若田宇宙飛行士、国際宇宙ステーションの組立フライトへ搭乗「地球人の世紀へ」
|
|
|
- とらふみ かやぬま
- 5 years ago
- Views:
Transcription
1
2 STS-92 A 7/ /09/25 P1-2 / /21 10/5 P1-12 /1.2-4 TM (2R) P1-18 /9-19 ( ) STS-92 B 8/7 P1-38/ ,20 STS-92 C 8/16 P1-11 / A 5A.1 P1-38/1.3-1 ( ) 1P P7-7 / ( ) 6 ( ) -54 /STS-106 STS-92 D 9/6 P1-2/1.1-1 ( ) P1-3 /1.1.3(4) P1-7 /1.2.2 Z1 P1 Z,P P1-13,14/ (1) CBM P1-21,22 /(1)ISS P1-30,31 ( ) ,17 P1-38 / ,20 ( ) Rev.F Update -26 ( ) ISS Rev.F
3 2000/09/25 STS-92 9/18 P1-2 / P1-38 /1.3-1 ( ) STS-106(2A.2b) P1-41 /(5)2A.2b ( ) STS-106(2A.2b) P7-4 /7-1 ( ) 2A.2b EVA / STS-106 ( ) STS-106(2A.2b) -55/ -6 ( ) STS-106(2A.2b) STS-92 9/ ,4 P1-1 ( ) ( 2 ) 1 P1-2 /1.1-1 ( ) P1-4 /1.1-1,2 ( ) 2P P1-6 /1.2-1 ( ) Flight Plan P1-7 /1.2-2 ( ) Z1 P1-35, 36 ( ) Flight Plan EVA P1-38 /1.3-1 ( ) 2P P1-46 /1.4-1 ( ) Flight Plan P1-52P1-64 ( ) 3 ( )
4 F 1. STS STS A STS Z (CMG) (PCU) PMA-3/ (SLP) (DDCU) (ETSD) IMAX3 (ICBC-3D) (DTO) ISS (RMS) RMS A RMS (EVA) (ISS) ISS ISS A ISS /ISS STS STS-92 ISS ( 1 12 ) 1-52
5 STS-92 NASA KSC
6 MS EVARMS EVA EVA EVA EMU( ) EVA EVA EVA 7-25
7 NASDA - 2 (1) (FMPT) 92-2 (2) (IML) - 3 (3) STS-72-6 (4) (MSL-1) - 8 (5) (MFD) -10 (6) STS (7) STS-90( ) -13 (8) STS (9) STS (10) STS (1) -17 (2) -23 (3) (JEM ) -24 (4) (JEM) -26 (5) (JEM) -27 (6) JEM NASDA CIS (STS-1STS-106 ) STS ISS 3-1 NASDA pdf
8
9 12
10 1.1.3STS-92 (1) (ISS) (2) (3) (4) (5) (6) 13
11 1.1.4 (1P) () (FGB) (1) PMA-1 PMA-2 Z1 (2P) 2P 3A 11 PMA-3 14
12 15
13
14 1.2.2 Z1 17
15 P6 (PMA-2) P6 (RTAS) ( 4) ( ) (MBM) (PCU)2 Ku (SGTRC) (ETSD) Z1 (CBM) ( ) 1.2-2(1/2) Z1
16 P6 (PMA-2) Ku (SGTRC) Ku P6 ( 4) ( ) (ETSD) S CMG4 S ACBSP OSR EVA Pool Handle 1.2-2(2/2) Z1
17 CMG(Control Moment Gyros) ( )
18 S Ku PCUPlasma Contactor Units)
19 TM (2R) S (Z1 ) ( ) P6 (4A ) ( ) Z1 P PMA-3 ODS( / ) A ISS < >
20 CBM ( ) ACBM PCBM ( CBM) ( CBM)
21 114
22 Z1 Z1 (QD) 115
23 1.2.3 PMA-3(Pressurized Mating Adapter) / (SLP) 116
24 PMA-3 PMA-3SLP MBM PMA-3 ETSD (ETSD) ( DDCU(DC to DC Converter Unit) ETSD(EVA Tool Stowage Device) 117
25 1.2.6 < > IMAX (ICBC-3D) Hail Columbia Dream Is Alive Blue Planet Destiny In Space Mission To MIR 118
26 (DTO)
27 120
28 ISS (1) ISS
29 122 (2) (3)
30 1.2.8 (RMS) RMS 123
31 124
32 125
33 ( 1 ) CCTV A7U THC CCTV 1,2 A8U RHC A8L 126
34 127
35 128 ( 10cm) ( ) : 57cm 26cm
36 3 CCTV (: ) 129
37 A RMS CBM
38 131 CBM
39 132
40 1.2.9 (EVA) 133
41 134
42 RTAS(Rocketdyne Truss Attachment System) 135
43 136
44 LED ON/OFF A/B MTL 137
45 (ISS)< > ISS NASA ( Florida Today 138
46 1.3.2 ISS ICC 139
47 140
48 141 < >
49 A ISS 1 ISS 142
50
51 144
52 145
53 146
54 147 STS
55 148
56 149
57 150
58 151
59 STS-92 ISS STS
60 STS-92 ISS FD1 Ku STS-92 KSC 39A ISS OMS 45 Ku Ku ISS FD 5 (Flight Day) 1 1 STS (STS-1)
61 STS-92 ISS FD2 EMU NASDA ISS RMS ISS 3 NASDA VIP 2 STS-99 NASDA (VIP ) VIP 1-54
62 STS-92 ISS FD3 ISS ISSPMA-2 ISS#1 ISS 3A 2A2A.2b -R Bar ISS ISSPMA ISS PMA-2 ODS ODS ISS ISS()# PMA-2 ISS ( 10/5,10/9 )4 1-55
63 STS-92 ISS FD4 Z1 ISS # psia 2/3 Z1 RMS ACBM ACBM Z1 RMS Z1 RMS Z1 Z1 CBMRMS Z1 ISS #1 FD3 ISS Z1 (CBM) (EVA) 10.2 psia 2/3 EVA ()FD4 2/3 EVA Z1 CBM(Common Berthing Mechanism) CBM ISS RMS /PMA-2 SVS(Space Vision System) TV PMA
64 STS-92 ISS 5 2/2 Z1 (1) Low HoverHigh Hover Z1 Low HoverHigh Hover (PMA-3 ) Low Hover Z1 Z1 PCBM( ) High Hover Z1 SVS (2)CBM (RMS)SVS ACBM()CBM PCBM (Z1 ) RMS RMS Z1 ACBM SVS CBM PCBM ACBM PCBM ACBM (ABOLT)(4 7kN ) 8 PCBM RMS ACBM PCBM (Z1 PMA-3 12 ) (IBOLT) ( kN 5 ) (FBOLT) ( kN ) 1-57
65 STS-92 ISS FD5 ISS #1 EVA# Z1 Z1 S-Band SASA S DDCU() 4A S Z1 SGANTKu Ku 4A P6 ETSD ISS #1 RCS ISS 3A 5 EVA RMS 1 EVA 3 EVA 1-58
66 STS-92 ISS FD6 ISS PMA-3 ISS #2 ISS PMA-3 RMS PMA-3 EVA SLP PMA-3 PMA-3 RMS PMA-3 2 EVA PMA-3 SLP 16 4 RMS RMS PMA-3 PMA-3 EVA PMA-3 PMA-3 ISS #2 RCS 2 SLP PMA-3 6 ( 15cm) 24 ( 61cm) RMS EVA RMS 1-59
67 STS-92 ISS FD7 ISS # EVA (DDCU) Z1 Z1 Z1 PMA-3 Z1 (DDCU) (ETSD) ISS #3 RCS ISS ISS 1-60
68 STS-92 ISS FD8 ISS # Z1 SAFER(Simplified Aid For EVA Rescue) SAFER STS-64 SAFER () ISS #4 RCS EVA ISS SAFER ISS EVA 1-61
69 STS-92 ISS FD psiaiss #2 ISS ISS # psia EVA 1 ISS #2 ISS ISS (2 ) ISS ISS ISS ISS #5 RCS ISS R TM ISS 34 3 ISS 1-62
70 STS-92 ISS FD10 ISS ISS ISS ISS ISS 3A ISS ISS FD4, 1-63
71 STS-92 ISS FD11 Ku Ku ( ISS ) 1-64
72 STS-92 ISS FD12 () 2 OMS (KSC) KSC KSC 12 KSC STS
73 21
74 m 23.8m (ET) 47.0m 8.4m 45.5m 3.7m 1,495/(1) 37.2m 23.8m 17.3m 18.3m 534/(3 ) (SRB) (ET) (SRB) ETSRB ( 2 )
75 ET SRB 37.2m 47.0m 45.5m 56.1m 23.8m( ) 8.4m 3.7m 23. 8m( ) 23.9m(ET+ ) 17. 3m( ) 750t 589t1 2,038t (SSME 3 ( ) ( ) ( ) ) 720t 496t/1 ( 2, t 29.9t 87t/1 2,050t ) 78.6t 78.3t 78.7t (986 SLWT 3,400kg (98.1 ) 26.5t ) SSME 1 ( 104%) ,495( )/1 SSME 3534t SRB 2 2,990t 3,524t 18.3m 4.6m SLWT(Super Light Weight Tank) 23
76 24
77 / SSME OMS RCS OMS/RCS T-0 RCS RMS 25
78 26
79 27
80 28
81 29
82 210
83 211
84 (SRB) (2 ) (850 ) 25) ( SLF) SRB SRB (8 )( 260km ) SRB (LC-39) (OPF) (VAB)
85
86
87
88 OMS ( km) ( km) (7 40 ) Roll to Head-up (6 ) ( km) ( 2 45km) Roll to Head-up STS-87 (SRB) STS-92 ( )
89
90
91 (SLF) (VAB) 39B 39A O&C (SSPF) (LCC) (OPF)
92
93 (MLP) (FSS) (RSS) ( ) (MLP)
94 311
95 312
96 313
97 314
98 315
99 41
100
101 ,496km km 26,576km 12 55km 13,317km 25,338m 2,735km 86 4,074m 682km 526m 576km 41m 496km 27m 430km
102 51
103 52
104 61
105 62
106 63
107
108 65
109 66
110 67
111 68
112 STS-92 (RMS) (EVA) (RMS) RMS (a)ses(shuttle Engineering Simulator) JSC Building 16 RMS 69
113 b)mdf(manipulator Development Facility) JSC Building 9 AFD RMS RMS SES RMS RMS RMS CCTVTV MDF (C)Integrated EVA/RMS Virtual Reality Simulation Trainer (SAFER Virtual Reality Laboratory Virtual Reality (VR) Lab ) JSC ( ) HMD(Helmet Mounted Display) 2 SAFER RMS EVA (STS
114 (d)p2t2(prototype Part Task Trainer) JSC Building 45 RMS RMS (e)sms(shuttle Mission Simulator) JSC Building 5 SMS MB( ) FB( ) SMS-MB( ) SMS-FB RMS CG 611
115 RMS RMS ( ) RMS SMS (AFD)RMS 612
116 (EVA) (a)nbl(neutral Buoyancy Laboratory ) JSC 45km ( ) NBL EVA EVA (STS-82 NBL ) 61.5m, 31.0m, 12.1m NBL RMS RMS NBL (b)integrated EVA/RMS Virtual Reality Simulation Trainer (SAFER Virtual Reality Laboratory Virtual Reality (VR) Lab ) (c) RMS EVA 613
117 614
118 615
119 71
120 7-1 (1/3) EVA 1 STS-06 (SM 6) H54m 2 STS-41B (SM H35m 10) H02m 4 STS-41C (SM 11) H59m 5 6 STS-41G (SM 13) H07m H29m 7 STS-51A (SM 14) H13m MMU STS-41C SMM J.van J.van EVA D. EVA J. MMU D. 8 9 STS-51D (SM 16) H01m H10m 10 STS-51I (SM 20) H20m H31m 12 STS-61B (SM H34m 23) H46m 14 STS H31m (SM39) H58m 16 STS H43m (SM47) H30m H29m H45m J. D. Syncom S. Unscheduled EVA( ) J.van Syncom W. J.van W. EASE/ACCESS GRO Unscheduled EVA CETA (EDFE) 6F-3 6F-3 6 F-3 ( 3 EVA) EVA EVA (ASEM) Manned Maneuvering Unit SMShuttle Mission 72
121 20 STS-54 (SM53) 21 STS-57 (SM56) 7-1 EVA 2/3 EVA H32m H50m EVA EVA ESA Unscheduled EVA HST EVA 22 STS H05m HST (SM57) EVA 23 STS H54m (SM59) H35m H47m H50m STS-64 (SM64) 29 STS-63 (SM67) 30 STS-69 (SM71) H21m H51m H39m H45m 31 STS H09m (SM74) STS-76 (SM76) H53m H02m 34 STS H42m (SM82) HST 1 5 EVA SAFER (SAFER ) EDFT-01( / ) EDFT-02( )/ EVA EDFT-03( #2)/ EVA ) EDFT-04( EVA )SAFER HST H28m H11m H34m H17m 73
122 7-1 EVA 3/3 EVA 39 STS H01m 40 STS H43m H00m 42 STS H21m H02m H59m 45 STS H55m 46 STS H15m H10m H08m 49 STS STS STS H44m 6H14m < > ( )EVA ( ) EVAEDFT-06 SAFER EDFT-05 ( EVA) TV SPRINT (ISS) 2A SAFER 7 EVA 44H09mEVA ( ) ISS 2A.1 HST 3 2,3,4 EVA ESA EVA ( 3 ) ISS 2A.2a ISS 2A.2b ( ) ISS 3A - - STS-XX SMShuttle Mission SAFERSimplified Aid for EVA Rescue EDFT : EVA Development Flight Test 74
123 EVA EMU: Extravehicular Mobility Unit EVA EVA EVA 7-1 EVA EMU (LSS) EVA EVA (PLSS) EMU (SCU) (DCM) (SOP) (SSA) HUT/ LTA ( ) EMU 7-1EVA 75
124 7.3.1 ( ) 76
125 2 1 ( ) ( ) 14 ( ) ( (7 ) ) 4 6 ( ) 5 ( ( ) ) 77
126 78
127 ( ) ( ) 79
128 710
129 711 / / ( )
130 712
131 713
132 EMUEVA EVA EVA( EVA ) EVA EVA 714
133 ISS 715
134 716 / EVA D
135 717
136 718 PAD PFR PFR PAD RMS
137 ( ) APFR (WIF) 719
138 ( ) 720
139 721
140 LED ON/OFF A/B MTL 722
141 723
142 7-21SAFER EVA 724
143 EVA EVA 725
144 726 psia : pounds per square inch absolute 7-23EVA ( ) EVA EMU EMU 100% psia (0.7 ) * 4. 3psia (1/3 ) psia (1 ) 14.7psia (1 ) 6 7 *:10.2psia
145 -1
146 -2
147 -3
148 -4
149 -5
150 -6
151 -7
152 -8
153 -9
154 -10
155 -11
156 -12
157 -13
158 -14
159 -15
160 -16
161 -
162 -
163 -
164 108m()80m() 44m kw() ()30kw 1140m (U.S. Lab) 1() 1(COF) 21, km480km (407km) 51.6 H-IIA()5() (TDRS) 20007NASA -
165 -
166 SSRMS( ) < > ( ) < > ( ) < > 2 ( ) ( ) -
167 -
168 -
169 -
170 - (EM) / (PFM) /
171 -
172 -
173 -
174 -
175 -
176 -
177 -
178 -
179 -
180 -
181 -
182 -
183 -
184 -
185 -
186 ( ) (/:) STS-1 (1) STS-2 (2) STS-3 (3) STS-4 (4) STS-5 (5) STS-6 (6) STS-7 (7) STS-8 (8) STS-9 (9) STS41-B (10) STS41-C (11) STS41-D (12) /06:21 ( ) /06:13 ( ) /00:05 ( ) /01:10 ( ) /02: /00:23 TDRS-A( ) EVA /02: /01:07 / ( ) /07:47 SEPAC( ) (6) /23:17 KSC /23:40 (SMM ) LDEF( ) (19901 STS-32 ) /00:56 ( ) -42
187 -43 ( ) (/:) STS41-G (13) ERBS( ) STS51-A (14) STS51-C (15) STS51-D (16) STS51-B (17) STS51-G (18) STS51-F (19)
188 -44 ( ) (/:) STS51-I (20) STS51-J (21) STS61-A (22) STS61-B (23) STS61-C (24) STS51-L (25) STS-26 (26)
189 ( ) (/:) STS-27 (27) STS-29 (28) STS-30 (29) STS-28 (30) STS-34 (31) STS-33 (32) STS-32 (33) STS-36 (34) STS-31 (35) STS-41 (36)
190 -46 ( ) (/:) STS-38 (37) STS-35 (38) STS-37 (39) STS-39 (40) STS-40 (41) STS-43 (42) STS-48 (43) STS-44 (44)
191 -47 ( ) (/:) STS-42 (45) STS-45 (46) STS-49 (47) STS-50 (48) STS-46 (49) STS-47 (50) STS-52 (51)
192 -48 ( ) (/:) STS-53 (52) STS-54 (53) STS-56 (54) STS-55 (55) STS-57 (56) STS-51 (57) STS-58 (58) STS-61 (59)
193 -49 ( ) (/:) STS-60 (60) STS-62 (61) STS-59 (62) STS-65 (63) STS-64 (64) STS-68 (65) STS-66 (66) STS-63 (67)
194 -50 ( ) (/:) STS-67 (68) STS-71 (69) STS-70 (70) STS-69 (71) 1995 STS-73 (72) STS-74 (73) STS-72 (74)
195 -51 ( ) (/:) STS-75 (75) STS-76 (76) STS-77 (77) STS-78 (78) STS-79 (79) STS-80 (80)
196 -52 ( ) (/:) STS-81 (81) STS-82 (82) STS-83 (83) STS-84 (84) STS-94 (85) STS-85 (86) CRISTA-SPAS-2
197 -53 ( ) (/:) STS-86 (87) STS-87 (88)
198 -54 ( ) (/:) STS-88 (93) STS-96 (94)
199 ( ) STS-92 (100) (/:) C: Commander( )P: Pilot( )PC: Payload Commander MS: Mission SpecialistPS: Payload Specialist NASA Kennedy Space Center Space Shuttle Status Report Space Shuttle Press Kit Reporter s Space Flight Note Pad (Boeing )Feb.,
200
201 AAEU Aquatic Animal Experiment Unit ACBM Active Common Berthing Mechanism ACCESS Assembly Concept for Construction of Erectable Space Structures ACTS Advanced Communications Technology Satellite (STS-51) ACUC Animal Care and Usage Committee AFD Aft Flight Deck AMS-1 Alpha Magnetic Spectrometer-1 (STS-91) AOA Abort Once Around AODA Attitude & Orbit Determination Avionics APFR Articulating Portable Foot Restraint APM Attached Pressurized Module (ESA COF ) APU Auxiliary Power Unit ARC Ames Research Center ARS Air Revitalization System ASCAN Astronaut Candidate ASEM Assembly of Station by EVA Method Exercise (STS-49) ASI Agenia Spatiale Italiano ATLAS Atmospheric Laboratory for Applications and Science ATO Abort To Orbit AXAF Advanced X-Ray Astrophysics Facility BIA Bus Interface Adapter BRT Body Restraint Tether BTV Biospecimen Transport Van (KSC) CAM Centrifuge Accommodations Module (ISS) CAPCOM Capsule Communicator CAT Canister Attachment Truss CBM Common Berthing Mechanism (ISS ) CCD Charge Coupled Device CCTV Closed Circuit Television CDR Critical Design Review CDR Commander CDT Central Daylight Time CEIT Crew Equipment Interface Test CETA Crew and Equipment Translation Aid CFRP Carbon Fiber Reinforced Plastic CG Computer Graphics CI Co Investigator CIS Commonwealth of Independent States CMD Command CMG Control Moment Gyro CNES Centre Natinal d'etudes Spatiales COAS Crewman Optical Alignment Sight C/O Check Out COF Columbus Orbital Facility (ESA) CPU Central Processing Unit CRISTA-SPAS Cryogenic Infrared Spectrometers and Telescopes for the Atmosphere - Shuttle Pallet Satellite (STS-66,85) CRL Communications Research Laboratory
202 CRV Crew Return Vehicle (ISS) CSA Canadian Space Agency CSR Customer Support Room CST Central Standard Time CSVS Canadian Space Vision System CTV Crew Transport Vehicle CVDA Commercial Vapor Diffusion Apparatus C/W Caution and Warning CWS Caution and Warning System DAP Digital Auto Pilot DARA Deutschen Agentur fur Raumfahrtangelegenheiten GmbH DARA( ) 97 DLR( ) ) DAT Digital Audio Tape DCM Docking Compartment Module (ISS) DCM Display and Control Module (EMU) DDCU DC-DC Converter Unit DFRC Dryden Flight Research Center DLR German Aerospace Reserch Establishment (Deutsche Forschungstalt fur Luft-und R) DoD Department of Defense DSM Docking and Stowage Module (ISS) DSO Detailed Supplementary Objectives DSP Defense Support Program (STS-44) DTO Detailed Test Objectives EarthKAM Earth knowledge Acquired by Middle school students EASE Experimental Assembly of Structures in EVA ECG Electrocardiogram ECLSS Environmental Control and Life Support System EDFE EVA Development Flight Experiment EVA (STS-37) EDFT EVA Development Flight Test EVA EDO Extended Duration Orbiter EDT Eastern Daylight Time EDW Edwards Air Force Base EE End Effector EECOM Electrical, Environmental, Consumables Engineer EF Exposed Facility ( JEM ) EGSE Electrical Ground Support Equipment ELM-ES Experiment Logistics Module-Exposed Section ( JEM ) ELM-PS Experiment Logistics Module-Pressurized Section ( JEM EM Engineering Model EMG Electromyography EMU Extravehicular Mobility Unit ( )
203 EORC Earth Observation Research Center (NASDA) EPS Electrical Power Syste ERBS Earth Radiation Budget Satellite (STS-41B) ERS Earth Remote Sensing Satellite (ESA ) ESA European Space Agency ESC Electric Still Camera EST Eastern Standard Time ET External Tank ETSD EVA Tool Stowage Device EURECA European Retrieval Carrier (STS-46) EUV Extreme Ultraviolet EVA Extravehicular Activity FAO Flight Activity Officer FCS Flight Control System FD Flight Day FD Flight Director FDO Flight Dynamics Officer FES Flash Evaporator System FGB Functional Cargo Block (Zarya) FM Frequency Modulation FMPT First Material Processing Test FOR Flight Operations Review FRD Flight Requirements Document FRGF Flight Releasable grapple Fixture FRR Flight Readiness Review FSE Flight Support Equipment FSS Fixed Service Structure GAS Get-Away Special GC Ground Control GC Ground Commanding (MFD) GDO Guidance Officer GF Grapple Fixture GIRA Galley Iodine Removal Assembly GLO Shuttle Glow Experiments GMT Greenwich Mean Time GN2 gaseous nitrogen GNC Guidance Navigation and Control GN&C Guidance Navigation and Control GPC General Purpose Computer GPWS Ground Proximity Warning System ( ) GPS Global Positioning System GRO Gamma Ray Observatory (STS-37) GSE Ground Support Equipment GSFC Goddard Space Flight Center
204 HC Hand Controller HDTV High Definition Television HEDS Human Exploration and Development of Space Enterprise HH Hitchhiker HH Horizontal transmit, Horizontal receive HMD Helmet Mounted Display HOST Hubble Space Telescope Orbital Systems Test Platform HRM High Rate Multiplexer HST Hubble Space Telescope HTD HEDS Technology Demonstration HUT Hard Upper Torso (EMU) IBSS Infrared Background Signature Survey (STS-39) ICBC-3D IMAX Cargo Bay Camera 3 Dimension IMAX3 ICC Inboard Corner Reflector IEH International Extreme Ultraviolet Hitchhiker IFM In-Flight Maintenance IGA Inter-Governmental Agreement IML-2 International Microgravity Laboratory IMU Inertial Measurement Unit INCO Instrumentation and Communication Officer INS Inertial Navigation System IRU Inertial Reference Unit ISS International Space Station ISSP International Space Station Program IVA Intra-Vehicular Activity IVHM Integrated Vehicle Health Monitoring IWG Investigator Working Group JEM Japanese Experiment Module JEMRMS JEM Remote Manipulator System JERS-1 Japanese Earth Resources Satellite -1 1 (NASDA) JIS Joint Integrated Simulation JPL Jet Propulsion Laboratory JSC Johnson Space Center JST Japanese Standard Time KSC Kennedy Space Center LAGEOS-2 Laser Geodynamic Satellite (STS-52) LC-39 Launch Complex LCC Launch Control Center LDEF Long Duration Exposure Facility (STS41-C) LDR Logistics Double Module LED Light Emitting Diode LES Launch and Entry Suit LIF Large Isothermal Furnace
205 LiOH Lithium Hydroxyde LITE-1 Lidar In-Space Technology Experiment-1 (STS-64) LMS Life and Microgravity Spacelab (STS-78) LSLE Life Sciences Laboratory Equipment LSS Life Support System (EMU) LTA Lower Torso Assembly (EMU) MAG Maximum Absorption Garment (EMU ) MBM Manual Berthing Mechanism MBS Mobile Remote Servicer(MRS) Base System MCC Mission Control Center (JSC) MDF Manipulator Development Facility MDM Multiplexers/Demultiplexers MECO Main Engine Cutoff MEDS Multifunction Electronic Display System MET Mission Elapsed Time MFD Manipulator Flight Demonstration MGBX Microgravity Globebox MLE Middeck Locker Equivalent MLI Mluti-Layer Insulator MLP Mobile Launcher Platform MMACS Maintenance, Mechanical, Arm, and Crew System MMH Monomethyl Hydrazine MM/OD Micro-Meteoroid and Orbital Debris MMU Manned Maneuvering Unit MPESS Multi-purpose Experiment Support Structure MPLM Multi-purpose Logistics Module MPM Manipulator Positioning Mechanism MRI Magnetic Resonance Imaging MRSE Microwave Remote Sensing Experiment MS Mission Specialist MSBLS Microwave Scan Beam Landing System MSD Medical Science Division MSFC Marshall Space Flight Center MSL-1 Microgravity Science Laboratory-1 MT Mobile Transporter (ISS) MVAK Module Vertical Access Kit MWS Mini-Workstation NASA National Aeronautics and Space Administration NASCOM NASA Communications Network NASA NASDA National Space Development Agency of Japan NBL Neutral Buoyancy Laboratory (JSC) NDAS Neural Data Acquisition System NIA National Institutes of Aging NIH National Institutes of Health NIH-C National Institutes of Health Cell Culture Module(CCM)
206 NIMA National Imagery and Mapping Agency NM nautical miles NOR Northrup Lakebed Landing Site OAST-Flyer Office of Aeronautics and Space Technology O&C Operations and Checkout O&CB Operations and Checkout Building OCA Orbiter Communications Adapter OCC Organic Crystal growth Chamber OCF Organic Crystal growth Facility (FMPT) OCGP Organic Crystal growth with G-jitter Preventive Measurement (IML-1) ODS Orbiter Docking System OFK Official Flight Kit OMDP Orbiter Maintenance Down Period OMS Orbiter Maneuvering System OPF Orbiter Processing Facility OPP Orbiter Patch Panel ORFEUS-SPAS Orbiting, Retrievable Far and Extreme Ultraviolet Spectrometer-SPAS (STS-51,80) ORU Orbital Replacement Unit OSAT Office of Aeronautics and Space Technology OSVS Orbiter Space Vision System OSVU Orbiter Space Vision Unit OTA Optical Target Assembly OTD ORU Transfer Device EVA P2T2 Prototype Part Task Trainer PAD PFR Attachment Device PAO Public Affair Office PAO Public Affair Officer PC Payload Commander PCBM Passive CBM CBM PCG Protein Crystal Growth PCG-STES Protein Crystal Growth - Single Locker Thermal Enclosure System PCU Plasma Contactor Units PDI Payload Data Interrogator PDR Preliminary Design Review PDRS Payload Deployment and Retrieval System PDSU Power Distributing and Switching Unit PFM Proto-Flight Model PFR Portable Foot Restraint PGF Plant Growth Facility PGSC Payload General Support Computer PGSC/BIA PGSC/Bus Interface Adapter PGT Pistol Grip Tool (EVA )
207 PHRR Payload High Rate Recorder SRTM PI Principal Investigator P/L Payload PLSS Primary Life Support System (EMU) PLT Pilot PM Phase Modulation PM Pressurized Module ( JEM ) PMA Pressurized Mating Adapter POCC Payload Operations Control Center POIC Payload Operations Integration Center PPK Personal Preference Kits PRLA Payload Retention Latch Actuators PS Payload Specialist psia pound per square inch absolute 1 ( ) PWP Portable Work Platform QD Quick Disconnect RAM Random Access Memory RBEV Robotics Birds Eye View RCRS Regenerable Carbon Dioxide Removable System RCS Reaction Control System RDA Radar Data Analyzer REM Release/Engage Mechanism (Spartan) RF Radio Frequency RIC Recorder Interface Controller RHC Rotational Hand Controller RMCD Radiation Monitoring Container Device RME Risk Mitigation Experiments RMS Remote Manipulator System - RPCM Remote Power Controller Module RSA Russian Space Agency RSAD RMS Situational Awareness Display RSS Rotating Service Structure RTAS Rocketdyne Truss Attachment System RTLS Return to Launch Site SAFER Simplified Aid For EVA Rescue EVA SAIL Shuttle Avionics Integration Laboratory SAMS Space Acceleration Measurement System SAR Synthetic Aperture Radar SAREX-II Shuttle Amateur Radio Experiment-II SASA S-band Antenna Structural Assembly SCU Service and Cooling Umbilical SDI Strategic Defense Initiative SEPAC Space Experiment Particle Accelerator SES Shuttle Engineering Simulator
208 SEU Single Event Upset SFU Space Flyer Unit SGANT Space-to-Ground Antenna Ku SGTRC Space to Ground Transmit/Receive Controller Ku SHUCS Spacehab Universal Communications System SIB Signal Isolation Box SIGI Space Integrated GPS/Inertial Navigation System GPS/INS SIMPLEX Shuttle Ionospheric Modification with Pulsed Local Exhaust SIR Spaceborne Imaging Radar SLF Shuttle Landing Facility SL-J Spacelab-J SLP SpaceLab Pallet SLS Spacelab Life Sciences (STS-40) SLWT Super Light Weight Tank SM Single Module SM Service Module (ISS) SM Shuttle Mission S/MM Shuttle/Mir Mission SMM Solar Maximum Mission SMS Shuttle Mission Simulator SMS-FB Shuttle Mission Simulator - Fixed Base SMS-MB Shuttle Mission Simulator - Motion Base SMS Science Mission Specialist SOHO Solar and Heliospheric Observatory SOP Secondary Oxygen Pack SPACEHAB-SM SPACEHAB-Single Module SPARTAN SPAS Shuttle Pallet Satellite SPDM Special Purpose Dexterous Manipulator (ISS) SPP Science Power Platform (ISS) SPPF SPACEHAB Payload Processing Facility SRB Solid Rocket Booster SRTM Shuttle Radar Topography Mission SRL Space Radar Laboratory (STS-59,68) SSA Space Suite Assembly SSBUV/A Shuttle Solar Backscatter Ultraviolet/A SSC Space to Space Comm SSCC Space Station Control Center SSFP Space Station Freedom Program SSIPC Space Station Integration and Promotion Center (TKSC) SSME Space Shuttle Main Engine SSP Standard Switch Panel SSRMS Space Station Remote Manipulator System SSV Sequential Still Video STA Star Tracker Assembly STDN Space Flight Tracking and Data Network STL Space Tissue Loss ( ) STS Space Transportation System ( )
209 SVS Space Vision System TACAN Tactical Air Navigation TAEM Terminal Area Energy Management TAGS Text and Graphics System TAL Trans-Atlantic Abort Landing TAS-1 Technology Application and Science-1 (STS-85) TBD To Be Determined TCDT Terminal Count down Demonstration Test TCP/IP Transmission Control Protocol/Internet Protocol TDPU Telemetry Data Processing Unit TDRS Tracking and Data Relay Satellite TEAMS Technology Experiments Advancing Mission in Space (STS-77) TEPC Tissue Equivalent Proportional Counter THC Translational Hand Controller TKSC Tsukuba Space Center TM Torque Multiplier TMG Thermal Micrometeoroid Garment (EMU) TPS Thermal Protection System TRAC Targeting and Reflective Alignment Concept TSS Truss Support Structure TSS-1 Tethered Satellite System-1 (STS-46,75) TVC Thrust Vector Control UARS Upper Atmosphere Research Satellite UCD Urine Collection Device UCSD University of California at San Diego UDM Universal Docking Module (ISS) UF Utilization Flight (ISS ) UHF Ultra High Frequency USML United States Microgravity Laboratory (STS- 53,73) USMP United States Microgravity Payload VAB Vehicle Assembly Building VFEU Vestibular Function Experiment Unit (FMPT) VFEU Vestibular Function Experiment Unit (STS-90,95) VFEU/NDAS (STS-90,95 ) VGS Video Guidance Sensor VH Vertical transmit, Horizontal receive VIP Very Important Person VRCS Vernier Reaction Control System VV Vertical transmit,vertical receive
210 WBSAAMD Wide Band Stand Alone Acceleration Measurement Device WCS Waste Collection System WIF Worksite Interface WSB Water Spray Boiler WSF Wake Shield Facility (STS-60,69,80) WSSH White Sands Space Harbor WSTF White Sands Test Facility X-SAR X-band Synthetic Aperture RadarX
211 STS-92 Flight Plan( Basic ) NASDA
212
213
214
215
216
217 3 ISS ISS NASA 7A, UF-1 ISS Rev.F( ) Rev.E, DCN-4( ) NASA Rev.E 8A ISS Rev.F -19
218 FGB) (1A/R ) PMA-1 OTD( ) NODE1 (2A ) Strela :2A.1 PMA A.1 (19996) < >
219 FGB) (1A/R ) PMA-1 Strela :2A.1+2A.2a OTD( :2A.1 ) NODE1 (2A ) PMA-2 ECOMM.7-2 2A.2a (20006) < >
220 < > R (20007 )
221 < > M1(1P) P (200089)
222 (2P) P ( ) < >
223 Z 2P( ) 11 3A PMA A (200010) < >
224 TM (2R) < > R( ) (200011)
225 TM (2R ) S (Z1 ) () P6 (4A ) ( ) Z1P6 ODS(/) Z1 PMA A (200012) < >
226 < > A (200012)
227 PMA-3 MBM() PMA-2 PMA-2 ( MBM) MBM 5A PMA-2 (MBM) 5A A ISS (20011) < >
228 < > (EETCS) A (20011)
229 (4P ) A4P ( (2R) ) ) (20011 < >
230 (4P) DC1(Docking Compartment 1) R (20012 Rev.F3) < >
231 MPLM CBM PMA-3 MPLM( ) MPLM( ) A.1 (20012) < >
232 4P 5P TM P(5A.1 ) (20014) < >
233 SLP SSRMS SSRMS MPLM ( ) UHF A (20014) < >
234 LCA(Lab Cradle Assmbly) S0 5A A (20014 ) < >
235 TM (2S) TM (2R(1S)) 2S S ) (20014 < >
236 A (20015) < >
237 < > A ( II ) (20015)
238 < > S A ( Rev.F )
239 ERA(ESA RMS) P3/P4 (12A ) SPP( ) 9A.1 P6 P6 P1 (11A ) (ETCS) 12A S1 (9A ) A.1 ( Rev.F 20032) < >
240 P6 UDM(UniversalDockingModule) 3R S3/S4 (13A ) A (20032 Rev.F ) < >
241 (ELM-PS) ( 2 ) (USPM) ( ) (Rev.F 1J ) J/A (20042) < >
242 < > J (20045)
243 ETCS (EF) (ELM-ES) (Express Pallet ) (UF-3,4 ) J/A (20051) < >
244 CAM( ) COF ESA 1E CRV 18A S6 15A UF-7(CAM) (Rev.F ) < >
245 (14A ) U.S.Hab ( ) (20A ) A( ) (Rev.F 16A ) < >
246 Tel: FAX: Home Page URL
表紙1
Graduate School of Engineering Nagasaki Institute of Applied Science Graduate School of Engineering Nagasaki Institute of Applied Science Institute for Innovative Science and Technology Doctoral Program
.... 3.... 3.... 4.... 6.... 6.... 7.... 9.... 9.... 12... 12... 13... 13... 14.... 17.... 17.... 22... 22... 22... 24.... 26.... 26.... 28.... 31.... 31... 31... 31 1 .... 33... 33... 35.... 35... 35...
untitled
Ver.1 29/5/2009 1 UNISEC (UNIversity Space Engineering Consortium) UNITEC-1 (UNIsec Technological Experiment Carrier-1) 2010 5 UNITEC-1 GHz C CW UNISEC AMSAT UNITEC-1 TBD CW UNITEC-1, 2 1. UNITEC-1 UNISEC
プロダクトガイド・表1
ystem S o l u t i o n s Storage Solutions HP Solutions e-business Solutions Mechanical Computer-Aided Design Authoring Software to Create Better Product Documentation Contents Secure File Transfer Solution
2). 3) 4) 1.2 NICTNICT DCRA Dihedral Corner Reflector micro-arraysdcra DCRA DCRA DCRA 3D DCRA PC USB PC PC ON / OFF Velleman K8055 K8055 K8055
1 1 1 2 DCRA 1. 1.1 1) 1 Tactile Interface with Air Jets for Floating Images Aya Higuchi, 1 Nomin, 1 Sandor Markon 1 and Satoshi Maekawa 2 The new optical device DCRA can display floating images in free
PowerPoint プレゼンテーション
2017 TRON Symposium 於東京ミッドタウン Open IoT:IoT 時代の人材育成産業界におけるIoT 分野の人材育成 1 Human resource development in industries for IoT applications 2017 年 12 月 14 日日本電気株式会社宇宙システム事業部 Space Systems Division, NEC Corporation
36 581/2 2012
4 Development of Optical Ground Station System 4-1 Overview of Optical Ground Station with 1.5 m Diameter KUNIMORI Hiroo, TOYOSHMA Morio, and TAKAYAMA Yoshihisa The OICETS experiment, LEO Satellite-Ground
untitled
CHAP. 1 ---------------------------------------------------------------- 5 1-1. ---------------------------------------------------------------- 5 1-2. ----------------------------------------------------------------
橡report.PDF
10 3 45 9 () Knowing Hazard Visualization of Crustal Strain in the Japanese Islands using GPS Data GPS Eric N. Oware Mitigation (SAR) (DIS) Preparedness Response & Recovery (SAR) Information Dissemination
main.dvi
A 1/4 1 1/ 1/1 1 9 6 (Vergence) (Convergence) (Divergence) ( ) ( ) 97 1) S. Fukushima, M. Takahashi, and H. Yoshikawa: A STUDY ON VR-BASED MUTUAL ADAPTIVE CAI SYSTEM FOR NUCLEAR POWER PLANT, Proc. of FIFTH
日立評論2008年1月号 : 基盤技術製品
Infrastructure Technology / Products HIGHLIGHTS 2008 HDD 2.5 HDD3.5 HDD 1 Deskstar 7K1000 HDD Hard Disk Drive 2006 5 PC 2.5 HDD HDD 3.5 HDD1 1 2007 3Deskstar 7K1000 3.5 HDD 1149 Deskstar 7K500 2 GMR Giant
3 16 2 27 4497 LAN(Local Area Network) OFDM(Orthogonal Frequency Division Multiplexing) 12 3 3 12 3 12 33. F/B 22.7dB 3 F/B i 1 1 2 3 8 2.1................................. 8 2.2.............................
Trip Trip Trip
- - - - 1999 Leonid MAC Multi-Instrument Aircraft Campaign November 8-23, 1999 1998-2002 (2001 ) Predictions, Observational Plans and Results for Leonid 1998-2002. Photo Gallery taken by Photographic Camera
光と電波による地球環境計測へのIT活用事例
IT IT Applications in Global Environment Observation Using Light and Radio Waves CRL Communications Research Laboratory IT 1998 IT Abstract Recently, there has been rising concern about global-scale environmental
- Principles for a Telecommunications management network 2.0 2001 11 27 THE TELECOMMUNICATION TECHNOLOGY COMMITTEE 2 JT-M3010 ...19...20...20...20...20...21...22...23...24 3 JT-M3010 ...26...28...29...34...34...35...35...37...37...37...37...37
特別寄稿.indd
特別寄稿 ソフトインフラとしてのデジタル地図を活用した自動運転システム Autonomous vehicle using digital map as a soft infrastructure 菅沼直樹 Naoki SUGANUMA 1. はじめに 1) 2008 2012 ITS 2) CO 2 3) 4) Door to door Door to door Door to door DARPA(
2-工業会活動.indd
工業会活動 ~SAE(Society of Automotive Engineers) 委員会参加報告 ~ 1. はじめに SAE RTCA Radio Technical Commission for Aeronautics ARINC Aeronautical Radio, Incorporated SAE RTCA ARINC FAA Federal Aviation Administration
1
5-3 Photonic Antennas and its Application to Radio-over-Fiber Wireless Communication Systems LI Keren, MATSUI Toshiaki, and IZUTSU Masayuki In this paper, we presented our recent works on development of
2章.doc
C 2 H 4 N 2 O 2 LPG LIF 13 2.1 2.1.1 2.1 2.2 115mm70mm 727cm 3 Hand Pump Injector Driver Computer Constant Volume Chamber Injector Piezo-electronic transducer Fan Spark Plug Temperature Indicator C 2 H
IPSJ SIG Technical Report Vol.2012-HCI-149 No /7/20 1 1,2 1 (HMD: Head Mounted Display) HMD HMD,,,, An Information Presentation Method for Weara
1 1,2 1 (: Head Mounted Display),,,, An Information Presentation Method for Wearable Displays Considering Surrounding Conditions in Wearable Computing Environments Masayuki Nakao 1 Tsutomu Terada 1,2 Masahiko
Newsletter Issue 16
Airbus Helicopters Japan Issue 16 2018 Oct/Nov/Dec CONTENTS 8 2016 25 550 11 28 30 2018 Japan International Aerospace Exhibition VR PRODUCT 2 H145//BK117D-2 H135 P3H H160 H125 H130 H135 H145EMS Voom SERVICE
ｽﾗｲﾄﾞ ﾀｲﾄﾙなし
DSRC 2003 9 24 ITS DSRC September 24, 2003 1 ( ) ITS 1 DSRC 2 DSRC 3. DSRC 4. DSRC 5. VSC 6 DSRC September 24, 2003 2 DSRC September 24, 2003 3 1. ETC DSRC 150 ( ) 2. ETC ITS - ETC Highway Highway Surveillance
資料1－3
WPT (2017) ( ) *JST Center of Innovation ( 13- ) Last 5X * 16 8, 15 7, 14 6 METLAB 16 20, 15 18 WPT * IEEE MTTS Wireless Power Transfer Conference ( 11-, ) MTTS TC-26 (Wireless Energy Transfer and Conversion
<30365F93C195CA8FDC5F88C092422E696E6464>
1 Sanders, G. B., William E. L., "Integration of In-Situ Resource Utilization into lunar/mars exploration through field analogs." Advances in Space Research 47, 1 2011, 20-29. 2 Sanders, G. B., William
<30345F90BC96EC90E690B65F E706466>
15 特集 国際宇宙ステーション日本実験棟 きぼう における流体実験 * Space Experiment on the Instability of Marangoni Convection in Liquid Bridge Koichi NISHINO, Department of Mechanical Engineering, Yokohama National University 1 thermocapillary
部内資料
- OERIEW OF DIGITAL SBSCRIBER LINE (DSL RECOMMENDATIONS 2.0 2002 5 30 THE TELECOMMNICATION TECHNOLOGY COMMITTEE (DSL... 4... 4... 4... 4... 4... 5... 6... 7... 8... 8... 9... 9... 9... 10... 11... 11...
専門力_総合力
Program for Leading Graduate Schools Program for Leading Graduate Schools INTRODUCTION 04 CONTENTS 10 15 23 24 30 32 33 34 36 38 39 DATA 40 42 44 Program for Leading Graduate Schools What is a DOCTOR??
TR-1341.p65
STOL 1 STOL Evaluation of STOL approach and landing of the Quiet STOL experimental aircraft ASKA Masaru NAKAMURA and Yushi TERUI Abstract The quiet STOL experimental aircraft ASKA was developed by the
3D UbiCode (Ubiquitous+Code) RFID ResBe (Remote entertainment space Behavior evaluation) 2 UbiCode Fig. 2 UbiCode 2. UbiCode 2. 1 UbiCode UbiCode 2. 2
THE INSTITUTE OF ELECTRONICS, INFORMATION AND COMMUNICATION ENGINEERS HCG HUMAN COMMUNICATION GROUP SYMPOSIUM. UbiCode 243 0292 1030 E-mail: {ubicode,koide}@shirai.la, {otsuka,shirai}@ic.kanagawa-it.ac.jp
110 JAXA JAXA / /
109 JAXA 4 1 2015 3 31 15 40 27 82 / 7/13 6/2 9/13 22/28 13 8 12 8 8 7 10 9 1 1 21 20 19 17 1988 63 2000 15 5 2 26 5 1 10 0 10 3 8 4 6 4 8 13 2 110 JAXA JAXA 9 12 80 60 40 20 / 50 40 30 20 10 / 0 0 3 18
Abstract 1 1 2 Abstract Fig. 1 Fig. 2 Fig. 3 Abstract 1 2 3 4 5 6 7 8 10 9 Abstract 1 1 2 3 4 5 6 7 8 9 Abstract 1 2 3 4 Abstract 1 1 2 2 3 4 5 6 3 7 8 9 4 Abstract 1 2 3 4 5 6 7 8 9 10
2 2. 13 2 1 1 PBS: Post-Boost Stage 1.2 2 30 JAXA 49 2 108 4 205
252 5210 3 1 1 e-mail: morita.yasuhiro@jaxa.jp 9 1. 1 F1 1 204 2015 4 2 2. 13 2 1 1 PBS: Post-Boost Stage 1.2 2 30 JAXA 49 2 108 4 205 IT IT 3 2 JAXA 2 3 1 2 2 2 3 2 206 2015 4 C/C 2 3. 3.1 1 SRB-A H2A
2
L C -60W 7 2 3 4 5 6 7 8 9 0 2 3 OIL CLINIC BAR 4 5 6 7 8 9 2 3 20 2 2 XXXX 2 2 22 23 2 3 4 5 2 2 24 2 2 25 2 3 26 2 3 6 0 2 3 4 5 6 7 8 9 2 3 0 2 02 4 04 6 06 8 08 5 05 2 3 4 27 2 3 4 28 2 3 4 5 2 2
Optical Lenses CCD Camera Laser Sheet Wind Turbine with med Diffuser Pitot Tube PC Fig.1 Experimental facility. Transparent Diffuser Double Pulsed Nd:
*1 *2 *3 PIV Measurement of Field of the Wind Turbine with a med Diffuser Kazuhiko TOSHIMITSU *4, Koutarou NISHIKAWA and Yuji OHYA *4 Department of Mechanical Engineering, Matsue National Collage of Technology,
( ) SSID)
21826 1 () 210826 767 747-400 SSID) 21826 Contents 1. 2. 3. 4. 767 5. 747-400 400 6. Contents 1. 2. 3. 4. 767 5. 747-400 6. 2 21826 1. System Structure MRB Report MPD Fig. A 1. MRB Maintenance Review Board
& Vol.5 No (Oct. 2015) TV 1,2,a) , Augmented TV TV AR Augmented Reality 3DCG TV Estimation of TV Screen Position and Ro
TV 1,2,a) 1 2 2015 1 26, 2015 5 21 Augmented TV TV AR Augmented Reality 3DCG TV Estimation of TV Screen Position and Rotation Using Mobile Device Hiroyuki Kawakita 1,2,a) Toshio Nakagawa 1 Makoto Sato
L C -6D Z3 L C -0D Z3 3 4 5 6 7 8 9 10 11 1 13 14 15 16 17 OIL CLINIC BAR 18 19 POWER TIMER SENSOR 0 3 1 3 1 POWER TIMER SENSOR 3 4 1 POWER TIMER SENSOR 5 11 00 6 7 1 3 4 5 8 9 30 1 3 31 1 3 1 011 1
英国のFunding Agency としてのResearch Councils の役割
Funding Agency Research Councils Chief Scientific Advisor Cabinet Parliament Council for Science & Technology Department of Trade & Industry Office of Science & Technology Director General of the Research
2
L C -24K 9 L C -22K 9 2 3 4 5 6 7 8 9 10 11 12 11 03 AM 04 05 0 PM 1 06 1 PM 07 00 00 08 2 PM 00 4 PM 011 011 021 041 061 081 051 071 1 2 4 6 8 5 7 00 00 00 00 00 00 00 00 30 00 09 00 15 10 3 PM 45 00
1 (5) ISAS/JAXA for the SRG SXC working group
1 (5) ISAS/JAXA for the SRG SXC working group 14 2 calendar year NeXT & SRG cooler development schedules SRG 2007 2008 2009 2010 2011 2012 basic design EM design EM fabrication & test PFM design PFM fabrication
untitled
2005 8 1...1 1.1...1 1.2...2 1.3...3 1.4...4 1.5...5 1.5.1...5 1.5.2...5 1.5.3...6 1.6...8 1.7...9 1.7.1...9 1.7.2...10 1.7.3...10 1.7.4...10 1.7.5... 11 1.8... 11 2...13 2.1...13 2.2...14 2.2.1...14
Frequently Asked Questions (FAQ) About Sunsetting the SW-CMMR
SW-CMM FAQ(Frequently Asked Questions) SEI Frequently Asked Questions (FAQ) About Sunsetting the SW-CMM The SEI Continues Its Commitment to CMMI SEI SEI SEI PDF WWW norimatsu@np-lab.com 2002/11/27 SEI
Development of Induction and Exhaust Systems for Third-Era Honda Formula One Engines Induction and exhaust systems determine the amount of air intake
Development of Induction and Exhaust Systems for Third-Era Honda Formula One Engines Induction and exhaust systems determine the amount of air intake supplied to the engine, and as such are critical elements
Neutron yield M.R. Hawkesworth, Neutron Radiography: Equipment and Methods, Atomic Energy Review 15, No. 2, , n µc -1 = n/(µa s) ~10 12 n
Cross Section 7MeV Proton Linac AFRD, LBL (courtesy of Jani Reionen) LINAC SYSTEMS Applied Pulsed Power Plasma Target D+D reaction driven by LASER Neutron yield M.R. Hawkesworth, Neutron Radiography: Equipment
2-工業会活動.indd
宇 宙 機 関 企 業 大 学 等 の 関 係 者 が 多 数 参 加 する 第 66 回 国 際 宇 宙 会 議 (66 th International Astronautical Congress 以 下 IAC2015)に 参 加 したので その 概 要 を 報 告 する 1.IAC2015の 概 要 International Astronautical Congress IAC International
三菱光デバイス
0.9 0.8 0.7 0.6 500 0.5 y 0.4 0.3 490 0.2 0.1 0.0 0.0 520 480 540 srgb CMY D65 Laser Display 560 580 600 620 700 470 460 380 0.1 0.2 0.3 0.4 x 0.5 0.6 0.7 0.8 RED [638nm] (Display System etc.) ML562G84
宇宙環境利用蛋白質結晶生成応用利用実証プロジェクトのご案内
16 8 23 1. 14 17 ISS JEM (JAXA) 2. JAXA 14 6 1 4 1 02/02/2003 29/08/2003 29/01/2004 11/08/2004 Baikonur Kazakhstan Progress 03/05/2003 28/10/2003 29/04/2004 19/10/2004 Kazakhstan Soyuz 13 weeks 9 weeks
untitled
No. JR 06-115 2003 2005 7 Record of Discussions: R/D 10 9 2006 9 APO Annual Plan of Operation BEE Black Economic Empowerment C/P Counterparts CSR Corporate Social Responsibility DFID Department for International
日立評論2009年1月号 : 社会基盤事業
14 1 21 CO 2 7 CO 2 2009.01 15 16 HIGHLIGHTS 2009 1996 2007, 21m 2 1,800 2005 2008 452007 14 1999 4 250 20003ISO14001 57 32 20032007 11% CO 2 0.60.70.9 FMSFlexible Manufacturing System 20102005 70 2 20072005
和文.PDF
No. J R 00-187 US$1.00=Rls.8,150 (2000 11 ) (i) CEST (gal) (MMI) ( ) (ii) 483,000 313,000 113,000 446,000 55% 36% 13% 51% 876,000 GDP * 22.07% 14.30% 5.16% 20.38% GDP (1998) 109 Billi. US$ 383,000
30 (Electrical Engineering I) () LED IC 1. LED, IC D () 2 2 LED 6 4 ANDORNOTEXOR : : () () () () () 1 LED, IC 2 LED, IC LED, I
30 (Information Processing I) () 2 1 2 Word Excel WordExcel 1. EXCEL,WORD 2. D () 2 10 4 2 10 2 30 : () () () () () 1 EXCEL,WORD EXCEL,WORD EXCEL,WORD EXCEL,WORD 2 30 (Electrical Engineering I) () 2 1
5b_08.dvi
, Circularly Polarized Patch Antennas Combining Different Shaped Linealy Polarized Elements Takanori NORO,, Yasuhiro KAZAMA, Masaharu TAKAHASHI, and Koichi ITO 1. GPS LAN 10% [1] Graduate School of Science
untitled
1 2 3 4 5 130mm 32mm UV-irradiation UV-cationic cure UV-cationic cure UV-cationic cure Thermal cationic Reaction heat cure Thermal cationic Cation Reaction heat cure Cation (a) UV-curing of
1 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15. 1. 2. 3. 16 17 18 ( ) ( 19 ( ) CG PC 20 ) I want some rice. I want some lice. 21 22 23 24 2001 9 18 3 2000 4 21 3,. 13,. Science/Technology, Design, Experiments,
Цифровой спутниковый ресивер Lumax DV 2400 IRD
13... 3 1.... 5 1.1 1.2... 5... 6 2.... 7 2.1 2.2 2.3... 7... 8... 9 3.... 10 3.1... 10 3.1.1 RF...10 3.1.2 SCART...11 3.2... 12 3.2.1 DISH IN...12 3.2.2 DiSEqC...13 4..... 14 4.1 0003.... 15 4.1.1...15
IP Management Within Universities: Experiences in the US
yuko.harayama@most.tohoku.ac.jp 17/3/2004 1 Ref. Sandelin TLO expertise Ref. AUTM 17/3/2004 2 Ref. Heller & Eisenberg, 1998 The scientific commons is becoming privatized! (Ref. Nelson, 2003) 17/3/2004
untitled
2004.11.18 1 3C everywhere Aoyama Morikawa Laboratory 2 3C Everywhere Computing everywhere PDA, Contents everywhere XMLmp3 1 terabyte 1 zettabyte (10 21 ) Connectivity everywhere 2G/3G/4GLAN DSL, DSRC,
Table 1: Basic parameter set. Aperture values indicate the radius. δ is relative momentum deviation. Parameter Value Unit Initial emittance 10 mm.mrad
SuperKEKB EMITTANCE GROWTH BY MISALIGNMENTS AND JITTERS IN SUPERKEKB INJECTOR LINAC Y. Seimiya, M. Satoh, T. Suwada, T. Higo, Y. Enomoto, F. Miyahara, K. Furukawa High Energy Accelerator Research Organization
IEEE HDD RAID MPI MPU/CPU GPGPU GPU cm I m cm /g I I n/ cm 2 s X n/ cm s cm g/cm
Neutron Visual Sensing Techniques Making Good Use of Computer Science J-PARC CT CT-PET TB IEEE HDD RAID MPI MPU/CPU GPGPU GPU cm I m cm /g I I n/ cm 2 s X n/ cm s cm g/cm cm cm barn cm thn/ cm s n/ cm
The Plasma Boundary of Magnetic Fusion Devices
ASAKURA Nobuyuki, Japan Atomic Energy Research Institute, Naka, Ibaraki 311-0193, Japan e-mail: asakuran@fusion.naka.jaeri.go.jp The Plasma Boundary of Magnetic Fusion Devices Naka Fusion Research Establishment,
橡
CO2 Laser Treatment of Tinea Pedis Masahiro UEDA:,' Kiyotaka KITAMURA** and Yukihiro GOKOH*** Table I Specifications 1. Kind of Laser 2. Wavelength of Lasers. Power of Laser. Radiation Mode. Pulse Duration.
RUPES BIGFOOT POLISHING SYSTEMS INNOVATIVE
RUPES BIGFOOT POLISHING SYSTEMS INNOVATIVE ROTARY GEAR DRIVEN RANDOM ORBITAL TRIPLE ACTION BIGFOOT POLISHING SYSTEMS ROTARY TRIPLE ACTION RUPES RANDOM ORBITAL GEAR DRIVEN PERFECT RESULTS BigFootBigFoot
PS
PS 3.7-2001 PS 3.7-2001 Digital Imaging and Communications in Medicine (DICOM) Part 7: Message Exchange Published by National Electrical Manufacturers Association 1300 N. 17th Street Rosslyn, Virginia
untitled
DICOM Digital Imaging and Communications in Medicine DICOM DICOM Digital Imaging and Communications in Medicine ACRNEMA CD-R DICOM 1 HIS Server PC HL7 RIS WEB Image/Report Viewer WEB RIS Server DICOM DICOM
Development and Field Test of a Portable Camera System for Long Term Observation of Natural Dam Ken AKIYAMA (Tohoku Univ.), Genki YAMAUCHI (Tohoku Uni
Development and Field Test of a Portable Camera System for Long Term Observation of Natural Dam Ken AKIYAMA (Tohoku Univ.), Genki YAMAUCHI (Tohoku Univ.), Shoya HIGA (Tohoku Univ.), Keiji NAGATANI (Tohoku
09＿理学部案内S2.indd
Okayama University Faculty of Science Okayama University Faculty of Science 2009 1 2 4 6 10 14 18 22 26 27 28 29 30 32 34 36 37 CONTENTS Okayama University Faculty of Science 1 Okayama University Faculty
GT-X980
NPD5061-00 JA ...6...10...10...11...13...15...20...21...21...22 /...23 PDF...27 PDF...31 /...35...38...43...46 EPSON Scan...49...49...49...50 EPSON Scan...51...51...52...52...53 2 Windows...53 Mac OS X...53...53...53...54...56...56...58...59...60...60...61...62...63
TH-42PAS10 TH-37PAS10 TQBA0286
TH-42PAS10 TH-37PAS10 TQBA0286 2 4 8 10 11 17 18 20 21 22 23 24 25 26 27 28 29 30 31 32 33 38 42 44 46 50 51 52 53 54 3 4 5 6 7 8 3 4 1 2 9 5 6 1 4 2 3 5 6 10 11 1 2 3 4 12 13 14 TH-42PAS10 TH-42PAS10
プラズマ核融合学会誌１１月【８１‐１１】／小特集５
Japan Atomic Energy Agency, Ibaraki 311-0193, Japan 1) Kyoto University, Uji 611-0011, Japan 2) National Institute of Advanced Industrial Science and Technology, Tsukuba 305-8569, Japan 3) Central Research
km 100 m/s moving flame Schubert and Whitehead,1969 Thompson Thompson,1970 Fels Lindzen 1974 Gierasch Gierasch, ,
Super Rotation of Venusian Atmosphere Takagi Seiko 2008 1 31 1960 1 65 km 100 m/s 243 70 moving flame Schubert and Whitehead,1969 Thompson Thompson,1970 Fels Lindzen 1974 Gierasch Gierasch,1975 1980,1982
1 1.1 PC PC PC PC PC workstation PC hardsoft PC PC CPU 1 Gustavb, Wikimedia Commons.
1 PC PC 1 PC PC 1 PC PC PC PC 1 1 1 1.1 PC PC PC PC PC workstation PC 1.1.1 hardsoft 1.1.2 PC PC 1.1 1 1. 2. 3. CPU 1 Gustavb, Wikimedia Commons.http://en.wikipedia.org/wiki/Image:Personal_computer,_exploded_5.svg
Microsoft PowerPoint - 山形大高野send ppt [互換モード]
![Microsoft PowerPoint - 山形大高野send ppt [互換モード]](/thumbs/96/127884904.jpg "Microsoft PowerPoint - 山形大高野send ppt [互換モード]")
, 2012 10 SCOPE, 2012 10 2 CDMA OFDMA OFDM SCOPE, 2012 10 OFDM 0-20 Relative Optical Power [db] -40-60 10 Gbps NRZ BPSK-SSB 36dB -80-20 -10 0 10 20 Relative Frequency [GHz] SSB SSB OFDM SSB SSB OFDM OFDM
三菱電線工業時報 第 105 号 2008 年 10 月 1 High-speed disaster prevention radio information system R-LCX50-4SL-75 LANIEEE b/g R-LCX50-4SL D 2 1
1 GHz GHz 帯長距離漏洩同軸ケーブルを用いた高速防災無線情報システムの研究開発 High Speed Communication System for Emergencies Using Long-distance GHz Leaky Coaxial Cables 長野県工業技術総合センター 国立大学法人信州大学 株式会社サーキットデザイン 加賀電子株式会社 菱星通信システム株式会社ネットワーク技術部
xx/xx Vol. Jxx A No. xx 1 Fig. 1 PAL(Panoramic Annular Lens) PAL(Panoramic Annular Lens) PAL (2) PAL PAL 2 PAL 3 2 PAL 1 PAL 3 PAL PAL 2. 1 PAL
PAL On the Precision of 3D Measurement by Stereo PAL Images Hiroyuki HASE,HirofumiKAWAI,FrankEKPAR, Masaaki YONEDA,andJien KATO PAL 3 PAL Panoramic Annular Lens 1985 Greguss PAL 1 PAL PAL 2 3 2 PAL DP
TB014 Book No BC4Z004 S N 11
TB014 Book No. BC4Z004 Serial No. 11400003- MACHINERY NAME LOWER FRAME SHOE SLIDE CRAWLER BELT TRACK ROLLER FRONT IDLER TRACK ADJUSTER (11400003-11400782) TRACK ADJUSTER (11400783-) TRAVEL DEVICE
VoIP Broadcasting System 2/2 IP Convergence Communication Solution IP paradigm Integration & Management VoIP IP VoIP VoIP IT < 02-06-12>
2003. 5. 22 AddPac Technology Proprietary VoIP Broadcasting System 2/2 IP Convergence Communication Solution IP paradigm Integration & Management VoIP IP VoIP VoIP IT < 02-06-12> 8Khz 16Khz CDMA ADSL VoIP
untitled
u-japan : HP: http://cis.k.hosei.ac.jp/~jianhua/ (Ubiquitous) (Ubiquitous) : : : : ( 1945 1975 1985 1995 2007 PC PC PC PDA, µ- chip Hitachi s RFID Chip in 2006 By Hitachi, 2003 015 0.15x0.15 015mm Integrated
258 5) GPS 1 GPS 6) GPS DP 7) 8) 10) GPS GPS 2 3 4 5 2. 2.1 3 1) GPS Global Positioning System
Vol. 52 No. 1 257 268 (Jan. 2011) 1 2, 1 1 measurement. In this paper, a dynamic road map making system is proposed. The proposition system uses probe-cars which has an in-vehicle camera and a GPS receiver.
2
L C -32D H 6 2 3 4 5 6 7 8 9 4444444444 4444444 444444444 0 2 3 OIL CLINIC BAR 4 5 6 7 88 9 2020 2 22 23 4 4 5 6 7 8 9 0 2 2424 25 26 27 2828 2 3 29 2 3030 3 3232 5 33 3434 35 3636 37 2 3838 3 2 3 2 3
VHDL-AMS Department of Electrical Engineering, Doshisha University, Tatara, Kyotanabe, Kyoto, Japan TOYOTA Motor Corporation, Susono, Shizuok
VHDL-AMS 1-3 1200 Department of Electrical Engineering, Doshisha University, Tatara, Kyotanabe, Kyoto, Japan TOYOTA Motor Corporation, Susono, Shizuoka, Japan E-mail: tkato@mail.doshisha.ac.jp E-mail:
EQUIVALENT TRANSFORMATION TECHNIQUE FOR ISLANDING DETECTION METHODS OF SYNCHRONOUS GENERATOR -REACTIVE POWER PERTURBATION METHODS USING AVR OR SVC- Ju
EQUIVALENT TRANSFORMATION TECHNIQUE FOR ISLANDING DETECTION METHODS OF SYNCHRONOUS GENERATOR -REACTIVE POWER PERTURBATION METHODS USING AVR OR SVC- Jun Motohashi, Member, Takashi Ichinose, Member (Tokyo
TK-M700…p†[…c…−…X…g
TK Tape cutter device Machine models M700 Series / TK Series Parts Catalog INTRODUCTION This parts catalog covers the TK Series device. On pages 3-12, each mechanism is arranged on facing pages, the first
Business-Higher Education Forum(BHEF) Nils Haselmo Hank McKinnell CEO Working Together, Creating Knowledge---The University-Industry Research Collabor
No.2 2002 11 Business-Higher Education Forum Business-Higher Education Forum(BHEF) Nils Haselmo Hank McKinnell CEO Working Together, Creating Knowledge---The University-Industry Research Collaboration
42 1 Fig. 2. Li 2 B 4 O 7 crystals with 3inches and 4inches in diameter. Fig. 4. Transmission curve of Li 2 B 4 O 7 crystal. Fig. 5. Refractive index
MEMOIRS OF SHONAN INSTITUTE OF TECHNOLOGY Vol. 42, No. 1, 2008 Li 2 B 4 O 7 (LBO) *, ** * ** ** Optical Scatterer and Crystal Growth Technology of LBO Single Crystal For Development with Optical Application
2-工業会活動.indd
1. はじめに I S O I n t e r n a t i o n a l O r g a n i z a t i o n f o r Standardization ISO/TC20 SC9 7 10 12 3 1 P 1 CAAC 写真 1 会議風景 21 2. 背景 SC9 IATA International Air Transport Association liaison IATA
1 158 14 2 8 00225 2 1.... 3 1.1... 4 1.2... 5 2.... 6 2.1...7 2.2... 8 3.... 9 3.1... 10 3.2... 16 4.... 17 4.1... 18 4.2... 20 4.3... 22 5.... 23 5.1... 24 5.2... 28 5.3... 34 5.4... 37 5.5... 39 6....
Nano Range Specification Stable & Stable Telescopic Resonators Model Nano S Nano S Nano S Nano S Nano L Nano L Nano L Nano L Nano L Nano L Nano L 130-
L i t r o n T o t a l L a s e r C a p a b i l i t y Nano Series Ultra Compact Pulsed Nd:YAG Lasers Product Range Specification Nano Range Specification Stable & Stable Telescopic Resonators Model Nano
MT-17J-003-a 表紙
MT-21J-003-B STP-301/451 3 -b 2002.3 Copyright 2002 Seiko Instruments Inc. All rights reserved. Printed in Japan. STP-301/451 STP STP, 1 STP-301/451 STP (MSDS Material Safety Data Sheet) ( ) MSDS STP 2
untitled
Application of image correlation technique to determination of in-plane deformation distribution of paper Toshiharu Enomae Graduate School of Agricultural and Life Sciences The University of Tokyo 1 Peters
m 1 AUV 10 m 1.3 m 1.5 m 10 tons 300 km 3,500 m 3 kn. Maximum 4 kn SSBL (, ) AUV 2,000 3,
19 pp.7-17 2006 Development of Deep Sea Cruising Autonomous Underwater Vehicle Taro Aoki Abstract The URASHIMA, a third-generation AUV (Autonomous Underwater Vehicle), can dive to a depth of 3,500 meters,
Vol.55 No (Jan. 2014) saccess 6 saccess 7 saccess 2. [3] p.33 * B (A) (B) (C) (D) (E) (F) *1 [3], [4] Web PDF a m
![Vol.55 No (Jan. 2014) saccess 6 saccess 7 saccess 2. [3] p.33 * B (A) (B) (C) (D) (E) (F) *1 [3], [4] Web PDF a m](/thumbs/92/108648363.jpg "Vol.55 No (Jan. 2014) saccess 6 saccess 7 saccess 2. [3] p.33 * B (A) (B) (C) (D) (E) (F) *1 [3], [4] Web PDF a m")
Vol.55 No.1 2 15 (Jan. 2014) 1,a) 2,3,b) 4,3,c) 3,d) 2013 3 18, 2013 10 9 saccess 1 1 saccess saccess Design and Implementation of an Online Tool for Database Education Hiroyuki Nagataki 1,a) Yoshiaki
A book
Hitachi Multi Payment Network communications server 3000-3-493-40 P-1B43-6111 Hitachi Multi Payment Network communications server Base 01-03( OS HP-UX 11.0 HP-UX 11i) P-1B43-6311 Hitachi Multi Payment
スペースプラズマ研究会-赤星.ppt
14 1 1 1 1 Pauline Faure 1 1 2 3 (1: 2: JAXA 3: IHI) IHI (C)(No.21560819) ISAS(JAXA) ISO TC20/SC14 / (Spall) 60~90% 2 (Cone) 1% (Jetting) CDV11227 Committee Draft for Comments CDV11227 Witness plate Sabot
技術創造の社会的条件
1999 10 21 21 i ... 1 1... 3 1-1. 20...3 1900 1945 3 1945 198x 4 198x 1999 5 1-2....7 1945 198x 7 HEMT 8 198x 1999 9 9 1-3....11 11 12 13 18 2 New Institutions... 21 2-1....21 22 24 26 2-2....27 28 29
HG…p†[…c…J…^…“…O
HG Hemming guide device Machine models W(T)664 Series / HG Series Parts Catalog INTRODUCTION This parts catalog covers the HG Series device. On pages 2-37, each mechanism is arranged on facing pages, the
untitled
22 23 3 1...1 1...1 2...2 3...3 4...4 2...5 1...5 2...8 3...9 1...9 2... 15 3... 17 4 US&R... 19 5 US&R... 22 6 US&R... 24 7... 26 4... 27 1... 27 2... 28 1... 28 2... 29 3... 32 4... 35 5... 37 3...
Microsoft Word - archip.doc
131 71 71 71 7 1 71 71 71 71 71 71 7 1 71 71 71 71 71 71 7-1 71 71 71 71 71 71 7-1 71 71 7 1 71 71 71 71 71 71 71 71 71 71 71 71 71 71 7 1 71 71 71 71 71 71 7 1 71 71 71 71 71 71 71 71 71 71 71 71 71 71
untitled
慣性運動計測機器 クロ ス ボ ー株 式 会 社 Crossbow Japan Ltd. MEMS 3 1 X Y Z 3 RS-232 Windows Gyro-View Nav-View GPS NAV420 3 AHRS400 VG400 6 IMU400 (AHRS) TEL: 06-6489-5922 FAX: 06-6489-5910 E-MAIL: sales@xbow.jp WEB:
研究開発評価活動の実例集 3． 6）琉球大学における評価活動について
1 / 12 ページ 2 / 12 ページ 3 / 12 ページ 4 / 12 ページ 5 / 12 ページ 6 / 12 ページ 7 / 12 ページ 8 / 12 ページ 9 / 12 ページ 資料 1 A dministrative Structure Chart M anagement C ouncil I nspector Pr esident B oar d of C ouncil C