NDLI: Development of Mission Payloads Onboard High Voltage Technology Demonstration Satellite HORYU-II

Content Provider	IEEE Xplore Digital Library
Author	Yoke, T. Iwai, S. Khan, A.R. Masui, H. Iwata, M. Toyoda, K. Mengu Cho
Copyright Year	1973
Abstract	High Voltage Technology Demonstration Satellite HORYU-II is a nanosatellite (30-cm cubic shape, 7 kg) developed by students at the Kyushu Institute of Technology. One of the objectives of this satellite is orbital demonstration of high-voltage technologies. The satellite with the highest voltage generation in low earth orbit (LEO) has been the International Space Station, generating 160 V. In orbit, especially LEO, the use of high voltage over 200 V induces arcing. HORYU-II is aimed to demonstrate new designs of solar array that can generate the power, free of arcs, by producing 300 V via a specially designed solar array itself, not via a conventional dc/dc converter. If successful, HORYU-II will become the first spacecraft in the world that achieves 300 V photovoltaic power generations in space. In this paper, we describe the detail of the mission payload development and verification. Preliminary flight results obtained since the satellite's launch on May 18, 2012 to the sun-synchronous orbit at 680-km altitude are also briefly presented.
Sponsorship	IEEE Nuclear and Plasma Sciences Society
Starting Page	3477
Ending Page	3486
Page Count	10
File Size	3484023
File Format	PDF
ISSN	00933813
Volume Number	41
Issue Number	12
Language	English
Publisher	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Publisher Date	2013-01-01
Publisher Place	U.S.A.
Access Restriction	One Nation One Subscription (ONOS)
Rights Holder	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Subject Keyword	Arrays Space vehicles Satellites Electric potential Inductors Payloads Power generation spacecraft charging Arcing high-voltage solar array space experiment
Content Type	Text
Resource Type	Article
Subject	Nuclear and High Energy Physics Condensed Matter Physics

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1	Ministry of Education (GoI), Department of Higher Education	Sanctioning Authority	https://www.education.gov.in/ict-initiatives
2	Indian Institute of Technology Kharagpur	Host Institute of the Project: The host institute of the project is responsible for providing infrastructure support and hosting the project	https://www.iitkgp.ac.in
3	National Digital Library of India Office, Indian Institute of Technology Kharagpur	The administrative and infrastructural headquarters of the project	Dr. B. Sutradhar bsutra@ndl.gov.in
4	Project PI / Joint PI	Principal Investigator and Joint Principal Investigators of the project	Dr. B. Sutradhar bsutra@ndl.gov.in Prof. Saswat Chakrabarti will be added soon
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A review on satellite solar array arcing phenomenon

Electrostatic Analysis of an Artificial Orbiting Satellite for Absolute Charging

Experiment study on electrostatic discharge of LEO high voltage solar array

Spacecraft Charging, Plume Interactions, and Space Radiation Design Considerations for All-Electric GEO Satellite Missions

Spacecraft Charging Analysis of Large GEO Satellites Using MUSCAT

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A review on the mechanisms of electrical arcing and electrostatic discharge on space solar arrays

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Charging and Arcing Test on Semiconductive Coated Solar Coupon Panel

Development of Mission Payloads Onboard High Voltage Technology Demonstration Satellite HORYU-II

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