578 - 日本ロケット協会
Contents
1.2. 1 1 1
3. JAXA R Ne en Mey
4. 9 14 2 H2A
5. M V 4 TAXA
6. 1 1
7. 2
8. 8 M V 2006 M V
9. 1 N A RAE HR
10. SPS JAXA
11. X 33 SSTO SSTO
12. _ 1 RN AC RR A SE A SR SAE SE A SE EAE SE EAE SE SAE SR SO 4 amp 2013 9 14 14 00 60 SPRINT A 3 1 H IA B SRB A 2 3 M V M 34 KM V2
13. CSR 10 16 50 11 7 ISS 4 3 16 4 ISS NASA 67 9
14. SRB A B1 Bl H IIA B CFT 5 B1 Bl B1 1 1
15. 10 9 JAXA 17 9 H2A 22 21 H2A JAXA 10 18 IHI HI 6 170 9
16. 600 700 1 1000 DC 1
17. 1 1 1999 2 TSTO NASDA ISAS IHNAL 3 TSTO AXA H IIA 6
18. TAXA KHI IHI IA WG JAXA IA KHI 1 PM KHI IA KHI
19. 10 27 26 2m 150mm 500 m
20. 252 5210 3 1 1 e mail shimada toru jaxa jD 5 5 25 10 31 300 100 0003 1 1 1 2F TEL 03 6267 4550 FAX03 6267 4555 101 0038 1 171960 Phone 03 3252 2149 161 0031 1 26 6 Phone 03 3952 4466 No 57 8 2013
21. Dnepr LEO2 840 42M Dnepr 36 2015 4 D2 2 4 30 70 9 20 LM 3B 12 D2 2 5 Cyclone 4 Cyclone 4
22. Dnepr Dnepr ICBM RD 810 URM universal rocket module D2 2 D2 2 2 Vostochny 2015 Soyuz2 NK 33 1 2020 Angara 2030 D2 2 3
23. 2003 IAC Exhibition 2014 ESA JAXA 3 1
24. 4 5 60km 10 25 10 6 NASA ILunar Atmo sphere and Dust Environment Explorer LADEE 2013 9 7 GMT NTO 100 445N 10 7 Aerojet Rocketdyne 10 25 4B 16 Shijian 16 10 25 NASA SpacefHight com 10 25 18 9 GMT ILS M M XM
25. D2 D2 1 D2 2 D2 4 C 4 40 C4 1 10 C4 1 1 The Development of LOX LH2 Engine in China YF 75 GG YF 75D
26. FM 6 Siriuns FM 6 10 26 ILS News 10 26 SNC NASA Dream Chaser 10 26 SNC 10 29 2C 18 Yaogan 18 10 29 SpaceHight Now Facebook URL http www jrocket org Facebook URL https www facebook com JpnRocketSociety
27. H2A nn 6 4 10 7 7 2014 H3 NASA
28. 100 10 1000 1
29. NGy Me Gy 1 CO EE EE 9 14 1 M V 7
30. expander 8 9 441000rpm 65000rpm 5 7 YEF 77 C4 1 2 Development Status of the Cryogenic Oxygen Hydrogen YF 77 Engine for Long March 5 YF 77 1 1 GG 70 2009 CDR 2014 2016 5 2015 1 YF 77 engine layout model 1 Major characteristics of YF 77 engine Item Nominal Value Unit Thrust vacuum 2 x700 kN Specific impulse 430 SeC Mixture rat
31. ISSN 0485 2877 A PUBLICATION OF JAPANESE ROCKET SOCIETY gz ZZo 2013 10 a 578 MAINICHI ACADEMIC FORUM Inc 1 1 1 Hitotsubashi Chiyoda ku Tokyo 100 0003 Japan 2013 Japanese Rocket Society IAC2013 3700 IAC C4 D2 C4 C4 1 C4 2 C4 4
32. io 5 5 Chamber pressure 10 2 MPa Weigh dry 2700 kg Expansion area ratio 49 Length 4200 mm Maximum diameter 5000 mm Flight burning 520 S Reliability 0 999 CONTENTS TAC 2013 YT ll Running Feature Article ER RR ERE RE 2 Epsilon Rocket Feature Article 1 ee 3 Epsilon Rocket Feature Article 2 ee 3 Domestic News 6 0g Overseas News RE ER RE RE ES EER ES EE ERE RE 7 D2 200 60 D2 1 C4 1 D2 1 Ariane5ME 6 D2 1 7
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