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LucasThil
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nasa_turbofan_degradation_FD002

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10K - 100K
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3.91
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
End of preview. Expand in Data Studio

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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