Hodoyoshi Panel Discussion
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1 Hodoyoshi Panel Discussion FREDDY PRANAJAYA Head of Research and Development Space Flight Laboratory University of Toronto Institute for Aerospace Studies 4925 Dufferin Street, Toronto, Ontario, Canada, M3H 5T6 UN/Japan Nano-Satellite Symposium, October 2012, Nagoya, Japan
2 Presentation Outline Operational Mission (Commercial, Governmental) Upcoming Missions (Scientific, Governmental) Discussion: Quality vs. Cost 11 Oct 2012 Pranajaya Hodoyoshi Panel Discussion 2
3 NTS Nanosatellite Tracking of Ships (also known as CanX-6) Ship tracking using Automatic Identification System (AIS) COM DEV Ltd, Canada COM DEV AIS Receiver 6.5 kg, 20 by 20 by 20 cm (excluding antenna) Initially technology demonstrator, become an operational mission Operational (4 years, 5 month) Rapid development and deployment (6 mo. development, launch in mo. 7) 11 Oct 2012 Pranajaya Hodoyoshi Panel Discussion 3
4 AISSat-1 Automatic Identification System Satellite 1 Ship tracking over Norway Norwegian Defense Research Establishment/FFI FFI/Kongsberg AIS Receiver 6.5 kg, 20 by 20 by 20 cm (excluding antenna) Initially technology demonstrator, become an operational mission Operational (2 years, 3 month) 11 Oct 2012 Pranajaya Hodoyoshi Panel Discussion 4
5 BRITE Constellation BRIght Target Explorer Six satellite space astronomy constellation for long-duration observation of bright stars with extremely long periods of oscillation. UniBRITE, BRITE-Austria (U. Vienna, TUG, FFG), BRITE-PL1, BRITE-PL2 (SRCPAS), BRITE-Toronto, BRITE-Montreal (CSA) 3 cm aperture optical telescope 6.5 kg, 20 by 20 by 20 cm (excluding antenna) Launch of UniBRITE and BRITE-Austria at the end of 2012 on PSLV-C20 Launch of BRITE-PL1 on Dnepr-2012#1 in 2013 Launch of BRITE-PL2 TBC Launch of BRITE-Toronto, BRITE-Montreal on Dnepr Oct 2012 Pranajaya Hodoyoshi Panel Discussion 5
6 NEMO-AM Nanosatellite for Earth Monitoring and Observation Aerosol Monitor Regional aerosol monitoring Indian Space Research Organization, India Observation in / / nm dual polarization, multi-illumination angle, 40 m to 200 m GSD, ~100 km Swath * nm band not used, instrument capable to 2.5 um 15 kg, 44 by 27 by 20 cm, with 60 by 60 cm main array In Final Manufacturing Phase Completion in 2013 Launch on PSLV Body Mounted Solar Array S-Band Antenna Fine Sun Sensor GPS Antenna S-Band Antenna Main Solar Array Instrument Aperture GPS Antenna Main Solar Array Instrument Aperture Star Tracker 11 Oct 2012 Pranajaya Hodoyoshi Panel Discussion 6 S-Band Antenna
7 AISSat-2 Automatic Identification System Satellite 2 Ship tracking over Norway Norwegian Defense Research Establishment/FFI (Governmental) FFI/Kongsberg AIS Receiver 6.5 kg, 20 by 20 by 20 cm (excluding antenna) Rebuild of AISSat-1 Launch TBA, in final negotiations 11 Oct 2012 Pranajaya Hodoyoshi Panel Discussion 7
8 NEMO-HD Nanosatellite for Earth Monitoring and Observation High Definition Multi-spectral high-resolution imaging Slovenian Centre of Excellence for Space Sciences and Technologies (SPACE-SI) 2.8 m GSD, 10 km Swath Multi-Spectral Imaging (PAN/B/G/R/NIR) and Real-time HD Video 75 m GSD Wide Swath HD Imaging and Video 50 kg, 44 by 27 by 20 cm Completion in end of 2013 Launch in 2014 Secondary Instrument Aperture Star Tracker S-Band Antenna Primary Instrument Aperture X-Band Antenna 11 Oct 2012 Pranajaya Hodoyoshi Panel Discussion 8
9 Discussion Quality vs. Cost Advanced nanosatellites open new application possibilities Performance driven by end-user, limited by physics New technologies improve performance, quality while controlling costs and schedule Design with margin helps ensure quality Heritage is important, reduces risks Small, tightly-knit, experienced team 11 Oct 2012 Pranajaya Hodoyoshi Panel Discussion 9
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