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MALAYSIA'S SPACE ACTIVITIES

MALAYSIA'S SPACE ACTIVITIES. OVERVIEW. Space Related Developments in Malaysia. 60’s:  First communication satellite receiving station established 1988:  Establishment of Malaysian Centre for Remote Sensing (MACRES) 1989:  First Planetarium in Malaysia (Kuching) officiated

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MALAYSIA'S SPACE ACTIVITIES

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  1. MALAYSIA'S SPACE ACTIVITIES OVERVIEW

  2. Space Related Developments in Malaysia • 60’s:  First communication satellite receiving station established • 1988:  Establishment of Malaysian Centre for Remote Sensing (MACRES) • 1989:  First Planetarium in Malaysia (Kuching) officiated • 1990:  JUPEM started using GPS for mapping • 1994:  National Planetarium officially opened • First professional astronomical observatory established in Malaysia (Terengganu) 1995 • 1995:  Initiation of National Microsatellite Programme • 1996:  Launch into space of MEASAT-1 and MEASAT-2 • 1997:  Cabinet approval of the MIGHT National Blueprint for the Development of the Malaysian Aerospace Industry • 1998:  First graduating batch of aerospace engineers from Universiti Putra Malaysia • 1998:  Malaysian Communication and Multimedia Commission established • 1999:  First Malaysian science payload launched onboard SunSAT

  3. Space Related Developments in Malaysia (cont.) • 2000:  Launch into space of microsatellite TiungSAT-1  Initiation of Medium-sized Aperture Camera (MAC) Programme  First graduating batch of BSc. (Remote Sensing) from Universiti Teknologi Malaysia • 2001:  Establishment of National Aerospace Council  Commencement of MACSAT Programme • 2002:  Establishment of National Space Agency (ANGKASA)  Cabinet approval for Near Equatorial Low Earth Orbit (NEqO) Satellite Constellation Programme  Commissioning of MACRES Ground Receiving Station • 2003:  MEASAT-3 Procurement Announcement  Announcement of National Astronaut Programme  Renaming of MACSAT to RazakSAT University Nanosat • 2004:  National Space Centre Commenced

  4. Space Related Developments in Malaysia (cont.) • 2005:  National Observatory Construction at Langkawi completed  Assembly, Integration and Test Facility commenced • 2006:  Launch of MEASAT-3  Feasibility studies for telecommunication satellite • 2007 :  Completion of feasibility studies for telecommunication satellite  Launch of Malaysia’s ANGKASAWAN

  5. OUTLINE • ANGKASA Overview • Division and Functions • Malaysia Space Centre • Micro-Satellite Program • Small Satellite Program • Research Satellite • Educational Satellite

  6. VISION To capitalize on space as a platform for enhancing the nation’s social, economic and strategic development. • MISSION • To enhance, stimulate and nurture the nation’s potential in the field of space through integrated and coordinated efforts in the development and application of space technology with a view to : • Providing a support system for solving national problems; • Adding value to national policies; • Promoting international cooperation; and • Advancing knowledge for the benefit of the people of Malaysia in particular and humankind in general.

  7. Divisons and Locations • Headquarters, Putrajaya (5th floor) • National Planetarium, Kuala Lumpur • National Observatory, Langkawi • Malaysia Space Centre, Banting

  8. MALAYSIA SPACE CENTRE • Development began towards the end of 2004.  • Situated in a 400 acre land in Sungai Lang, Banting, Selangor. • Development Phases: • Phase 1 – Mission Control Facility • Phase 1B – Optical Calibration Lab • Phase 2 – Quarters & Mes • Phase 3 – Satellite Technology Facilities

  9. Phase 1 – Mission Control Facility Satelit-satelit LEO & MEO RazakSAT TT & C X-band data X-BAND DATA RECEPTION TT&C Centre

  10. Phase 1B – Optical Calibration Lab

  11. Micro-Satellite Program TiungSAT-1 • NORAD TLE No: 26548U • Launch Date: 26th Sept 2000, 10:05 UT • Launch Site – Baikonor, Kazakhstan • Orbital Elements • Orbital inclination: 64.5 degree • Orbit type :LEO circular • Altitude: 650 km • Periods: 97 min

  12. Structure & Bus: • Weight : 50 kg (35kg platform, 15kg payloads) • Dim : 690 x 366 x 366 mm • ADCS : 3 axis stabilized (experimental) • Comms: Amateur Satellite Frequencies VHF/UHF • Payload: • CCD cameras (1 WAC and 3 NAC) • Cosmic ray Energy Deposition Experiment (CEDEX) • Digital Signal Processing Experiment (DSPE) • Mission Lifetime : 3 years

  13. TiungSAT-1 PayloadCCD cameras characteristics

  14. TiungSAT-1 Payload (cont) • CEDEX characteristics • characterize the TiungSat-1 orbit radiation environment in terms of the observed particle LET (Linear Energy Transfer) spectrum at the spacecraft. • Multi-channel analyzer with 512 channels and a 0.5 pC (pico-coulomb) charge resolution • DSPE characteristics • used for processing audio transmission for rebroadcast

  15. Image of Penang Island acquired from TiungSAT-1 on 6th April, 2001.

  16. Small Satellite ProgramRazakSAT™ • Structure & Bus: • Mass – 200 kg • Ø 1200 x 1200 mm hexagonal shape • ADCS: 3-axis stabilization based on 4 reaction wheels • Sun tracking system • Designed Life Time – 3 years

  17. RazakSAT™ Payload Characteristics: • Medium Aperture Camera (MAC) • GSD – 2.5m (PAN), 5m (Multi-Spectral) • PAN Band – 510-730 nm, MS Band - 450-520, 520-600, 630-690, 760-890 nm • Swath Width – 20km • Data Rate – 30 Mbps • Quantization – 8 bit • Mass Storage – 32 Gbit

  18. RazakSAT Orbital Location A Comparison Sun-synchronous orbit Altitude: 822 km Inclination: 98.7 deg TIUNGSAT Altitude: 650 km Inclination: 64 deg RAZAKSAT Near Equatorial Orbit Altitude: 685 km Inclination: 9 deg

  19. RazakSAT – Launch Vehicle Omelek Island, 9º2.890’N, 167º44.585’E Falcon-1

  20. Research SatelliteCubeSat • Pico-satellite • 10cm cubes, with mass <1kg • Using commercial off-the-shelf components • Typical lifetime: 6 months • Use of standard deployment system P-POD • Advantage • “Smaller, Cheaper, Faster, Better” • able to perform as a test bed for new systems and core space technologies to be applied to space programs

  21. INNOSAT • Also known as Innovative Satellite • Participation from Malaysia universities • Stack from 3U CubeSat kit • Some subsystem design & develop by universities, e.g. ADCS & power • Will be launched together with RazakSAT™

  22. Educational SatelliteSiswaSAT • Well known as CanSat. • Weighing 350 to 1050 g • CanSat is a simulation of a real satellite • Include most subsystems found in satellite • Simulate subsystem requirements of real satellite • All basic functions of a satellite, such as those of power and communications, are fitted into a soda can of 350 ml • Usually, CanSat launch as the payload in an amateur rocket up to altitude of 3000m and have their own recovery system; usually a parachute or parafoil that will allow a slow drift about 20 minutes.

  23. CanSat Sample

  24. Malaysia SiswaSAT competition • New initiative for national space educational programs • Provide entry level platform to undergraduate student in experiencing satellite development process • Development, launch and operation of SiswaSAT • Standard kit which only covers main subsystem will be provided; allow them to have flexibility and innovative idea in designing their SiswaSAT • Participants will be evaluated based on compliance to mission requirements, documentation and presentation during PDR & CDR, engineering and management aspect. Bonus point will be given for their creativity & innovative. • SiswaSAT will be carried by captive balloon with helium gas up to 150m from ground and launch.

  25. Thank You

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