学科課程カリキュラム 及び 授 業 計 画
Contents
1.2.
3. 4
4. 1
5. f 4
6. 1 1
7. 3878 I Flight Operating Engineering 1
8. 3 E MTTF MTBF
9. E 1 2 3
10. 1 2 I 3 T 4 5 6 7 I 8
11. 3157 T Stochastics II 4 2 1 2 1
12. 1 2 3 Q 4 5 3 6 7
13. 2 3 36 3551 Introduction to Space Science 1 2
14. 4 2 2
15. 1 2 ISA 3 4 5 6
16. 1 2 3 4 Q 5 6 7 8 5
17. 1 2 3 4 5 6 7 8
18. 2 1 CAD CAD 1 Undo Redo 2 E 1 3 E 4 E
19. NN CELSS H
20. 3 3 3 1 2
21. 1 2 3 1 4 2 5 1 6 2 7 3 8 4 9 Q 3
22. 0921 Computer Hiteracy 1 1
23. 8 3 1 TI DC DC DC NB DC
24. 1 1 1 Vn Q 1 1 3 4
25. 2 2 4 1 1 Q 2 2 8 3 4 4 5 5 6
26. 3 T 31 3869 TI Strength of Aircraft Structures II 4 2
27. 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15
28. 7 779 7 4 2 5
29. 120 44 44 40 99 4 124 TA Department of Aeronautical Engineering A1 Aeronautical Engineering Course A2 Astronautical Engineering Course A3 Aircraft Maintenance Course A4 Flight Operation Course 3153 Complex analysis
30. 2 1 3 2 4 1 5 2 6 7 8 9 1 10 2 11 1 12 2
31. 1 2 1 1 1 2 1 3 2 3 4 5 6 7 8 9
32. 3 1 1 2 2 0 3 SI 4 1 3 1
33. TV ISDN WWW E
34. E ze 1 2
35. KA 1 1 2 2 3 3 4 4 5 5 6 1 7 8 9 1
36. B f T 32 3451 Bngineering Thermodynamics 2 2 M 0 2
37. o amt dm IO 1 TR Tw TR CNC CNC 4 1 M M Ed 4 Eb a N ET ET EE 3
38. 1 2 PDCA 3 4 1 5 6 7 8
39. 1 2 3 4 1 2 5 E
40. 5 1 1 1 2 2 2 3 4 5 1 6 2 Pg 3 8 9 2 10 1 1 1 2 13 1 4 1 1 5 2
41. 3 3 1 2 3 4 3 5 6 3 7 8 9 A 10 11 12 8 13
42. Navigation Log 1 2 3 4 FIR 5 RNAV 6 SVFR 8
43. 4 60 100 20 20 90 80 90 70 809 609 70 609 10 60 0711 Differential equation E 2 1 2 1
44. DC MPD MPD MPD Rocket Propulsion Elements GPSutton John Wiley amp Sons 2 3 40 3539 Heat Transfer
45. Java 7 n Java Application 7 nr Java Java Java Java else 7 4 new 4 Java 2 7 Java API Java API Java
46. CAD 1 2 3 4 5 6 7 8 9 Design of Liquid Propellant Rocket Engines D K Huzel NASA SP 123 H H 52
47. Nd 64 3883 Al Internship 3 2
48. 4 E 4 E JH TS 43 Systems Engineering 4 2 9
49. 1 SI 2 1 3 2 4 3 5 H 6 1 7 2 8 1 H 9 4 2 10 1
50. 3870 Engine run for multi engine aircraft 3 1 2 1 2 95 B55 2 4 95 BS5 a 95 B55 6 9 5 BSS
51. l sl 1 B 46 Drawing Technology
52. 1 2 3 4 5 9 7 8 9 10 3 11 3 12 1
53. 3452 Applied Engineering Thermodynamics 2 2 p h 1 1 2 2 3 3
54. 45 3758 Design of machine elements H CAD 1
55. 1 2 3 PA 28 150 4 PA 28 150 5 PA 28 150 6 PA 28 150 7 8 9 10 11 12 13 14 15 62
56. X X X 1I SS J EM MTTF 2 3 4 5 6 7 8 9 2 3 38 3557
57. 1 2 3 4 5 6 7 8 9 E
58. 4 1 2 8 a 1
59. 58 3880 Flight Operating Engineering I 4 1 Tt FAA 3 3 p3 1 ICAO 2
60. 1 2 3 4 1 5 2 6 3 7 8 9 5 6 10 11 12 1 13 I 14 1
61. 2 2 gt CA 3 D ID 53 3875 I
62. 20 ZFSC FSC 21 3 22 23 24 SD STAR 25 ADF VOR DME 26 WX MINIMA 27 NAVIGATION LOG VER Fisht Log 28 NAVIGATION LOG VER Flight Log 29 30 AIM J
63. 55 8877 4 1 1 3 1 5 7 9 11 13
64. E TT 1 2
65. 3753 CAD CAD exercises 2 1 CAD CAD CAD 1 1 e 2 2 3 3 4 1 F V 5 2 U U 2 6 3 7 8 5 9 6 3
66. 2 Windows 3 IME Input Methods Editoyy 4 Word 5 6 Q Excel 7 8 3 9 PowerPoint 10 Access 11 1 Word
67. 7 2 1 2 PowerPoint 66 0985 Marketing Theory 2 2
68. 1 2 1 3 2 4 1 5 2 6 3 7 1 8 2 9 3 10 4 11 1 12 2 13 3 14 4
69. QA TQM QC7 H 44 3662 Reliability Engineering 4
70. 26 3367 Engineering Materials for Aerospace 1 2
71. 3 SWOT 4 2 SWOT 5 3 6 7 5 8 1 4 P 9 2 10 3 11 4 12 5 13
72. 5 Rn 3 3 8 Rh 3 E 1 21 3255 Basic Aerodynamic theory 3
73. 3 4 1 1 2 1 2 f 1 E i i
74. 1 1 E JIS T SO V 5
75. 20 1 3 2 5 lg O 4 TL JAVA 3261 2 3262 I 2 3 3263 IL 2 QO 32
76. 8 9 10 11 12 18 1 18 Aircraft Dynamics II
77. 11 2 12 1 13 2 14 15 f 1 41 3651 Control system analysis 3 2
78. 9 10 11 12 13 14 15 16 17 AIP 18 OAT ICAO 19
79. 14 I TT 1 15 1 1 MBA 2 MEBA 67
80. 6 t B JIS 48 3752 CAD CAD Hiteracy
81. 7 8 9 1 10 2 11 3 12 CHECK LIST ATIS 13 ATIS 14 NOTAM AIP 15 16 17 18 19
82. 5 6 1 2 7 9 1 9 2 10 2 1 12 13 15 H H 42
83. 4 5 6 7 8 9 2 10 3 11 12 5 13 14 15
84. 4 Conrol system design 3 2 3 E 4 k 1 1 g i
85. 0921 Computer literacy 1 16 1 PowerPoint 17 18 Word 19 20 Excel
86. 1 1 2 2 3 3 4 H 5 6 7 8 3 9 ohmsha 29 3362 II Strength of Materials IL 3 2
87. H 25 3264 2 HHE Introduction of Helicopter Dynamics 4 2 LL 3 H E E
88. 1 1 3 6 1 1 7 1 1 9 5 7 5 7 10 2 11 2 12 2 13 1 0 1 2 1 0 1 2
89. 34 3455 Propulsion Engineering 3 2
90. 9 10 11 12 13 14 15 1 3160 Engineering Mechanics 1 2 2 4
91. 1 3 h 1
92. 1 2 E 1 2 3
93. 3 2
94. 2 VC VP TCPIP7r WWW _ 15 0924 JAVA m Java Programming 3 4 2
95. 2 4 4 3 3 23 H Compressible Aerodynamic Theory H
96. 3 4 6 7 VMC 8 9 10 11 12 G 13 14 15 AIM 59 3881
97. 7 np Java HTML Java Applet Java Applet Random 22 Applet 7 nm Java 500 SCC Java 16 3261 Introduction of Aircraft Dynamics 1 2
98. 13 14 15 Pt 3159 2 7 Vector analysis and Fourier series E 2
99. 5 6 7 8 9 Q 10 11 1 2 12 13 14 15 1 1 f 14 Computer Network 3 2 ISDN
100. 7 8 9 10 11 12 13 14 15 1 63 3871 Workshop Pactice 4 2
101. Java Java Java Java VM OS Java E Java 7 nm 5 Java 7 7 pm Java 7 nm 77 7 7
102. I 1 2 3 4 5 1 6 2 t 7 3 F 8 1 9 2 10 11 12 1 13 2
103. Meteorological Engineering 3 METAR TAF 1 2 3
104. 2 8 4 5 1 6 2 t 7 3 T 8 1 9 2 10 11 12 1 13 2 E 14 3 15 1 1
105. 2 8 4 5 6 7 8 9 10 11 12 18 14 15 16 17 18 19 20 21 22 28
106. O 3 1 Solid Works 50 3760 Preliminary Airplane Design 4 1 CAD 1
107. 7 2 8 1 9 2 10 1 1 1 2 1 2 13 2 2 14 3 1 15 3 2 SNR AN 22 Viscosity Aerodynamic Theory
108. 4 5 1 3 F 6 2 7 3 8 4 9 5 10 11 1 12 2 13 3 1 4 4 15 JIS 47 3751 Aircraft Basic Drafting Technology
109. 14 3 15 1 3158 Electrric Engineering 2 2 b 3
110. 1 H Rocket Propulsion Elements GPSutton John Wiley Sons 2 3 39 3558 Electric Propulsion 3 f
111. 15 1 1 H Ts 2 3 35 3454 Jet Engine E 3 2
112. 3 1 E 2 Wtlo We Wf 6 3 Wo We Wf 7 Wo We Wf 8 CAD CAD 3 CAD 3 1 CAD 3
113. 4 5 6 7 8 SS 9 10 11 12 13 14 EE 15 16 RVR 17 18 tw METAR SPECI 3 TREND RMK SCAN METAR to METAR Wn METAR
114. 1 2 2 PHS TP ISDN 1 ISDN ISDN 2 I MMOG OR X 25 1 CIR
115. 1 2 24 3258 4 2
116. MTBF MTBF x MTBF FMEA FMEA FTA FTA 0C DR ISO IS09000
117. 9 Q Q gt 3 Q ohmsha 30 3868 1 Strength of Aircraft Structures 3
118. TAF TAF le na ln ln ln Nn ln xn ln PIREP SIGMET 29 30 AIM J T 60 3882 Aeronautical Radio Operation Engineering 2 1
119. 9 17 1 Aircraft Dynamics I 2 2
120. 21 Excel 22 Excel Excel 23 Excel Excel 24 Excel 25 Excel Excel Excel Excel VBA Visual Basic E 13 0922 1 Information literacy 2 2
121. 3 Hy ul 2 1 2 1 3 2 4 5 2 6
122. 12 2 13 3 14 1 Excel 15 3 E HH HT 12
123. 4 9 3 I 2 3 1 3 4 6 H 20 3254 Transient Response of Aircr
124. 4 4 5 1 4 1 4 6 7 8 6 7 6 7 9 1 10 2 11 12 su 13 9 1 2 12 14 15 f
125. 6 1 5 5 7 1 6 8 1 7 9 1 8 10 1 9 9 11 1 10 12 1 11 13 1 14 2 15 1 1 11
126. RLC 1 3156 I Stochastics I
127. CAD BH 3 Aircraft Design Preliminary sizing of Airplanes DAR corporation Dr Jan Roskam CAD 51 3761 Preliminary Rocket Design 4 1 E
128. 3 1 1 2 1 1 8 1 2 4 1 3 5 1 4 1
129. 13 3 14 1 15 27 HH Foundations for Mechanics of Materials 2 2
130. 15 1 3154 Complex number and matrix computation 2 2
131. 29 30 30 9 5 7 3 54 3876 3 3 2 4
132. 3 5 E 6 E 7 8 Ei 3 Auto CAD LT B 49
133. 6 7 7 8 8 9 9 10 10 11 11 12 12 13 13 14 14 15 1 15 16 16 Q 17 17 18 18 3 19 19 4 20 20 21 21 1 22 22 H 23 23 24 24 25 25 26 26 TPC 27 27 28 28 29 3
134. 65 0934 Theory of Venture Business 3 2
135. E 2 2 2 3 4 1
136. 19 3253 Fundamentals of Flight Dynamics 4 S 1 IT 1
137. 1 2 E 28 1 Strength of Materials 1 2
138. 14 1 15 1 ul H 2 3 ul 33
139. 18 1 19 19 19 2 20 20 20 21 21 21 22 1 22 22 23 23 23 24 1 24 24 25 2 25 1 25 26 26 26 27 2 27 1 27 28 1 28 28 29 2 29 3 29 30 4 30 5 30 6 3 10 2
140. 20 21 22 23 24 25 S 26 SHORT FIELD SOFT FIELD 27 28 ADF VOR DME ILS 29 57 3879 II Flight Operating Engineering IT 3
141. Experiments in Aeronautical Engineering 0 6 3 E
142. 1 1 2 2 2 1 3 8 ADEVORJILSDME 8 4 1 4 ATCIRSRADAR 4 3 5 2 5 5 4 6 3 6 6 1 7 7 7 2 8 8 8 3 9 9 ACARS 9 4 10 10 10 11 11 FMS 11 12 12 PMS 12 13 13 ILS 13 1 14 14 14 2 15 1 15 2 15 3 16 Q 16 16 17 17 17 18 18
143. 24 I 25 I 26 27 28 I 29 I 380 61 3869 Engine run for single engine aircraft 3 1 3 1 1
144. 2 3 37 3552 Imtroduction to Space Engineering 2 2 Du
145. 3 2 2 2
146. Rocket Engine 3 2 2 EE 1
147. 15 1 17 19 21 23 25 27 29 1 2 Q 4 6 8 1 10 12 14 16 18 20 1 922 24 26 28 2 30 2 56
148. 2 3 1 6 gt E
149. 53 2 3 3254 2 10 3255 2 3256 2 QO 3257 2 QO RTR TR RR RTR TIR ITIRIR RTR TRIRIR RTIRIRIRIRIR 1 II MTR RIR RIR RTRIR CAD B 4 1 I I I I
150. aft 4 2 2 4 3
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