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NASA C-MAPSS Turbofan Engine Degradation — 4 Sub-datasets, 21 Sensors [Run-to-Failure]

Industrial IoT & Predictive Maintenance Industrial IoT
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Catalog Summary

"NASA Prognostics Center run-to-failure simulation dataset for turbofan engines. Four operational sub-datasets with 21 sensor channels and 3 operational settings. TXT/CSV format. Primary benchmark for Remaining Useful Life (RUL) estimation."

Catalog Notes

Overview

The C-MAPSS (Commercial Modular Aero-Propulsion System Simulation) Turbofan Engine Degradation Simulation Dataset is one of the most widely used public benchmarks in industrial predictive maintenance. Released by the NASA Ames Prognostics Center of Excellence (PCoE), it simulates run-to-failure degradation trajectories for fleets of turbofan jet engines under varying operational conditions and fault modes.

The dataset is divided into four sub-challenges (FD001–FD004) of increasing complexity, reflecting one or two fault modes and one or six operational conditions per challenge. In the training set, engines run from normal operation to failure. In the test set, the time series ends at some point before failure, and the goal is to predict the Remaining Useful Life (RUL) for each engine unit.

Each record captures 21 sensor readings including fan inlet temperature, LPC outlet temperature, HPC outlet temperature, LPC outlet pressure, physical fan speed, corrected fan speed, bypass ratio, and bleed enthalpy, among others. C-MAPSS remains the standard RUL benchmark in industrial IoT, deep learning, and prognostics research.

Column Schema

ColumnDescription
unit_idEngine unit number identifier.
time_cyclesOperational time in engine cycles.
op_setting_1Operational setting 1 (one of 3 settings).
op_setting_2Operational setting 2.
op_setting_3Operational setting 3.
sensor_1 … sensor_2121 sensor measurement channels (temperature, pressure, speed, etc.).
RULRemaining Useful Life label (provided in separate RUL file for test set).

Key Statistics

  • Sub-datasets: FD001, FD002, FD003, FD004
  • Features: 26 columns (unit ID, time, 3 op settings, 21 sensors)
  • Fault Modes: 1 or 2 per sub-dataset
  • Operational Conditions: 1 or 6 per sub-dataset
  • File Format: TXT (space-delimited, CSV-compatible)
  • Time Period: Released 2008

Use Cases

  • Remaining Useful Life (RUL) estimation and prognostics modelling
  • Deep learning benchmarking with LSTM, CNN, Transformer architectures
  • Anomaly detection and fault mode classification in industrial engines
  • Transfer learning across operational conditions for IIoT systems

Source & Attribution

Created by Abhinav Saxena and Kai Goebel at the NASA Ames Prognostics Center of Excellence. The dataset is hosted on NASA's Open Data Portal and also mirrored on Zenodo. It is cited in thousands of prognostics and health management publications worldwide.

View Data Structure

To explore column names, data types, and sample rows, visit the official dataset page on Government.

Preview on Government

Cite This Dataset

Saxena, A., & Goebel, K. (2008). CMAPSS Jet Engine Simulated Data. [Dataset]. NASA Ames Prognostics Center of Excellence / NASA Open Data Portal. https://data.nasa.gov/dataset/cmapss-jet-engine-simulated-data

Source metadata: NASA Ames Prognostics Center of Excellence / NASA Open Data Portal (2008)

Indexed by IoTDataset.com on Apr 10, 2026

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Confirm the licence, version, access conditions, file format, and provenance at the source before use.

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