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LucasThil
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nasa_turbofan_degradation_FD002

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10K - 100K
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5.71
138.52
2,211.57
8,304.33
1.02
42.23
130.29
2,387.59
8,073.22
9.3868
0.02
332
2,212
100
10.59
6.4427
93
1
57
20.0046
0.7003
100
491.19
606.65
1,486.48
1,255.67
9.35
13.65
334.77
2,323.93
8,713.81
1.08
44.4
314.39
2,388.05
8,048.96
9.2407
0.02
365
2,324
100
24.68
14.6122
92
1
58
35.0031
0.84
100
449.44
555.58
1,371.01
1,133.15
5.48
8
193.74
2,222.67
8,334.28
1.02
42.06
182.41
2,387.75
8,056.45
9.3193
0.02
334
2,223
100
14.73
8.8635
91
1
59
42.0053
0.8412
100
445
549.36
1,352.92
1,125.09
3.91
5.71
138.73
2,211.56
8,303.55
1.02
42.2
130.35
2,387.66
8,064.02
9.368
0.02
330
2,212
100
10.45
6.3491
90
1
60
25.002
0.62
60
462.54
537.03
1,262.69
1,047.52
7.05
9.02
175
1,915.12
7,999.59
0.94
36.74
164.32
2,028.02
7,864.81
10.8843
0.02
308
1,915
84.93
14.31
8.6567
89
1
61
20.0011
0.7
100
491.19
607.51
1,481.61
1,253.1
9.35
13.65
334.33
2,323.98
8,707.14
1.07
44.47
315.14
2,388.06
8,045.61
9.2412
0.02
367
2,324
100
24.53
14.6998
88
1
62
0.0029
0
100
518.67
643.24
1,591.46
1,405.31
14.62
21.61
553.34
2,388.14
9,040.41
1.3
47.54
521.83
2,388.21
8,117.75
8.4424
0.03
392
2,388
100
38.83
23.1994
87
1
63
41.9992
0.8413
100
445
550.1
1,355.17
1,123.54
3.91
5.71
138.41
2,211.53
8,311.01
1.02
42.27
130.96
2,387.6
8,066.56
9.362
0.02
331
2,212
100
10.36
6.3852
86
1
64
35.0052
0.8406
100
449.44
555.71
1,359.17
1,129.99
5.48
8
193.78
2,222.73
8,340.5
1.02
42.2
183.37
2,387.79
8,055.84
9.3277
0.02
334
2,223
100
14.76
8.8812
85
1
65
0.0016
0.0006
100
518.67
642.62
1,596.62
1,404.65
14.62
21.61
553.42
2,388.18
9,040.81
1.3
47.55
521
2,388.11
8,127.28
8.4554
0.03
394
2,388
100
38.73
23.1253
84
1
66
35.0053
0.84
100
449.44
555.55
1,371.45
1,128.96
5.48
8
194.45
2,222.68
8,341.42
1.02
42.25
182.98
2,387.74
8,055.26
9.3331
0.02
334
2,223
100
14.92
8.8907
83
1
67
10.0015
0.25
100
489.05
605.01
1,504.34
1,311.13
10.52
15.49
392.95
2,318.99
8,763.55
1.26
45.64
371.09
2,388.19
8,111.05
8.6675
0.03
372
2,319
100
28.47
17.1321
82
1
68
0
0
100
518.67
642.88
1,586.74
1,409.1
14.62
21.61
554.08
2,388.1
9,043.13
1.3
47.58
521.51
2,388.15
8,120.24
8.478
0.03
394
2,388
100
38.9
23.2609
81
1
69
0.0009
0.0009
100
518.67
642.48
1,591.9
1,409.85
14.62
21.61
552.82
2,388.15
9,042.91
1.3
47.63
521.43
2,388.08
8,125.99
8.4428
0.03
392
2,388
100
38.9
23.2975
80
1
70
42.0024
0.8411
100
445
549.91
1,352.21
1,125
3.91
5.72
139.43
2,211.62
8,303.98
1.02
42.04
130.67
2,387.57
8,073.45
9.3926
0.02
330
2,212
100
10.53
6.4002
79
1
71
20.0074
0.7
100
491.19
607.44
1,482.17
1,253.33
9.35
13.65
334.53
2,323.93
8,712.14
1.08
44.5
314.82
2,388.01
8,054.48
9.2346
0.02
365
2,324
100
24.4
14.6559
78
1
72
25.0057
0.62
60
462.54
536.96
1,260.81
1,040.99
7.05
9.02
175.52
1,915.1
7,996.85
0.94
36.92
164.35
2,028.03
7,859.5
10.8678
0.02
307
1,915
84.93
14.24
8.6689
77
1
73
25.0025
0.6217
60
462.54
536.57
1,260.77
1,050.42
7.05
9.03
176.3
1,915.13
8,004.96
0.94
36.85
164.95
2,028.04
7,864.94
10.8815
0.02
308
1,915
84.93
14.16
8.6025
76
1
74
20.0033
0.702
100
491.19
607.16
1,485.05
1,253.12
9.35
13.65
334.09
2,323.95
8,704.89
1.08
44.36
314.49
2,388.09
8,048.84
9.2487
0.03
366
2,324
100
24.33
14.689
75
1
75
25.0039
0.62
60
462.54
536.43
1,258.23
1,049.25
7.05
9.02
175.13
1,915.07
7,995.45
0.94
36.81
164.46
2,027.99
7,864.99
10.894
0.02
308
1,915
84.93
14.19
8.5761
74
1
76
25.0023
0.62
60
462.54
537.02
1,268.7
1,049.71
7.05
9.03
176.05
1,915.11
8,003.74
0.94
36.81
164.05
2,028.03
7,863.25
10.9035
0.02
308
1,915
84.93
14.2
8.6043
73
1
77
42.0008
0.8405
100
445
549.99
1,356.65
1,129.01
3.91
5.71
137.8
2,211.59
8,304.05
1.02
42.07
130.41
2,387.63
8,071.77
9.3571
0.02
330
2,212
100
10.59
6.4279
72
1
78
25.0024
0.62
60
462.54
536.41
1,262.7
1,048.63
7.05
9.03
175.2
1,915.15
8,000.19
0.94
36.71
164.53
2,027.99
7,865.97
10.9131
0.02
308
1,915
84.93
14.15
8.5599
71
1
79
42.0017
0.84
100
445
549.7
1,354.71
1,120.3
3.91
5.71
138.79
2,211.6
8,303.68
1.02
42.15
130.63
2,387.63
8,065.68
9.3851
0.02
333
2,212
100
10.71
6.3779
70
1
80
42.0037
0.84
100
445
549.39
1,362.36
1,135.78
3.91
5.71
138.94
2,211.57
8,304.73
1.02
42.19
130.11
2,387.63
8,069.07
9.4237
0.02
330
2,212
100
10.61
6.4276
69
1
81
20.0011
0.7
100
491.19
607.61
1,491.73
1,263.49
9.35
13.66
335.04
2,323.94
8,708.2
1.08
44.52
314.39
2,388.05
8,049.96
9.2411
0.02
366
2,324
100
24.45
14.6586
68
1
82
0.0027
0.0008
100
518.67
643.26
1,588.99
1,407.97
14.62
21.61
552.85
2,388.2
9,039.16
1.3
47.84
521.02
2,388.16
8,126.13
8.4342
0.03
395
2,388
100
38.63
23.2127
67
1
83
42.0068
0.84
100
445
549.11
1,352.66
1,135.18
3.91
5.71
138.17
2,211.6
8,301.72
1.02
42.07
130.25
2,387.66
8,068.96
9.3919
0.02
332
2,212
100
10.39
6.2655
66
1
84
41.9983
0.84
100
445
549.65
1,352.66
1,134.46
3.91
5.71
138.3
2,211.59
8,300.56
1.02
42.26
130.73
2,387.66
8,069.87
9.3779
0.02
332
2,212
100
10.64
6.4574
65
1
85
0
0.0011
100
518.67
642.74
1,587.82
1,409.12
14.62
21.61
553.48
2,388.1
9,041.37
1.3
47.68
521.22
2,388.2
8,118.69
8.4494
0.03
393
2,388
100
38.88
23.2781
64
1
86
42.0045
0.84
100
445
549.23
1,357.31
1,129.9
3.91
5.71
138.09
2,211.6
8,307.89
1.02
42.1
130.21
2,387.58
8,074.9
9.3934
0.02
332
2,212
100
10.58
6.2943
63
1
87
42.0024
0.8413
100
445
549.92
1,353.15
1,123.53
3.91
5.72
138.61
2,211.56
8,309.33
1.02
42.3
130.28
2,387.61
8,072.4
9.3545
0.02
331
2,212
100
10.49
6.3436
62
1
88
35.0043
0.8416
100
449.44
555.62
1,368.09
1,125.3
5.48
8
194
2,222.68
8,338.97
1.02
42.1
182.76
2,387.78
8,051.96
9.383
0.02
335
2,223
100
14.61
8.8893
61
1
89
9.9995
0.2514
100
489.05
605.25
1,504.64
1,312.96
10.52
15.5
393.97
2,319.06
8,763.25
1.26
45.65
371.25
2,388.2
8,113.05
8.6515
0.03
369
2,319
100
28.72
17.1524
60
1
90
0.0003
0
100
518.67
642.95
1,588.98
1,409.61
14.62
21.61
553.31
2,388.13
9,041.44
1.3
47.61
520.9
2,388.14
8,127.02
8.4451
0.03
396
2,388
100
38.74
23.1633
59
1
91
25.0027
0.62
60
462.54
536.99
1,266.82
1,051.87
7.05
9.02
175.02
1,915.11
8,001
0.94
36.97
165.07
2,028.02
7,863.25
10.9231
0.02
308
1,915
84.93
14.17
8.5937
58
1
92
41.9984
0.8411
100
445
548.99
1,352.89
1,137.5
3.91
5.71
138.58
2,211.59
8,317.33
1.02
42.26
130.61
2,387.58
8,072.97
9.3743
0.02
332
2,212
100
10.54
6.3763
57
1
93
20.0005
0.7009
100
491.19
608
1,486.6
1,260.39
9.35
13.66
334.76
2,323.95
8,717.43
1.08
44.58
314.62
2,388.08
8,054.57
9.2455
0.02
366
2,324
100
24.43
14.6864
56
1
94
41.9992
0.84
100
445
550.1
1,353.17
1,126.68
3.91
5.72
139.02
2,211.61
8,305.16
1.02
42.11
129.63
2,387.68
8,066
9.436
0.02
331
2,212
100
10.67
6.3511
55
1
95
35.0058
0.8403
100
449.44
555.64
1,369.57
1,136.49
5.48
8
193.87
2,222.64
8,339.32
1.02
42
182.37
2,387.76
8,058.75
9.3649
0.02
335
2,223
100
14.8
8.8716
54
1
96
42.0062
0.8402
100
445
549.65
1,358.37
1,125.38
3.91
5.71
139
2,211.54
8,308.02
1.02
42.2
130.49
2,387.55
8,067.54
9.3981
0.02
330
2,212
100
10.49
6.3469
53
1
97
42.0015
0.8413
100
445
549.43
1,354.86
1,127.44
3.91
5.71
138.91
2,211.66
8,314.36
1.02
42.39
130.44
2,387.63
8,071.46
9.3681
0.02
329
2,212
100
10.75
6.3409
52
1
98
0.0025
0.0015
100
518.67
643.26
1,593.43
1,409.77
14.62
21.61
553.19
2,388.13
9,048.15
1.3
47.49
521.22
2,388.17
8,124.58
8.4587
0.03
395
2,388
100
38.62
23.3025
51
1
99
10.0051
0.2502
100
489.05
604.97
1,501.19
1,309.55
10.52
15.5
393.8
2,319.04
8,763.64
1.26
45.62
371.05
2,388.25
8,119.05
8.6636
0.03
369
2,319
100
28.53
17.1145
50
1
100
20.0027
0.7
100
491.19
607.6
1,488.43
1,259.11
9.35
13.66
333.85
2,323.93
8,704.26
1.08
44.83
314.17
2,388.06
8,048.36
9.249
0.03
367
2,324
100
24.51
14.6742
49
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CMAPSS Jet Engine Simulated Data FD002 - NASA

This dataset contains simulated data from the CMAPSS (Commercial Modular Aero-Propulsion System Simulation) Jet Engine by NASA, FD002.

Train trjectories: 260 Test trajectories: 259 Conditions: SIX Fault Modes: ONE (HPC 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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