MIL-PRF-23699 Turbine Oil Viscosity Calculator

MIL-PRF-23699 Kinematic Viscosity Chart

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Black: NIST IR 8263 measurement of a qualified MIL-PRF-23699 oil (μ ÷ ρ; dashed where the density is extrapolated above 70 °C). Colored: manufacturer typical values (marked points) joined by ASTM D341. Red crosses: MIL-PRF-23699G limits. Other AeroShell turbine oils and the Lee Company chart are on the next chart. Y-axis is logarithmic.

Other Turbine Oils and Cross-Check: Kinematic Viscosity Chart

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Colored: AeroShell turbine oils that are not MIL-PRF-23699 (manufacturer typical values, marked points, joined by ASTM D341). Grey dashed: The Lee Company chart for MIL-PRF-23699, a cross-check. Black: the NIST IR 8263 MIL-PRF-23699 measurement from the chart above, for reference. Toggle data sets by clicking the legend. Y-axis is logarithmic.

MIL-PRF-23699 Dynamic (Absolute) Viscosity Chart

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Black: dynamic viscosity measured by NIST (IR 8263, Table B4, atmospheric pressure, uncertainty 5 %). Colored: product typical kinematic viscosity × NIST density (μ = ν × ρ), only from 5 to 70 °C, where that density is measured (Table 23). Toggle data sets by clicking the legend. Y-axis is logarithmic.

MIL-PRF-23699 Viscosity Calculator
Degrees (°F):
Degrees (°C):
Kinematic Viscosity
mm²/s (= cSt):  
Centistokes (cSt):  
Stokes (cm²/s):  
m²/s:  
in²/s:  
ft²/s:  
Dynamic (Absolute) Viscosity
mPa·s (= cP):  
Centipoise (cP):  
Poise (g/(cm·s)):  
Pa·s (Poiseuille):  
lbm/(ft·s):  
kg/(m·h):  
Viscosity of MIL-PRF-23699 Turbine Oil
Kinematic Viscosity

MIL-PRF-23699 is defined as a 5 mm²/s class oil. The specification sets a narrow kinematic viscosity band at 100 °C (4.90–5.40 mm²/s) to ensure consistent lubrication film thickness across qualified products. At cold temperatures the viscosity rises steeply — the spec allows up to 13 000 mm²/s at −40 °C — which governs engine cold-start and ground-start limits.

Why Viscosity Matters in Turbine Lubrication

Turbine bearing systems operate over an extreme temperature range, from arctic ground starts (−54 °C) to bearing compartment temperatures that can exceed 200 °C. Too high a viscosity at cold temperatures means the oil cannot be pumped to bearings during start-up; too low a viscosity at high temperatures means inadequate hydrodynamic film thickness and accelerated wear. The narrow 100 °C band ensures all qualified oils deliver predictable film thickness in the normal operating regime.

Dynamic (Absolute) vs. Kinematic Viscosity
Dynamic (Absolute) Viscosity — μ

Dynamic viscosity measures a fluid's resistance to shear — the internal force per unit area required to make one layer slide past another. It is independent of density. The SI unit is the pascal-second (Pa·s); the common engineering unit is the millipascal-second (mPa·s), numerically equal to centipoise (cP).

\[ \tau = \mu\,\frac{du}{dy} \]
Kinematic Viscosity — ν

Kinematic viscosity is the ratio of dynamic viscosity to fluid density. The SI unit is m²/s; the common unit is mm²/s, numerically equal to centistokes (cSt). Most turbine oil specifications grade viscosity kinematically because viscometers measure time-of-flow under gravity, which naturally yields kinematic viscosity.

\[ \nu = \frac{\mu}{\rho} \quad\Rightarrow\quad \mu\ [\text{mPa}\cdot\text{s}] = \frac{\nu\ [\text{mm}^2/\text{s}] \times \rho\ [\text{kg/m}^3]}{1000} \]
Kinematic Viscosity by Temperature (mm²/s)
Temperature (°F) Temperature (°C) NIST IR 8263 (generic MIL-PRF-23699) AeroShell Turbine Oil 500
MIL-PRF-23699G Grade STD
AeroShell Turbine Oil 560
MIL-PRF-23699G Grade HTS
AeroShell Ascender
MIL-PRF-23699G Grade HTS
Mobil Jet Oil II
MIL-PRF-23699 STD (approved)
Eastman Turbo Oil 2380
MIL-PRF-23699 STD (qualified)
-40-40.0–921510229–110007950
-30-34.4–44854950–52993919
-20-28.9–23452573–27442072
-10-23.3–13051425–15141166
0-17.8–768.0834.6–883.5692.2
10-12.2–474.7513.6–541.9431.4
20-6.7–306.5330.2–347.4280.6
30-1.1–205.7220.8–231.6189.5
404.4–142.9152.8–159.9132.5
5010.0–102.3109.1–113.995.39
6015.6–75.3480.07–83.4270.58
7021.160.2256.8560.25–62.6453.50
8026.745.2343.8546.35–48.1041.43
9032.235.0834.5036.38–37.6932.72
10037.827.8227.6329.07–30.0726.29
11043.322.7022.4623.5522.7224.2221.44
12048.918.7418.5219.3318.6419.7317.72
13054.415.6015.4716.0915.5116.3014.84
14060.012.9213.0813.5613.0613.6512.57
15065.610.7211.1811.5511.1311.5710.77
16071.19.368*9.6499.9459.5809.9139.313
17076.78.345*8.4058.6418.3248.5768.126
18082.27.215*7.3817.5727.2947.4867.148
19087.86.288*6.5326.6866.4416.5876.335
20093.35.527*5.8205.9465.7295.8405.652
21098.94.896*5.2195.3235.1295.2135.075
220104.44.367*–––––
230110.03.939*–––––
240115.63.584*–––––
250121.13.263*–––––
260126.72.981*–––––

Kinematic viscosity in mm²/s (cSt). NIST column: μ/ρ from NIST IR 8263 Tables B4 and 23 (16.9–126.9 °C); *density extrapolated above 70 °C. Product columns: manufacturer typical values joined by ASTM D341, only between the lowest and highest published temperature. “–” = outside the data.

Published Typical Values and Specification Limits
OilSpecification (from data sheet)Kinematic viscosity, mm²/s (cSt)Source
MIL-PRF-23699G limitsAll classes (STD, HTS, C/I, EE)≤ 13 000 at −40 °C; ≥ 23.0 at 40 °C; 4.90–5.40 at 100 °CMIL-PRF-23699G Table I
AeroShell Turbine Oil 500MIL-PRF-23699G Grade STD; SAE AS5780D SPC9215 at −40 °C; 25.4 at 40 °C; 5.11 at 100 °CData sheet
AeroShell Turbine Oil 560MIL-PRF-23699G Grade HTS; SAE AS5780D SPC10229 at −40 °C; 26.7 at 40 °C; 5.21 at 100 °CData sheet
AeroShell AscenderMIL-PRF-23699G Grade HTS; SAE AS5780D HPC25.77 at 40 °C; 5.02 at 100 °CData sheet
Mobil Jet Oil IIMIL-PRF-23699 STD (approved); SAE AS5780 SPC11000 at −40 °C; 27.6 at 40 °C; 5.1 at 100 °CData sheet
Eastman Turbo Oil 2380MIL-PRF-23699 STD (qualified); SAE AS5780 SPC7950 at −40 °C; 24.2 at 40 °C; 4.97 at 100 °CData sheet
AeroShell Turbine Oil 555DOD-PRF-85734A (not MIL-PRF-23699)11000 at −40 °C; 26.5 at 40 °C; 5.2 at 100 °CData sheet
AeroShell Turbine Oil 750DEF STAN 91-98 (not MIL-PRF-23699)11531 at −40 °C; 32 at 40 °C; 7.65 at 100 °CData sheet
AeroShell Turbine Oil 308MIL-PRF-7808M Grade 3 (not MIL-PRF-23699)7600 at −51 °C; 12 at 40 °C; 3.1 at 100 °CData sheet
AeroShell Turbine Oil 390DEF STAN 91-94 (not MIL-PRF-23699)2000 at −40 °C; 12.9 at 40 °C; 3.4 at 100 °CData sheet
AeroShell Turbine Oil 3DEF STAN 91-99 (not MIL-PRF-23699)1149 at −25 °C; 12.66 at 40 °CData sheet

Typical values are as printed on each manufacturer’s current data sheet; production lots vary. AeroShell Ascender’s −40 °C value is published only as “<12 000” and is not plotted.

Sources
  • A. Fortin et al., Thermophysical Properties of Polyol Ester Lubricants, NIST IR 8263, National Institute of Standards and Technology, 2019. Table B4 (dynamic viscosity, generic qualified MIL-PRF-23699 oil; supplier and grade not stated; expanded uncertainty 5 {'nist': 'https://nvlpubs.nist.gov/nistpubs/ir/2019/NIST.IR.8263.pdf', 'spec': 'https://everyspec.com/MIL-PRF/MIL-PRF-010000-29999/MIL-PRF-23699G_50301/'}t atmospheric pressure) and Table 23 (density, 5–70 °C). PDF
  • MIL-PRF-23699G, Lubricating Oil, Aircraft Turbine Engine, Synthetic Base, 13 March 2014, Table I. EverySpec
  • Shell Aviation, AeroShell Turbine Oil 500, 555, 560, Ascender, 750, 3, 308 and 390 technical data sheets (current revisions); ExxonMobil, Mobil Jet Oil II product data; Eastman, Turbo Oil 2380 technical data sheet. Links in the table above.
  • ASTM D341, Standard Practice for Viscosity-Temperature Equations and Charts for Liquid Petroleum or Hydrocarbon Products — the interpolation used between published typical values.
  • The Lee Company, Viscosities of Typical Fluids vs. Temperature — shown only as a cross-check; it agrees with the NIST and AeroShell 500 data within about 2–6 %.

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