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| Paper Abstract and Keywords | ||
| Presentation | 2016-05-19 16:40 [Special Talk] CURRENT STATUS AND EVOLVING PLAN OF JAPANESE FLAGSHIP LAUNCH VEHICLE Takanobu Kamiya (MHI)  SAT2016-7 |
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| Abstract | (in Japanese) | (See Japanese page) |
| (in English) | The Japanese flagship launcher, H-IIA and H-IIB have succeeded continuously and the launch success rate has reached to 97 percent. Last year, the H-IIA flight No. 29 launched a commercial satellite in Nov. 2015. Some new technologies such as “upgrade” developed by Japan Aerospace Exploration Agency (JAXA) were adopted in the flight, so that the H-IIA is able to inject satellites closer to geostationary orbit than conventional geostationary transfer orbit. To meet various worlds commercial satellite needs, the price of flagship launcher should be verify flexibly, however, the “upgrade” could enhance its performance with some optional items. Therefore, Japanese government started developing a series of new flagship launch vehicle, H3, in order to aim to be more competitive in satellite launch market much. H3 has the plan to launch first flight in FY2020. The launcher would provide attractive price, almost half price compared with previous launcher such as H-IIA and H-IIB, and high reliability succeeding to the previous one. Current status of H-IIA/B and the H3 development is reported. | |
| Keyword | (in Japanese) | (See Japanese page) |
| (in English) | H-IIA / H-IIB / H3 / Flagship launch vehicle / / / / | |
| Reference Info. | IEICE Tech. Rep., vol. 116, no. 41, SAT2016-7, pp. 37-40, May 2016. | |
| Paper # | SAT2016-7 | |
| Date of Issue | 2016-05-12 (SAT) | |
| ISSN | Print edition: ISSN 0913-5685 Online edition: ISSN 2432-6380 | |
| Copyright and reproduction |
All rights are reserved and no part of this publication may be reproduced or transmitted in any form or by any means, electronic or mechanical, including photocopy, recording, or any information storage and retrieval system, without permission in writing from the publisher. Notwithstanding, instructors are permitted to photocopy isolated articles for noncommercial classroom use without fee. (License No.: 10GA0019/12GB0052/13GB0056/17GB0034/18GB0034) | |
| Download PDF | SAT2016-7 |
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| Conference Information | |
| Committee | SAT WBS |
| Conference Date | 2016-05-19 - 2016-05-20 |
| Place (in Japanese) | (See Japanese page) |
| Place (in English) | Nagoya Institute of Technology |
| Topics (in Japanese) | (See Japanese page) |
| Topics (in English) | Coding, Modulation, Signal Processing, etc. |
| Paper Information | |
| Registration To | SAT |
| Conference Code | 2016-05-SAT-WBS |
| Language | Japanese |
| Title (in Japanese) | (See Japanese page) |
| Sub Title (in Japanese) | (See Japanese page) |
| Title (in English) | CURRENT STATUS AND EVOLVING PLAN OF JAPANESE FLAGSHIP LAUNCH VEHICLE |
| Sub Title (in English) | |
| Keyword(1) | H-IIA |
| Keyword(2) | H-IIB |
| Keyword(3) | H3 |
| Keyword(4) | Flagship launch vehicle |
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| 1st Author's Name | Takanobu Kamiya |
| 1st Author's Affiliation | Mitsubishi Heavy Industries,LTD. (MHI) |
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| Speaker | Author-1 |
| Date Time | 2016-05-19 16:40:00 |
| Presentation Time | 50 minutes |
| Registration for | SAT |
| Paper # | SAT2016-7 |
| Volume (vol) | vol.116 |
| Number (no) | no.41 |
| Page | pp.37-40 |
| #Pages | 4 |
| Date of Issue | 2016-05-12 (SAT) |
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