JERG-2-320 構造設計標準 - 安全・信頼性推進部
Contents
1.2.
3.
4.
5.
6. 6 2 3 1 NDD
7. 3 71 JERG 2 320A
8. 4 8 2 1
9. 5 3
10. 6 2 2 4 Proto Flight Test Proto Flight Model PFM
11. 4 8 2
12. 20 JERG 2 320A 4 2 4 2 1 4 2 1 1
13. 1 2 3
14. 74 Bread Board Model BBM 75 Structure Development Model
15. 5 10 a 2
16. 70 JERG 2 320A 1 2 3 4 5 6 X 7 8 6 2 4 1
17. 29 JERG 2 320A 4 3 4 3 1 4 3 2 1 4 2 3 4 1 1
18. 5 6 JERG 2 130 HB002
19. 6 2 6 2
20. 4 3 6 4 3 6 1 JERG 0 001 4 3 6 2
21. 4 MMPDS Aerospace Structural Metal Handbook 5 13 1 G
22. 4 5 3 5 43 JERG 2 320A 6
23. 98 Functional Test gt 99 Pressure Vessel 1 0 MPa 0 2 MPa 100 Composite Overwrapped Pressure Vessel COPV 101 Propellant Tank 102 Attach Plane and Mount Plane
24. 5 JAXA a
25. JAXA
26. 2 4 3 8 4 3 8 1 MIL
27. JAXA 1 A 2 B
28. 5 8 4 2 2
29. 5 5
30. a b c d 4 a b JAXA a 1 5 b 2
31. FED SPC MMM A 132 50 JERG 2 320A 4 8 4 8 1
32. 2
33. 3 4 a b c d e f
34. 4 JERG 0 001 4 3 14 4 3 13
35. 5 3 4 2 3 4 2 2
36. 45 JERG 2 320A 4 6 1 2 a 3 1 2
37. c 4 2 4 1 3 1
38. Appendix A 73 JERG 2 320A
39. 41 4 4 JERG 2 320A 4 1 4 3 4 6 4 9 5 6 1 RG Q S GG 5 6 7 8 9 D
40. 2 2 1 2 1 2 3 1 DC
41. 4 5 2 4 1 2 1 34 JERG 2 320A 2
42. JAXA 2 74 JERG 2 320A
43. 4 JERG 2 320A Appendix B 1 2
44. 2 1 2 3
45. 3
46. 31 JERG 2 320A PFM 4 3 2 1 1 1 20 A 1 1 lt PM FM OF 1 25
47. 1 30 JERG 2 320A 0 29 2 4 3 2 4 3 2 1
48. 92 Acoustic Test 93 Shock Test 94 Pyro Shock Test Pyrotechnic Test
49. 100Hz 1 JERG 2 130 HB003
50. 5 11 4 3 13 1 2 4 3 13 38 JERG 2 320A
51. 4 PAF PAF
52. 2 28 JERG 2 320A ISO 14644 1 8 FED STD 209D 100000 3
53. 2 AT 4 1 5 2 QT 77 JERG 2 320A 6 2 7 2
54. JERG 2 002 4 3 3 1 JRM 004A 4 4 3 1 4 JERG 2 002 4 3 3 2 JRM 005 4 8 3 5
55. 2 4 3 16 39 JERG 2 320A 1 2
56. 4 2 2 3 4 2 2 4 1mm
57. 2 CFRP TML 1 0 CVCM 0 1 1 2 TML CVCM WVR
58. JERG 2 310 1 2
59. JAXA 67 JERG 2 320A 6 2 2 3 Acceptance Test Flight Model FM PM PM FM
60. 76 Thermal Development Model 77 Flight Model FM JERG 2 320A 78 Prototype Model PM
61. MIL MIL 0 25 PFM
62. JMR 005 4 9 2 4 9 4 JAXA 4 9 2 4 9 2 1 1 2
63. 4 2 3 4 2 3 1 1
64. 30 500 m 23 JERG 2 320A 4 2 2 5
65. H IIA Load Factor M V 1
66. 5 4 JERG 2 320A
67. 3 a b c d e g h iD G k 1 6 2
68. gt 82 Test 83 Development Test 84 Qualification 85 Qualification Test QT Proto Model PM JERG 2 320A 86 Acceptance Test AT
69. 3 a b c d e g bh 0 k 4 7 1 MMPDS Metallic Materials Properties Development and Standardization MIL HDBK 1 7 C
70. 1 37 JERG 2 320A 1 2 CFRP 2 2 D
71. 87 Proto Flight Test PFT 88 Proof Test 89 Environmental Test 90 91 Vibration Test
72. 4 3 2 3 4 3 2 3 1 4 3 2 3 1
73. 4 3 4 1 2 4 3 5 1
74. 2 120Hz
75. MLI JERG 2 311 MLI 1 A V 1 x10 cm2 cm 35 JERG 2 320A 1 1 0 1 5 mm 4 3 7 1
76. 4 5 2 1 2 H IIA 25mm 3
77. 1 3 1 2 I 1 2
78. 109 6 2 7 6 2 7 1 1 2 1
79. 1 2 3 4 5 4 2 1 2 1 a b c d 2 a
80. 103 Solar Array Paddle JERG 2 320A 104 Deployable Antenna 105 Pyrotechnic Device 106 Thermal Insulation
81. 6 2 2 64 JERG 2 320A 1 Proof Test 2 Qualification Test QT 3 Acceptance Test AT 4 Proto Flight Test PFT PM FM PM FM PFM QT AT
82. 25 JERG 2 320A 5 100Hz 20 2000Hz Coupled Load Analysis CLA CLA 2
83. 2 a b c d e f JERG 2 320A 3
84. 6 2 2 5 6 2 2 6
85. 114 Special Process 115 Lot 116 Inspection 117 Non Destructive Inspection 118 Nonconformance
86. JERG 2 002 4 3 3 3 JRM 005 4 8 4 6 JRM 005 4 8 4 7 JERG 2 002 4 3 6 2 JRM 005 4 8 8 2 Appendix C 3 1 M 1 1 4 JERG
87. 0 G 5 14 61 JERG 2 320A 6 6 1
88. 119 Failure 120 Quality JERG 2 320A 121 Quality Requirement 122 Quality Assurance 123 Safety AT BBM CLA CVCM EM EMC FM MEOP N A PAF PFM PFT PM QT TML WVR Acceptance Test Bread Board Model Coupled Load Analysis Collected Volatile Condensable Material Engineering Model Electromagnetic Compatibil
89. JERG 2 320A 95 Tnermal Vacuum Test 96 Thermal Balance Test 97 Special Test
90. 1 JERG 2 130 HB002 Appendix D 2 60 JERG 2 320A 5 12 5 11
91. 4 5 6 7 8
92. 48 Yield Strength 0 296 49 Proof Stress 0 29 50 Ultimate Strength Ultimate Tensile Strength 51 A B S A value B value S value A 99 959 B 9096 95
93. PFM a b a PFM EM PFM b PFM PFM
94. QT QT AT PFT Appendix A 6 2 2 1 Proof Test 1 a b c
95. 42 JERG 2 320A 4 5 4 2 2 4 2 3 4 6 4 5 1 1
96. 2 6 2 6 1 2 3 4 5 JERG 2 130 HB003 JERG 2 130 HB002 JERG 2 021 JAXA
97. 6 2 10 1 2 1 2 3 4 1
98. JERG 0 001 4 3 15 1 2 1
99. 42 Catastrophic Failure 43 Ultimate 44 Collapse JERG 2 320A 45 Buckling 46 Crippling gt 47 Allowable Load Stress Strain
100. 1 SN 2 5 2 4 2 3 2
101. 6 2 8 1G G 6 2 9 5 14 6 1 1
102. 2 G 3 4 5
103. 4 3 2 3 1 CFRP 0 2 1 2 0 25 1 25 0 25 1 25 0 25 1 25 33 JERG 2 320A 4 3 3 1 2
104. 1 2 4 3 2 3 a PM 69 JERG 2 320A 1 25 x1 25 x12 b PFM
105. 57 JERG 2 320A 5 7 Coupled Load Analysis Coupled Load Analysis 1 2
106. PAF a PAF PAF PAF 44 JERG 2 320A b PAF PAF PAF
107. PFM FM d b JAXA PM 65 JERG 2 320A PM
108. 58 JERG 2 320A i iD ii 5 9
109. JERG 2 320A 2 JAXA 2 1 1 2 3 4 5 6 7 8 9 2 2 1 2 3 4 JAXA JERG 0 001 JERG 2 002 JERG 2 130 HB003 JERG 2 130 HB002 JERG 2 021 JERG 2 310 JERG 2 311 MLI JERG 2 152 JMR 010 MMPDS Metallic Materials Properties Development and Standardization MIL HDBK 17 Composite Materials Handbook Aerospace Structural Metal Handbook ISO 14644 1 Cleanrooms and associated controlled environments Part 1 Classification of air
110. interface Control Specification jnterface Control Drawing 110 Configuration JERG 2 320A 111 Operation Life 112 Useful Life 113 Fabrication
111. 5 mm 2 10 0 1 JAXA b 3 10 N A kg m
112. MIL 0 25 2 PFM FM 6 2 2 2
113. gt 68 Mass Properties 69 Alignment 70 Alignment Measurement JERG 2 320A 71 Electromagnetic Compatibility gt 72 Project 73 Development Model
114. 107 _ Wire Harness gt 108 Reliability 109 Interface Control Document Interface Control Specification Interface Control Document
115. 4 1 1 1 2 3
116. 4 1 2 1 2 3 JERG 2 320A 4 5 6 7 8 9 10 11 12 13 14 15 16 17 4 1 3
117. MMPDS Metallic Materials Properties Development and Standardization Aerospace Structural Metal Handbook A 4 7 2 MMPDS Metallic Materials Properties Development and Standardization Aerospace Structural Metal Handbook ASTM A B 4 7 3 48 JER
118. 54 JERG 2 320A 5 1 2 3 4 5 6 7 Coupled Load Analysis 8 9 10 a b c d 11 12 13 14
119. 2 4 3 2 2 4 2 2 4 2 3 Margin of Safety MS 4 3 2 1 4 2 3 4 32 JERG 2 320A LL gt N J MM MMPDS A 4 7
120. b 21 JERG 2 320A or x 1 2 OO Q 3 4 4 2 2
121. 53 JERG 2 320A 4 9 3 4 9 3 1 1 2 3 4 5 6 2 3 IN 4 9 3 2
122. 79 Proto Flight Model PFM 80 Structural Analytical Model Structural Mathematical Model 81 Thermal Analytical Model Thermal Mathematical Model
123. JAXA PFM FM JAXA 6 2 6 5
124. 1 JAXA 4 3 9 1 2 36 JERG 2 320A 1
125. 4 2 2 1 H IA Load 22 JERG 2 320A Factor M V 4 2 2 2
126. 4 2 6 JERG 2 152 4 2 7 1 3 JMR 010 1
127. gt 31 Static Load quasi static load 32 Thermal Stress 33 Residual Stress 34 35 Maximu
128. 4 8 2 2 4 8 2 3 51 JERG 2 320A 4 00 3 4 8 4 52 JERG 2 320A 4 9 4 9 1
129. 79 JERG 2 320A Appendix A 1 2 3
130. b 59 JERG 2 320A c
131. Q RRS RRS JERG 2 130 HB002 2 PSD JERG 2 130 HB002 JAXA PSD 8Hz 6 2 6 4
132. 68 JERG 2 320A PFM c d c PFM d PM FM
133. gt 24 POGO 25 Burnout 26 Sloshing 27 Eclipse JERG 2 320A 28 Albedo 29 _ Cosmic Ray w 30 Contamination
134. 4 3 18 4 3 19 4 3 19 1 4 3 19 2 4 3 19 3
135. 3 4 5 6 X 7 8 4 9 2 2 4 9 2 3 4 9 2 4
136. P xy mirxiryi P yz miryi zi P zx mirzirxi JAXA 46 JERG 2 320A 4 7 1 2
137. 14 Equipment Unit 15 Assembly 2 16 Device 17 Par 1 2 JERG 2 320A 18 Material 19
138. 65 Damage Tolerance Design 66 Damage Control 2 67 Damage Prevention Control
139. RF 49 JERG 2 320A 1 2 3 4 1 4 7 6
140. FM 2
141. PAF PAF a PAF PAF b PAF PAF
142. 2 2 2 4 3 1 1 4 3 1 1 CFRP wrinkling 3
143. nk 40 59 18 41 gt I 41 2191 7 RN 41 A4819 2 Sn 41 935 41 4 4 IkI 42 4 5 kz 43 4 5 1 43 4 5 2 44 4 5 3 45 6 NO NC 46 JERG 2 320A 47 A 47 ey Pb gt DR 48 A4773 7 XRF ITSY Nd EN 48 A474 OECD 49 4 49 4 7 6 Uz 50 4 8 kk 51 4 8 ER 51 4 8 2 zk 51 I TOO 51 4 8 2 2 51 482 3S RN TT 51 8S SC NEG tp 52 4 8 ee 52 97 53 A 53 4 9 2 53 E29 53 4 9 2 2 53 4 9 2 3 4 53 4 9 2 4 53
144. 1 25 c FM 1 0 1 2 d 6 2 3
145. JAXA 6 2 6 3 1 75 JERG 2 320A PSD JERG 2 130 HB002 JAXA PSD 8Hz PSD PSD
146. gt 1 24 JERG 2 320A 2
147. 12 Subsystem 13 Component
148. 4 2 3 3 4 2 3 4 a 3 26 JERG 2 320A b
149. 3 3 4 POGO
150. M 1 2 4 Structure 20 Structural Analytical Model 80 Structural Mathematical Model Structural Assembly 21 Structure Development Model 75 Yield Strength 48 Yield Load 39 Failure 119 Contamination 30 Configuration 110 Component 13 Thermal Insulation 106 Water Vapor Regained WVR 61 Collected Volatile Condensable 60 Material CVCM Maximum Expected Operating 35 Pressure MEOP Maximum Expected Load 36 Material 18 Buckling 45 Operation Life 111 Subsystem 12 Residual Stress 33 Test 82 System 11 Mass Properties 68 Ultimate 43 Ultimate Load 40 Ultimate Strength 50 Primary Structure 22 Lifetime 9 Shoc
151. Appendix B 5 1 1 2 3 55 JERG 2 320A 5 2
152. 2 3 4
153. 4 9 3 3 4 9 3 4 1 2 3 4 9 4
154. M S 1 0 b 6 2 5 1 2 72 JERG 2 320A
155. TML 1 0 24H 7x10 Pa 125 CVCM 0 1 25 C 4 3 17 1 40 JERG 2 320A 2
156. 39 Yield Load 0 2 40 Ultimate Load 41 Detrimental Deformation
157. JERG 2 002 62 JERG 2 320A 6 1 1 1 2
158. 4 3 2 1 1 4 3 2 1 1
159. 7 Bus Equipment 8 Operation 9 Lifetime Service Life Life Cycle JERG 2 320A 10 Required Life lt gt 11 System
160. MIL MIL 0 25 FM MIL
161. 19 4 1 3 20 A AT A 21 22 ne 21 4 2 1 1 21 21 ee eT 22 4 2 2 1 22 A ON 2 RRB 23 A422 92 23 4722 4 SSRN Ni 23 4 2 2 5 24 2190 24 EC 2 I O 24 A292 ET Ee 26 4 D2 30 9 mn 26 2 2 84 SR 26 0 0 Ne 27 yy 28 0 PR PP 28 4 2 7 273 ya 28 JERG 2 320A 4 3 30 4 ee 30 We Wr OO A en A 31 4 372 1 Do 31 GS ro ee 32 4 3 2 3 33 1 2 34 3 34 4 3 5 4 34 lt 5 35 4 9 6 1 i 35 4 B65 2 NV 35 yc By Eo En RT 36 9 Se ono oo ARG 36 4 3 8 1 es 36 Dc te ly Sr aS Bi I OO 36 4 3 10 Ek 37 95 38 4 3 12 38 KM 38 42914N Goa 39 4 3 15 39 4 3 16 HH 39 4 3 17
162. 63 JERG 2 320A 4 a b c d e f JERG 2 002 Appendix B 6 2 1 1 PM FM 2 PFM 3
163. S A B 52 Creep JERG 2 320A 53 Stress Rupture L 54 Corrosion 55 Stress Corrosion Cracking 56 Galvanic Corrosion 57 Fretting Corrosi
164. 2 27 JERG 2 320A 3 4 2 5 2 1 2
165. 2 3 4 1 2 3 4 1 2 4 7 5
166. Collapse 44 POGO 24 Mission 4 Mission Equipment 6 Mission Requirement 5 Detrimental Deformation 41 Useful Life 112 Required Life 10 Lot 115 Wire Harness 107
167. Thermal Vacuum Test 95 Thermal Balance Test 96 Thermal Development Model 76 Burnout 25 Catastrophic Failure 42 Pyro Shock Test 94 Pyrotechnic Test Bus Equipment 7 JERG 2 320A M 1 4 4 Non Destructive Inspection 117 34 Fatigue 62 Fatigue Life 63 Quality 120 Quality Assurance 122 Quality Requirement 121 Fail Safe Design 64 Nonconformance 118 Composite Overwrapped 100 Pressure Vessel COPV Corrosion 54 Part 17 Flight Model FM 77 Proof Test 88 Fretting Corrosion 57 Bread Board Model BBM 74 Project 72 Prototype Model PM 78 Proto Flight Test PFT 87 Proto Flight Model PFM 79
168. d 5 11 1
169. 6 2 6 1 1
170. PAF 5 6 4 5 3
171. Qualification Test Proto Model PM 66 JERG 2 320A 6 2 2 3 QT AT
172. 1 Q 10 1 3 2 Q 10 1 3 76 JERG 2 320A
173. MMPDS Aerospace Structural Metal Handbook S N S N 50 2 4 1
174. 1 1 DC 2 3 2 4 3 10 1
175. 24 lt gt 62 Fatigue JERG 2 320A 63 Fatigue Life 64 Fail Safe Design
176. Item 20 Structure 21 Structural Assembly 22 Primary Structure 23 Secondary Structure
177. PM FM PM PM FM PM FM 2 PFM PFM 2 PM FM PFM
178. 6 2 1 2 3 4 5 6 7 8 9
179. 2 320A Item 19 Out Gas 58 Pressure Vessel 99 Alignment 69 Alignment Measurement 70 Albedo 28 Factor of Safety 38 Safety 123 Interface Control Document 109 7 Acceptance Test AT 86 Spacecraft 1 Cosmic Ray 29 Space Probe 3 Operation 8 A B S A value B value S value 51 Stress Corrosion Cracking 55 Acoustic Test 92 Development Test 83 Development Model 73 Pyrotechnic Device 105 90 Environmental Test 89 Equipment Unit 14 Functional Test 98 Allowable Load Stress Strain 47 Assembly 15 Creep 52 Crippling 46 Inspection 116 JERG 2 320A
180. A PFM 1 25 1 25 1 5 1 5 2 0 1 25 1 5 1 2 1 1 JAXA 1 0 3 1 5 1 25 1 25 PFM PFM PFM PFM
181. ISO 22010 Space systems Mass properties contro 2 78 JERG 2 320A 6 2 11 a b PAF 6 3
182. 3 4 5 6 7 JERG 2 002 JMR 005 JMR 004A 1 a 4 1 2 b 4 1 3 c 4 2 3 d 5
183. 4 9 3 54 459 9 NN ON 54 4 9 3 2 54 469 9 90 54 4 933 4 RE 54 A 4 54 5 55 5 55 5 2 56 5 3 56 5524 56 5 5 57 5 6 57 5 7 Coupled Load Analysis 4 58 0 PP 58 JERG 2 320A 5 9 59 5 10 59 oo I 5 1 60 5 1 on 61 1 EC 1 2 2 TO 61 SS 61 Gi 62 6 1 es 62 6 1 1 63 6 2 63 6 2 1 64 6 2 4 64 6 2 2 1 Proof Test es 65 6 2 2 2 Qualification Test EI 66 6 2 2 Acceptance Test I 68 6 2 2 4 Proto Flight Test 2 4 68 6 2 2 I 69 6 2 2 6 OUWT 69 6 237 70 6 2 3 1 NDD ee 70 6 2 4 71
184. 6 2 5 4 72 6 2 6 73 6 2 6 1 74 6 2 6 2 75 6 2 6 3 ee 75 6256 4 EE 76 6 2 6 5 5 L Ed 77 6 2 7 77 6 7 KK 77 6 2 7 2 78 6 2 8 7541XYFD 78 6 2 9 78 6 2 10 78 6 2 11 4 79 6 3 ca 79 JERG 2 320A AppendixA A 1 Appendix B B 1 Appendi C I C 1 Vi JERG 2 320A 1 1 1 1 JAXA 2
185. C 3 4 3 11 EMC 4 3 12 1 2 JERG 0 001
186. G 2 320A ASTM A B 10 4 7 4 1
187. JERG 2 320A 2 3 5 3 1 A JAXA JAXA Disclaimer The information contained herein is for general informational purposes only JAXA makes no warranty express or implied including as to the accuracy usefulness or timeliness of any information herein JAXA will not be liable for any losses relating to the use of the information 305 8505 2 1 1 JAXA Japan Aerospace Exploration Agency JERG 2 320A 1 COOISHRIHOSRSHORRRGSRIGRR8283RRSSRSOEHEHERIOEIRO 1 Tel OO 1 OD 1 1 2 2 2 2 1 JAXA kk 2 272 2 3 3 3 3 SN NN 18 9 Rn 19 19 4 1 1 19 192
188. cleanliness MIL HDBK 5 Metallic Materials and Elements for Aerospace Vehicle Structures 0o JERG 2 320A 3 3 1 Appendix C gt 1 Spacecraft 2 Artificial Satellite 3 Space Probe 4 Mission 5 Mission Requirement 6 Mission Equipment
189. ity Flight Model Maximum Expected Operating Pressure Not Applicable Payload Attach Fitting Proto Flight Model Proto Flight Test Prototype Model Qualification Test Total Mass Loss Water Vapor Regained JERG 2 320A JERG 2 320A 4 4 1
190. k Test 93 Eclipse 27 Artificial Satellite 2 Vibration Test 91 Reliability 108 JERG 2 320A M 1 3 4 Propellant Tank 101 Stress Rupture 53 Sloshing 26 Limit Load 37 Fabrication 113 Static Load 31 Total Mass Loss TML 59 Damage Control 66 Damage Tolerance Design 65 Damage Prevention Control 67 Solar Array Paddle 103 Proof Stress 49 Device 16 Deployable Antenna 104 Electromagnetic Compatibility 71 Galvanic Corrosion 56 Special Process 114 Special Test 97 Attach Plane and Mount Plane 102 Qualification 84 Qualification Test QT 85 Secondary Structure 23 Thermal Stress 32 Thermal Analytical Model 81 Thermal Mathematical Model
191. m Expected Operating Pressure MEOP 36 Maximum Expected Load 37 Limit Load JERG 2 320A 38 Factor of Safety Safety Factor Design Factor Design Safety Factor
192. omposite Materials Handbook Aerospace Structural Metal Handbook MIL HDBK 5 Metallic Materials and Elements for Aerospace Vehicle Structures JAXA MIL HDBK 5 47 JERG 2 320A
193. on 58 Out Gas 59 Total Mass Loss TML 60 Collected Volatile Condensable Material CVCM 61 Water Vapor Regained WVR TML CVCM 509 23C
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