MIL-PRF-23699 Thermal Conductivity Chart

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Values measured at near-ambient pressure (0.35–1.0 MPa). Data range: 83 °F to 439 °F (28 °C to 226 °C).

Data from: NIST IR 8263 — Thermophysical Properties of Polyol Ester Lubricants, Table A4.

Toggle data sets by clicking the legend.

MIL-PRF-23699 Thermal Conductivity Calculator
Degrees (°F):
Degrees (°C):
W / (m·K):  
mW / (m·K):  
BTU / (h·ft·°F):  
BTU·in / (h·ft²·°F):  
W / (cm·K):  
Thermal Conductivity of MIL-PRF-23699 Turbine Engine Oil
About This Data

The thermal conductivity data shown here was measured by NIST using a transient hot-wire instrument at pressures ranging from 0.4 to 69 MPa across isotherms from 300 K to 500 K (27 °C to 227 °C). The values tabulated here correspond to the lowest-pressure measurements at each isotherm, which are representative of near-ambient conditions.

Thermal conductivity decreases approximately linearly with increasing temperature over this range, falling from about 0.145 W/(m·K) at 83 °F (28 °C) to about 0.114 W/(m·K) at 439 °F (226 °C). The combined expanded uncertainty in the thermal conductivity measurements is approximately ±1 %.

MIL-PRF-23699 is a fully qualified synthetic turbine engine oil based on polyol esters (POE), widely used in aircraft gas turbine engines. Its thermal conductivity is significantly lower than water and is relatively insensitive to pressure at modest pressures.

MIL-PRF-23699 — Thermal Conductivity vs. Temperature
Temp (°C) Temp (°F) Pressure (MPa) λ (W/m·K) λ (mW/m·K) λ (BTU/h·ft·°F)
28.483.10.400.1451145.10.0839
93.6200.50.720.1358135.80.0785
126.8260.20.950.1307130.70.0755
159.9319.80.730.1250125.00.0722
192.7378.90.540.1193119.30.0689
226.3439.30.620.1139113.90.0658

Near-ambient pressure measurements extracted from NIST IR 8263, Table A4. Expanded uncertainty: ±1 %.

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