Presentation 2002/10/4
A Tennis-court-sized Reflector for Communication Satellites : Use for Engineering Test Satellite VIII
Akihiro MIYASAKA, Kyoji SHINTATE, Akio TSUJIHATA, Yuji TSUTSUMI, Makoto YOSHIHARA,
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Abstract(in Japanese) (See Japanese page)
Abstract(in English) Large deployable reflector (LDR) is state-of-the-arts technology in communication satellites to achieve some satellite communication services. Government agencies of Japan are planning some experiments on communication and broadcasting services via satellites. Engineering Test Satellite VIII (ETS-VIII) will be launched in 2004, and demonstrated satellite voice communication by using cellular phones and high-quality audio broadcasting. An antenna system is a combination of the LDR and active-phased-array feeders. The LDR, 20 m along its major axis, based on a modular-mesh concept in which structure consists of several basic modules has extensibility. In order to develop the LDR, the design points on surface accuracy and electrical performance are evaluated. A surface error caused by the assembly of multiple modules was evaluated. The surface accuracy measured data compared with analysis results. Hence, the surface of the LDR was accurate enough within the system requirement. The electrical performance, especially, passive intermodulation (PIM) was measured by using a 7-module reflector. The measured PIM is so small that the LDR is satisfied the system requirements.
Keyword(in Japanese) (See Japanese page)
Keyword(in English) Large deployable reflector / LDR / Engineering Test Satellite VIII / Reflector / Deployment / PIM
Paper # SAT2002-84
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Conference Information
Committee SAT
Conference Date 2002/10/4(1days)
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Registration To Satellite Telecommunications (SAT)
Language ENG
Title (in Japanese) (See Japanese page)
Sub Title (in Japanese) (See Japanese page)
Title (in English) A Tennis-court-sized Reflector for Communication Satellites : Use for Engineering Test Satellite VIII
Sub Title (in English)
Keyword(1) Large deployable reflector
Keyword(2) LDR
Keyword(3) Engineering Test Satellite VIII
Keyword(4) Reflector
Keyword(5) Deployment
Keyword(6) PIM
1st Author's Name Akihiro MIYASAKA
1st Author's Affiliation National Space Development Agency of JAPAN()
2nd Author's Name Kyoji SHINTATE
2nd Author's Affiliation National Space Development Agency of JAPAN
3rd Author's Name Akio TSUJIHATA
3rd Author's Affiliation National Space Development Agency of JAPAN
4th Author's Name Yuji TSUTSUMI
4th Author's Affiliation NEC TOSHIBA Space Systems, Ltd
5th Author's Name Makoto YOSHIHARA
5th Author's Affiliation NEC TOSHIBA Space Systems, Ltd
Date 2002/10/4
Paper # SAT2002-84
Volume (vol) vol.102
Number (no) 360
Page pp.pp.-
#Pages 5
Date of Issue