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unit_number
int64
1
100
time_cycles
int64
1
525
setting_1
float64
-0.01
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setting_2
float64
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setting_3
float64
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100
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float64
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519
s_2
float64
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645
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float64
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float64
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1.44k
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float64
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s_6
float64
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s_7
float64
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float64
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float64
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float64
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float64
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float64
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float64
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float64
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float64
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float64
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s_17
int64
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int64
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float64
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float64
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float64
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24
RUL
int64
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4
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5
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100
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1
6
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100
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7
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8
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100
39.05
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251
1
9
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100
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392
2,388
100
38.99
23.4693
250
1
10
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100
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1
11
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12
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100
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13
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100
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14
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390
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100
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15
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100
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100
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244
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16
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17
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47
521.98
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100
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18
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19
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20
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21
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22
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23
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24
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25
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26
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27
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28
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29
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30
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100
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229
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31
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32
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33
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34
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35
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36
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40
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43
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48
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49
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50
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51
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52
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100
38.96
23.4014
203
1
57
-0.0024
-0.0003
100
518.67
642.47
1,586.13
1,396.03
14.62
21.61
554.29
2,387.97
9,074.48
1.3
47.11
522.14
2,387.99
8,148.7
8.3816
0.03
391
2,388
100
39
23.4644
202
1
58
-0.0043
-0.0001
100
518.67
641.98
1,587.55
1,402.61
14.62
21.61
553.84
2,387.98
9,068.44
1.3
47.17
521.89
2,388.05
8,148.44
8.4089
0.03
393
2,388
100
39.2
23.353
201
1
59
0.0002
-0
100
518.67
642.01
1,589.14
1,405.41
14.62
21.61
554.48
2,387.96
9,066.73
1.3
47.24
522.84
2,388.01
8,151.41
8.4339
0.03
393
2,388
100
38.98
23.4888
200
1
60
-0.0001
-0.0003
100
518.67
642.52
1,578.91
1,406.32
14.62
21.61
554.16
2,388.03
9,069.03
1.3
47.31
522.32
2,387.98
8,148.29
8.3837
0.03
392
2,388
100
38.99
23.3179
199
1
61
0.003
-0.0004
100
518.67
641.97
1,584.13
1,400.11
14.62
21.61
554.09
2,388.01
9,075.7
1.3
47.23
522.28
2,387.98
8,152.04
8.3578
0.03
391
2,388
100
39.19
23.4228
198
1
62
0.0031
-0.0004
100
518.67
642.47
1,593.91
1,397.99
14.62
21.61
554.15
2,388.04
9,067.62
1.3
47.25
522.33
2,388.02
8,150.95
8.4285
0.03
390
2,388
100
38.91
23.3841
197
1
63
0.0008
-0.0002
100
518.67
641.82
1,583.91
1,403.75
14.62
21.61
554.73
2,388.01
9,065.3
1.3
47.32
522.76
2,388.04
8,151.24
8.3982
0.03
391
2,388
100
38.98
23.4328
196
1
64
-0.0006
0.0002
100
518.67
642.49
1,589.38
1,399.53
14.62
21.61
554.89
2,388
9,072.87
1.3
47.34
522.81
2,387.98
8,146.73
8.4168
0.03
391
2,388
100
38.92
23.3717
195
1
65
-0.0035
-0.0003
100
518.67
642.15
1,589.05
1,391.23
14.62
21.61
554.01
2,387.96
9,068
1.3
47.31
522.59
2,387.97
8,153.43
8.398
0.03
391
2,388
100
39.07
23.4992
194
1
66
0
-0.0002
100
518.67
642.16
1,586.02
1,397.9
14.62
21.61
554.5
2,387.97
9,072.46
1.3
47.36
521.68
2,387.99
8,147.89
8.4487
0.03
391
2,388
100
39.03
23.2868
193
1
67
0.0005
0
100
518.67
642.01
1,585.57
1,399.69
14.62
21.61
554.3
2,388.03
9,072.09
1.3
47.36
521.77
2,388.03
8,152.11
8.4355
0.03
391
2,388
100
38.79
23.2883
192
1
68
0.0006
-0.0005
100
518.67
642.07
1,580.92
1,401.99
14.62
21.61
554.2
2,388.04
9,072.69
1.3
47.35
521.81
2,387.95
8,142.59
8.4185
0.03
391
2,388
100
38.97
23.4363
191
1
69
0.0002
0.0001
100
518.67
642.88
1,589.68
1,399.78
14.62
21.61
553.99
2,388.05
9,068.54
1.3
47.11
522.55
2,388.05
8,153.08
8.4486
0.03
392
2,388
100
39.07
23.3217
190
1
70
-0.002
-0.0005
100
518.67
642.34
1,591.65
1,401.42
14.62
21.61
554.43
2,388.02
9,071.32
1.3
47.26
522.22
2,388.05
8,148.04
8.4294
0.03
393
2,388
100
39.14
23.3813
189
1
71
0.0032
0.0004
100
518.67
642.58
1,583.72
1,397.76
14.62
21.61
553.97
2,388.03
9,073.21
1.3
47.19
522.21
2,387.98
8,145.76
8.4168
0.03
391
2,388
100
39.13
23.4798
188
1
72
0.0012
0.0002
100
518.67
641.91
1,582.17
1,402.51
14.62
21.61
554.38
2,388.02
9,076.78
1.3
47.26
522.23
2,388.06
8,144.3
8.4528
0.03
392
2,388
100
39.04
23.3875
187
1
73
-0.0004
-0.0004
100
518.67
642.02
1,586.87
1,397.72
14.62
21.61
554.42
2,388.04
9,073.4
1.3
47.34
522.23
2,388.03
8,148.12
8.4825
0.03
393
2,388
100
39.05
23.3951
186
1
74
-0.0004
-0.0001
100
518.67
641.86
1,583.99
1,399.91
14.62
21.61
554.14
2,388.01
9,065.14
1.3
47.22
522.22
2,388.01
8,151.44
8.428
0.03
393
2,388
100
39.02
23.3814
185
1
75
-0.001
0.0004
100
518.67
642.22
1,587.16
1,396.3
14.62
21.61
553.64
2,388
9,064.8
1.3
47.19
522.32
2,387.98
8,150.37
8.3836
0.03
393
2,388
100
39.02
23.4318
184
1
76
0.0017
-0
100
518.67
642.85
1,586.17
1,400.01
14.62
21.61
554.37
2,387.98
9,068.07
1.3
47.15
522.64
2,388.02
8,155.63
8.4061
0.03
392
2,388
100
38.77
23.3529
183
1
77
-0.0072
-0.0001
100
518.67
642.02
1,581.99
1,399.58
14.62
21.61
554.14
2,388
9,070.8
1.3
47.29
521.91
2,388.08
8,148.31
8.3727
0.03
391
2,388
100
38.96
23.3415
182
1
78
-0
0.0001
100
518.67
642.86
1,578.35
1,400.19
14.62
21.61
554.23
2,388.01
9,074.23
1.3
47.22
522.15
2,388.09
8,153.43
8.4288
0.03
391
2,388
100
38.88
23.4148
181
1
79
0.0008
0.0003
100
518.67
642.03
1,583.5
1,400.42
14.62
21.61
553.98
2,388.02
9,070.53
1.3
47.08
522.01
2,388.03
8,150.68
8.3895
0.03
391
2,388
100
38.99
23.4047
180
1
80
0.0028
0.0003
100
518.67
641.53
1,586.62
1,393.1
14.62
21.61
554.63
2,388.01
9,067.76
1.3
47.22
521.93
2,387.98
8,153
8.408
0.03
393
2,388
100
38.85
23.458
179
1
81
0.0021
0
100
518.67
642.13
1,581.98
1,402.49
14.62
21.61
553.72
2,388.02
9,070.82
1.3
47.02
522.32
2,388.06
8,153.66
8.4433
0.03
394
2,388
100
38.94
23.4212
178
1
82
-0.0018
-0.0005
100
518.67
642.55
1,587.08
1,402.42
14.62
21.61
554.5
2,388.02
9,064.56
1.3
47.19
522.19
2,388.05
8,151.48
8.4196
0.03
393
2,388
100
39.12
23.3853
177
1
83
-0.0053
-0.0004
100
518.67
641.85
1,587.23
1,401.86
14.62
21.61
555.2
2,388.01
9,063.6
1.3
47.25
521.93
2,388.04
8,152.49
8.3843
0.03
393
2,388
100
39
23.3097
176
1
84
0.0035
0.0001
100
518.67
641.94
1,585.55
1,398.99
14.62
21.61
554.75
2,388.03
9,066.72
1.3
47.27
521.97
2,388.07
8,153.01
8.3854
0.03
390
2,388
100
38.98
23.3584
175
1
85
0.0003
-0.0004
100
518.67
642.57
1,587.23
1,399.21
14.62
21.61
553.87
2,388.02
9,070.36
1.3
47.43
522.11
2,388.04
8,149.97
8.4385
0.03
395
2,388
100
38.96
23.4284
174
1
86
-0.0012
0.0003
100
518.67
642.07
1,590.38
1,403.18
14.62
21.61
554.77
2,388.02
9,065.76
1.3
47.34
522.02
2,387.96
8,145.53
8.4299
0.03
393
2,388
100
38.88
23.4409
173
1
87
-0.004
0.0001
100
518.67
642.27
1,584.76
1,399.41
14.62
21.61
553.7
2,388.05
9,066.48
1.3
47.46
521.75
2,388.05
8,155.21
8.4388
0.03
392
2,388
100
39.02
23.4712
172
1
88
0.0006
0.0004
100
518.67
641.46
1,587.88
1,396.91
14.62
21.61
553.85
2,387.99
9,067.25
1.3
47.23
522.05
2,388.01
8,145.17
8.4211
0.03
392
2,388
100
39.08
23.3099
171
1
89
0.0001
-0.0002
100
518.67
642.67
1,593.73
1,406.77
14.62
21.61
555.48
2,388.06
9,069.17
1.3
47.18
522.79
2,388.02
8,149.34
8.4099
0.03
392
2,388
100
38.88
23.4671
170
1
90
-0.0011
-0.0002
100
518.67
642.33
1,581.98
1,398.82
14.62
21.61
554.22
2,388.03
9,077.2
1.3
47.34
522.08
2,387.99
8,153.72
8.3848
0.03
392
2,388
100
39.03
23.3154
169
1
91
-0.002
-0.0004
100
518.67
642.58
1,592.53
1,406.11
14.62
21.61
554.64
2,388.02
9,063.78
1.3
47.37
522.34
2,388.05
8,144.94
8.3901
0.03
394
2,388
100
38.92
23.3784
168
1
92
0.0016
-0.0004
100
518.67
641.88
1,587.25
1,398.36
14.62
21.61
553.74
2,388
9,076.64
1.3
47.32
522.04
2,387.98
8,140.49
8.3986
0.03
393
2,388
100
38.92
23.3472
167
1
93
0.0019
-0.0001
100
518.67
642.59
1,581.57
1,403.57
14.62
21.61
554.65
2,388.05
9,074.6
1.3
47.43
522.15
2,388
8,152.64
8.3652
0.03
392
2,388
100
38.95
23.3151
166
1
94
0.0029
0.0002
100
518.67
642.7
1,585.22
1,394.97
14.62
21.6
554.19
2,387.97
9,071.37
1.3
47.09
522.4
2,388.02
8,151.88
8.3962
0.03
392
2,388
100
38.9
23.247
165
1
95
0.0027
-0.0001
100
518.67
642.8
1,577.32
1,406
14.62
21.61
554.29
2,388.02
9,067.45
1.3
47.31
522.18
2,388.02
8,150.69
8.4321
0.03
392
2,388
100
38.93
23.3817
164
1
96
-0.0028
0.0003
100
518.67
642.12
1,587.08
1,398.42
14.62
21.61
553.97
2,388.04
9,066.45
1.3
47.36
522.14
2,388.05
8,152.69
8.4205
0.03
393
2,388
100
38.78
23.4411
163
1
97
0.0007
-0.0004
100
518.67
642.22
1,584.55
1,388.13
14.62
21.61
554.57
2,388.07
9,066.66
1.3
47.45
522.43
2,388.05
8,145.15
8.4114
0.03
392
2,388
100
38.85
23.363
162
1
98
-0.0009
0.0003
100
518.67
642.17
1,583.35
1,402.22
14.62
21.61
553.88
2,388.1
9,069.55
1.3
47.34
522.14
2,388.02
8,152.62
8.4121
0.03
393
2,388
100
39.08
23.4234
161
1
99
0.0012
0.0003
100
518.67
642.83
1,584.77
1,402.31
14.62
21.61
554
2,388.04
9,070.04
1.3
47.22
522.13
2,388.08
8,153.16
8.4409
0.03
393
2,388
100
38.93
23.3767
160
1
100
0.0011
0
100
518.67
642.11
1,582.26
1,402.79
14.62
21.61
553.71
2,388.01
9,065.77
1.3
47.52
521.92
2,387.99
8,151.54
8.4052
0.03
392
2,388
100
39.09
23.382
159

CMAPSS Jet Engine Simulated Data FD003 - NASA

This dataset contains simulated data from the CMAPSS (Commercial Modular Aero-Propulsion System Simulation) Jet Engine by NASA, FD003.

Train trjectories: 100 Test trajectories: 100 Conditions: ONE (Sea Level) Fault Modes: TWO (HPC Degradation, Fan Degradation)

Sensor Descriptions

Sensor ID Description Units
s_1 Total temperature at fan inlet ◦R
s_2 Total temperature at LPC outlet ◦R
s_3 Total temperature at HPC outlet ◦R
s_4 Total temperature at LPT outlet ◦R
s_5 Pressure at fan inlet psia
s_6 Total pressure in bypass-duct psia
s_7 Total pressure at HPC outlet psia
s_8 Physical fan speed rpm
s_9 Physical core speed rpm
s_10 Engine pressure ratio (P50/P2) -
s_11 Static pressure at HPC outlet psia
s_12 Ratio of fuel flow to Ps30 pps/psia
s_13 Corrected fan speed rpm
s_14 Corrected core speed rpm
s_15 Bypass Ratio -
s_16 Burner fuel-air ratio -
s_17 Bleed Enthalpy -
s_18 Demanded fan speed rpm
s_19 Demanded corrected fan speed rpm
s_20 HPT coolant bleed lbm/s
s_21 LPT coolant bleed lbm/s

Units Explanation

  • ◦R: Rankine scale
  • HPT: High Pressure Temperature
  • LPT: Low Pressure Temperature
  • HPC: High Pressure Chamber
  • LPC: Low Pressure Chamber
  • rpm: rotation per minute
  • psia: pound per square inch
  • pps: pulse per second
  • lbm: pound mass

Source

CMAPSS Jet Engine Simulated Data

Citation

@article{Saxena2008DamagePM,
  title={Damage propagation modeling for aircraft engine run-to-failure simulation},
  author={Abhinav Saxena and Kai Goebel and Donald C. Simon and Neil H. W. Eklund},
  journal={2008 International Conference on Prognostics and Health Management},
  year={2008},
  pages={1-9},
  url={https://api.semanticscholar.org/CorpusID:206508104}
}
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