. June 3, S Symposium, Madeira 12
13 Launch of MAIDO MAIDO From GOSAT (Primary payload) monitor camera
14 Satellite operation /1/23 MAIDO Satellite Operation Events Launch up Separation, 1st AOS picture of Japanese Islands 2009/1/24 Critical phase EPS check out ACS check out Nutation dump Spin Axis Control Spin Rate Control 2009/1/ /2/ /2/ /2/ /2/ /2/15 Critical phase GPSR check out Moniter camera get pictures from space Radiation monitor check out BMW antenna deployment BMW detects the thunder storm from space GPSR continuous operating test BMW catch a thunder storm 2009/2/23 H-band antenna deployment
15 Satellite Operation /2/ /2/ /3/ /3/23 BMW experiments GPSR+SLR (To estimate orbit determination accuracy) BMW experiments 2009/4/ /4/09 AMI continuous operating 2009/4/ /4/17 Boom deployment test 2009/4/ /4/25 Moniter cmaera get pictures 2009/5/ /5/ /10/10 MAIDO FINAL Operation Nominal phase MAIDO Satellite Operation Events Boom Deployment results Send a power down command
16 Mission Experiments Results Mission Orbit determination technology demonstration radiation monitoring CIGS solar cells 64bit MPU Advanced Micro processing In-orbit experiment (AMI) Moniter Camera Deployable Boom Sun Sensor demonstration Broadband Measurement for Waveforms of VHF Lightning Impulses (BMW) Conducted operations and results All functions were working well. Radiation absorbed dose was measured with propriety Degradation of Si solar cell (reference) and thin-film solar cells are compared All parts were working well. -MPU is functioning in 50MIPS SEUs are observed MPU cache area. -Error detection and correction is also working well. All functions were working well. Use this camera, Deployable boom can be confirmed Function was working well All Functions were working well. All functions were working well.
17 Technology Transfer and its results Satellite main Structure On Board Computer Battery Moniter Camera All Components had been working well till final operation.
18 Example of Technology Spreading BMW Deveolping new BMW for ISS (International Space Station) Moniter Camera 3 Cameras in Space 1 Camera waiting for launch Developing advanced-moniter Camera high resolusion easily data handling action mode
19 Conclusion The Satellite program To complete satellite development Launch and operate satellite in successfully Technology transfer activity system analysis components
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