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LucasThil
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nasa_turbofan_degradation_FD004

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100K - 1M
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unit_number
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9.35
13.61
333.13
2,323.69
8,713.43
1.07
44.08
313.51
2,387.8
8,052.98
9.189
0.02
362
2,324
100
24.42
14.5716
265
1
57
0.0015
0.0008
100
518.67
642.24
1,572.87
1,401.95
14.62
21.58
551.39
2,387.33
9,034.22
1.3
47.08
518.82
2,387.35
8,121.79
8.4091
0.03
391
2,388
100
38.76
23.2879
264
1
58
42.0047
0.84
100
445
549.06
1,341.57
1,106.69
3.91
5.7
138.78
2,211.87
8,305.27
1.02
41.75
130.18
2,387.96
8,076.8
9.3639
0.02
327
2,212
100
10.54
6.275
263
1
59
24.9987
0.6209
60
462.54
536.57
1,251.72
1,035.54
7.05
9.01
174.73
1,915.23
8,003.35
0.93
36.48
163.88
2,028.13
7,868.12
10.8975
0.02
305
1,915
84.93
14.34
8.5356
262
1
60
20.0033
0.7007
100
491.19
606.79
1,476.45
1,236.52
9.35
13.62
333.23
2,323.68
8,711.42
1.07
44.15
313.04
2,387.8
8,056.63
9.2197
0.02
362
2,324
100
24.26
14.7787
261
1
61
35.0027
0.84
100
449.44
555.26
1,358.23
1,112.98
5.48
7.97
194.11
2,222.82
8,338.06
1.02
41.44
182.03
2,387.88
8,060.79
9.2936
0.02
333
2,223
100
14.68
9.0174
260
1
62
42.0028
0.841
100
445
549.01
1,344.57
1,111.48
3.91
5.7
137.91
2,211.9
8,312.01
1.01
41.7
129.38
2,387.95
8,078.08
9.3956
0.02
329
2,212
100
10.59
6.3125
259
1
63
0.0026
0
100
518.67
642.41
1,574.98
1,388.29
14.62
21.57
550.74
2,387.57
9,037.5
1.3
46.95
519.63
2,387.56
8,120.54
8.4093
0.03
390
2,388
100
38.83
23.3222
258
1
64
9.9987
0.25
100
489.05
603.91
1,492.47
1,295.89
10.52
15.47
392.92
2,318.69
8,768.53
1.26
45.03
370.33
2,387.88
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0.03
370
2,319
100
28.66
17.2008
257
1
65
0.0002
0.001
100
518.67
641.68
1,576.52
1,391.43
14.62
21.58
552.7
2,387.96
9,047.17
1.3
46.91
521.18
2,387.92
8,126.44
8.3885
0.03
389
2,388
100
39.06
23.4061
256
1
66
42.0043
0.84
100
445
549.25
1,338.23
1,115.55
3.91
5.69
137.76
2,211.91
8,309.32
1.01
41.64
129.91
2,388
8,070.94
9.3859
0.02
327
2,212
100
10.65
6.303
255
1
67
35.0054
0.84
100
449.44
555.43
1,351.45
1,109.9
5.48
7.98
193.43
2,222.81
8,339.26
1.02
41.55
182.41
2,387.89
8,062.45
9.3215
0.02
333
2,223
100
14.9
9.0315
254
1
68
0.0001
0
100
518.67
641.78
1,581.16
1,390.67
14.62
21.58
552.27
2,387.91
9,044.67
1.3
46.91
520.44
2,387.95
8,130.78
8.4128
0.03
392
2,388
100
39.14
23.4225
253
1
69
0.0008
0
100
518.67
641.46
1,579.82
1,390.55
14.62
21.59
553.15
2,387.96
9,053.86
1.3
47.14
520.54
2,387.93
8,129.57
8.4031
0.03
391
2,388
100
39.06
23.3688
252
1
70
41.9999
0.8414
100
445
548.58
1,344.66
1,117.54
3.91
5.7
137.96
2,211.94
8,311.46
1.02
41.72
130.09
2,388.03
8,078.86
9.3526
0.02
329
2,212
100
10.57
6.3225
251
1
71
10.0061
0.25
100
489.05
603.79
1,491.5
1,300.18
10.52
15.46
393.13
2,318.68
8,762.49
1.26
44.93
370.13
2,387.85
8,123.16
8.6166
0.03
367
2,319
100
28.65
17.2694
250
1
72
42.0007
0.84
100
445
548.97
1,351.21
1,112.23
3.91
5.7
138.63
2,211.95
8,308.92
1.02
41.76
129.71
2,387.99
8,078.28
9.3343
0.02
328
2,212
100
10.68
6.431
249
1
73
34.9996
0.8401
100
449.44
554.68
1,354.64
1,124.58
5.48
7.98
193.48
2,222.83
8,334.68
1.02
41.52
182.67
2,387.85
8,058.77
9.3464
0.02
331
2,223
100
14.88
8.9067
248
1
74
19.9997
0.7002
100
491.19
606.46
1,481.83
1,239
9.35
13.61
332.58
2,323.72
8,709.37
1.07
44.19
312.94
2,387.8
8,053.3
9.2153
0.02
363
2,324
100
24.38
14.725
247
1
75
10.0057
0.25
100
489.05
604.12
1,497.28
1,290.6
10.52
15.46
394.29
2,318.67
8,772.98
1.26
44.66
370.84
2,387.85
8,120.32
8.6157
0.03
367
2,319
100
28.58
17.2542
246
1
76
20.0005
0.7007
100
491.19
606.66
1,474.37
1,230.09
9.35
13.61
332.67
2,323.7
8,724.32
1.07
43.85
312.88
2,387.89
8,053.53
9.1911
0.02
363
2,324
100
24.48
14.7474
245
1
77
41.9999
0.8409
100
445
548.65
1,341.13
1,109.07
3.91
5.69
138.25
2,211.9
8,301.9
1.01
41.76
129.83
2,387.96
8,072.08
9.3752
0.02
330
2,212
100
10.5
6.3132
244
1
78
42.0033
0.8413
100
445
549.59
1,339.95
1,115.48
3.91
5.69
138.12
2,211.94
8,310.39
1.02
41.64
129.83
2,387.92
8,075.21
9.3775
0.02
328
2,212
100
10.36
6.3782
243
1
79
42.0033
0.84
100
445
549.69
1,346.74
1,108.7
3.91
5.7
138.93
2,211.9
8,302.15
1.02
41.53
129.94
2,387.97
8,069.63
9.3518
0.02
330
2,212
100
10.57
6.3827
242
1
80
10.0077
0.25
100
489.05
604.09
1,488.22
1,293.47
10.52
15.46
393.64
2,318.67
8,772.66
1.26
45.03
369.94
2,387.78
8,119.38
8.6532
0.03
367
2,319
100
28.52
17.1861
241
1
81
20.0068
0.7005
100
491.19
606.94
1,473.75
1,233.96
9.35
13.61
332.48
2,323.7
8,713.87
1.07
43.87
313.92
2,387.85
8,054.25
9.18
0.02
364
2,324
100
24.42
14.6309
240
1
82
35.004
0.8412
100
449.44
555.3
1,360.17
1,118.89
5.48
7.98
193.52
2,222.84
8,337.16
1.02
41.62
182.14
2,387.87
8,061.6
9.3146
0.02
330
2,223
100
14.67
8.9893
239
1
83
25.005
0.621
60
462.54
536.28
1,257.13
1,042
7.05
9
174.94
1,915.19
7,998.88
0.94
36.42
163.75
2,028.11
7,871.52
10.8468
0.02
305
1,915
84.93
14.25
8.5233
238
1
84
20.0031
0.7
100
491.19
606.79
1,469.57
1,238.58
9.35
13.61
332.53
2,323.7
8,702.15
1.07
43.94
313.84
2,387.83
8,055.89
9.1847
0.02
364
2,324
100
24.43
14.7178
237
1
85
42.0007
0.8417
100
445
549.1
1,350.3
1,109.72
3.91
5.7
137.88
2,211.86
8,306.62
1.02
41.71
130.58
2,387.93
8,077.56
9.3514
0.02
329
2,212
100
10.59
6.4113
236
1
86
0.0013
0
100
518.67
642.36
1,578.24
1,386.45
14.62
21.58
552.46
2,387.88
9,047.93
1.3
47.03
520.7
2,387.93
8,136.59
8.3964
0.03
390
2,388
100
38.98
23.3123
235
1
87
35.0073
0.8411
100
449.44
555.32
1,352.58
1,120.51
5.48
7.98
193.76
2,222.79
8,333.99
1.02
41.51
182.26
2,387.86
8,065.45
9.3221
0.02
331
2,223
100
14.79
8.9154
234
1
88
42.0001
0.8408
100
445
549.67
1,341.56
1,115.3
3.91
5.69
137.32
2,211.96
8,306.42
1.02
41.48
130.09
2,387.99
8,070.55
9.357
0.02
329
2,212
100
10.67
6.3949
233
1
89
20.0045
0.7
100
491.19
606.67
1,483
1,246.45
9.35
13.62
333.57
2,323.78
8,711.38
1.07
44.01
313.33
2,387.85
8,053.25
9.1871
0.02
364
2,324
100
24.63
14.7623
232
1
90
0.0021
0.0006
100
518.67
642.07
1,576.06
1,384.53
14.62
21.58
552.98
2,387.94
9,048.04
1.3
47.19
520.69
2,387.94
8,131.56
8.4011
0.03
391
2,388
100
38.95
23.4175
231
1
91
9.9992
0.25
100
489.05
604.5
1,495.21
1,297.27
10.52
15.47
394.31
2,318.68
8,770.68
1.26
45.18
370.4
2,387.93
8,125.2
8.6104
0.03
366
2,319
100
28.62
16.9787
230
1
92
25.0046
0.62
60
462.54
536.56
1,249.6
1,040.22
7.05
9
174.66
1,915.25
8,002.67
0.94
36.26
163.55
2,028.15
7,863.43
10.8294
0.02
305
1,915
84.93
14.33
8.6429
229
1
93
20.0071
0.7
100
491.19
606.58
1,473.21
1,232.98
9.35
13.61
332.83
2,323.65
8,705.95
1.07
43.89
312.7
2,387.82
8,045.65
9.1983
0.02
363
2,324
100
24.33
14.6484
228
1
94
9.9987
0.2513
100
489.05
604.23
1,492.53
1,295.91
10.52
15.47
393.14
2,318.68
8,770.96
1.26
44.96
370.77
2,387.92
8,127.89
8.6593
0.03
368
2,319
100
28.64
17.12
227
1
95
25.0055
0.6209
60
462.54
536.4
1,249.04
1,037.81
7.05
9
174.46
1,915.25
8,001.66
0.94
36.29
163.76
2,028.13
7,863.31
10.8898
0.02
305
1,915
84.93
14.41
8.6036
226
1
96
42.0036
0.84
100
445
549.52
1,343.06
1,106.93
3.91
5.69
137.55
2,211.88
8,301.31
1.02
41.71
129.93
2,387.96
8,078.97
9.3636
0.02
328
2,212
100
10.62
6.3795
225
1
97
10.0032
0.2518
100
489.05
603.39
1,489.59
1,295.78
10.52
15.47
393.26
2,318.66
8,769.86
1.26
44.92
371.2
2,387.89
8,122.65
8.5626
0.03
368
2,319
100
28.85
17.3044
224
1
98
10.0022
0.2515
100
489.05
604.08
1,495.81
1,303.74
10.52
15.47
393.61
2,318.65
8,755.21
1.26
44.94
370.9
2,387.86
8,129.98
8.6377
0.03
369
2,319
100
28.55
17.1995
223
1
99
41.9985
0.84
100
445
549.42
1,346.47
1,111.37
3.91
5.7
137.6
2,211.91
8,304.08
1.02
41.49
129.92
2,388.06
8,077.4
9.3458
0.02
329
2,212
100
10.71
6.2607
222
1
100
35.0077
0.84
100
449.44
555.41
1,362.76
1,117.42
5.48
7.97
193.17
2,222.83
8,331.29
1.02
41.46
181.85
2,387.9
8,060.14
9.2897
0.02
329
2,223
100
14.87
8.7767
221
End of preview. Expand in Data Studio

CMAPSS Jet Engine Simulated Data FD004 - NASA

This dataset contains simulated data from the CMAPSS (Commercial Modular Aero-Propulsion System Simulation) Jet Engine by NASA, FD004.

Train trjectories: 248 Test trajectories: 249 Conditions: SIX 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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