Density of Dry Air vs Temperature and Pressure Calculator

Air Density Chart

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Density of dry air vs temperature in degrees Fahrenheit at 1 atm, 10 bar and 100 bar, with the ideal gas curve at 100 bar

Dry air, calculated with CoolProp 7.2.0 (Lemmon et al. 2000 equation of state). Y-axis is logarithmic. The dotted line is the ideal gas law at 100 bar, shown to see how far real air departs from it.

Air Density Calculator
Degrees (°F):
Degrees (°C):
Pressure:
Density (real gas)
Density (kg/m³):  
Density (lb/ft³):  
Density (g/L = g/dm³):  
Density (lb/US gal):  
Specific volume (m³/kg):  
Specific volume (ft³/lb):  
Ideal gas, R = 287.05 J/(kg·K)
Ideal-gas density (kg/m³):  
Ideal-gas density (lb/ft³):  
Ideal gas minus real (% of real):  
Compressibility factor Z:  

Dry air, absolute pressure. Range: −100 to 1000 °C (−148 to 1832 °F) and 1 atm to 100 bar (14.696 to 1450 psia). Outside it the calculator shows “Out of Range”. Values are interpolated linearly in temperature (10 °C grid) and in ln P between 1 atm, 2, 5, 10, 20, 50 and 100 bar. Interpolation adds about 0.1 % at most (checked against CoolProp at six off-grid points).

Density of Air
Quick answer

Dry air at 15 °C (59 °F) and 1 atm has a density of 1.2255 kg/m³ (0.07651 lb/ft³). At 20 °C it is 1.2046 kg/m³. Density falls as air gets hotter and rises with pressure.

This page is for dry air. Humid air is lighter. For humid air use the wet bulb calculator. For density at altitude use the density altitude calculator.

Real gas versus ideal gas

For an ideal gas, density is set by the ideal gas law:

ρ = P / (R·T)

with P in Pa, T in K and R = 287.05 J/(kg·K) for dry air (8.31432 J/(mol·K) divided by 28.9644 g/mol, from the U.S. Standard Atmosphere 1976). Real air is described with the compressibility factor Z:

ρ = P / (Z·R·T)

At 1 atm the ideal gas law is within about 0.1 % of the real value above 0 °C. At 100 bar and −100 °C, Z is 0.659, so the ideal gas law is about 52 % too high there. At 100 bar and 1000 °C, Z is 1.027. Use the real-gas value above about 10 bar or below about −50 °C.

Where the numbers come from

Accuracy. Lemmon et al. (2000) state an uncertainty of about 0.1 % in density, 0.2 % in speed of sound and 1 % in heat capacity from the solidification point to 873 K (600 °C) and up to 70 MPa. Above 873 K there were no reliable air data, so nitrogen data were used and the paper gives about 0.5 % for density. Lemmon & Jacobsen (2004) state about 5 % for the viscosity and thermal conductivity of air, and more near the critical point. Viscosity and conductivity above about 600 °C, and the 1000 °C end of the range, are less certain than that. CoolProp uses a molar mass of 28.96546 g/mol, the U.S. Standard Atmosphere uses 28.9644 g/mol. That is the main reason CoolProp density at 15 °C and 1 atm is 0.04 % above the Standard Atmosphere value.

Dry Air Density at 1 atm (101.325 kPa)

Density of dry air every 20 °C from −100 to 1000 °C at 1 atm.

Temp
(°C)
Temp
(°F)
Density
(kg/m³)
Density
(lb/ft³)
Ideal gas
(kg/m³)
Ideal minus
real (%)
Z
-100.0-148.02.04670.12782.0386-0.3920.99608
-80.00-112.01.83250.11441.8275-0.2710.99729
-60.00-76.001.65920.10361.6561-0.1890.99811
-40.00-40.001.51600.094641.5140-0.1320.99869
-20.00-4.0001.39570.087131.3944-0.09100.99910
032.001.29310.080721.2923-0.06110.99940
20.0068.001.20460.075201.2041-0.03820.99962
40.00104.01.12750.070381.1272-0.02130.99979
60.00140.01.05960.066151.0595-0.008490.99993
80.00176.00.999520.062400.999540.002401.0000
100.0212.00.945870.059050.945970.01031.0001
120.0248.00.897700.056040.897840.01651.0002
140.0284.00.854200.053330.854380.02121.0002
160.0320.00.814730.050860.814930.02521.0003
180.0356.00.778750.048620.778960.02801.0003
200.0392.00.745810.046560.746040.03041.0003
220.0428.00.715550.044670.715780.03231.0003
240.0464.00.687650.042930.687880.03361.0003
260.0500.00.661850.041320.662080.03481.0004
280.0536.00.637910.039820.638140.03541.0004
300.0572.00.615650.038430.615870.03611.0004
320.0608.00.594890.037140.595110.03651.0004
340.0644.00.575480.035930.575690.03681.0004
360.0680.00.557300.034790.557510.03701.0004
380.0716.00.540240.033730.540440.03681.0004
400.0752.00.524190.032720.524380.03661.0004
420.0788.00.509060.031780.509250.03671.0004
440.0824.00.494790.030890.494970.03641.0004
460.0860.00.481290.030050.481470.03621.0004
480.0896.00.468510.029250.468680.03591.0004
500.0932.00.456390.028490.456560.03551.0004
520.0968.00.444890.027770.445050.03531.0004
540.010040.433950.027090.434100.03501.0004
560.010400.423530.026440.423680.03451.0004
580.010760.413610.025820.413750.03411.0003
600.011120.404130.025230.404270.03391.0003
620.011480.395080.024660.395220.03341.0003
640.011840.386430.024120.386560.03291.0003
660.012200.378150.023610.378270.03251.0003
680.012560.370220.023110.370340.03211.0003
700.012920.362610.022640.362730.03171.0003
720.013280.355310.022180.355420.03121.0003
740.013640.348300.021740.348410.03101.0003
760.014000.341560.021320.341660.03041.0003
780.014360.335070.020920.335170.03011.0003
800.014720.328830.020530.328930.02951.0003
820.015080.322810.020150.322910.02911.0003
840.015440.317010.019790.317110.02901.0003
860.015800.311420.019440.311510.02861.0003
880.016160.306020.019100.306110.02811.0003
900.016520.300800.018780.300890.02761.0003
920.016880.295760.018460.295850.02771.0003
940.017240.290890.018160.290970.02721.0003
960.017600.286170.017870.286250.02661.0003
980.017960.281600.017580.281680.02661.0003
100018320.277180.017300.277250.02601.0003

Calculated with CoolProp 7.2.0. Ideal gas uses R = 287.05 J/(kg·K).

Dry Air Density at 1 atm, 10 bar and 100 bar

Density at selected temperatures and three pressures (1 atm = 1.013 bara = 14.696 psia).

Temp
(°C)
Temp
(°F)
Pressure
(bara)
Pressure
(psia)
Density
(kg/m³)
Density
(lb/ft³)
Ideal gas
(kg/m³)
Ideal minus
real (%)
Z
1 bara (1 atm, 14.7 psia)
-100-148.01.01314.72.04670.12782.0386-0.3920.99608
032.001.01314.71.29310.080721.2923-0.06110.99940
100212.01.01314.70.945870.059050.945970.01031.0001
200392.01.01314.70.745810.046560.746040.03041.0003
400752.01.01314.70.524190.032720.524380.03661.0004
60011121.01314.70.404130.025230.404270.03391.0003
80014721.01314.70.328830.020530.328930.02951.0003
100018321.01314.70.277180.017300.277250.02601.0003
10 bara (145 psia)
-100-148.01014520.9361.30720.120-3.900.96102
032.001014512.8260.800712.754-0.5650.99435
100212.0101459.32490.58219.33600.1191.0012
200392.0101457.34000.45827.36280.3111.0031
400752.0101455.15620.32195.17520.3681.0037
6001112101453.97640.24823.98980.3371.0034
8001472101453.23660.20213.24620.2971.0030
10001832101452.72920.17042.73630.2611.0026
100 bara (1450 psia)
-100-148.01001450305.5219.07201.20-34.10.65854
032.001001450131.438.205127.54-2.960.97037
100212.0100145091.1615.69193.3602.411.0241
200392.0100145070.9714.43173.6283.741.0374
400752.0100145049.8033.10951.7523.911.0392
6001112100145038.5562.40739.8983.481.0348
8001472100145031.5071.96732.4623.031.0303
10001832100145026.6561.66427.3632.651.0265

The calculator above covers 2, 5, 20 and 50 bar as well.

Related Air Pages and Tools

Other air pages: General Properties | Specific Heat Capacity | Thermal Conductivity | Dynamic and Kinematic Viscosity | Prandtl Number | Thermal Diffusivity | Thermal Expansion Coefficient | Speed of Sound.

Density is used with viscosity to find the Reynolds number in pipe velocity work, and for gas flow in gas mass flow rate. Compare with water density.

Sources
  • E. W. Lemmon, R. T. Jacobsen, S. G. Penoncello and D. G. Friend, “Thermodynamic Properties of Air and Mixtures of Nitrogen, Argon, and Oxygen From 60 to 2000 K at Pressures to 2000 MPa,” J. Phys. Chem. Ref. Data 29(3), 331–385, 2000. doi:10.1063/1.1285884. Equation of state for dry air: density, specific heats, speed of sound, compressibility factor. Opened the NIST reprint, accessed 25 Oct 2026.
  • E. W. Lemmon and R. T. Jacobsen, “Viscosity and Thermal Conductivity Equations for Nitrogen, Oxygen, Argon, and Air,” Int. J. Thermophys. 25(1), 21–69, 2004. doi:10.1023/B:IJOT.0000022327.04529.f3. Viscosity and thermal conductivity of air. Only the abstract was read (NIST publication page), accessed 25 Oct 2026.
  • I. H. Bell, J. Wronski, S. Quoilin and V. Lemort, “Pure and Pseudo-pure Fluid Thermophysical Property Evaluation and the Open-Source Thermophysical Property Library CoolProp,” Ind. Eng. Chem. Res. 53(6), 2498–2508, 2014. doi:10.1021/ie4033999. The software used (CoolProp 7.2.0, fluid “Air”) to evaluate the two correlations above.
  • NOAA, NASA and USAF, U.S. Standard Atmosphere, 1976, NASA-TM-X-74335. ntrs.nasa.gov/citations/19770009539. Sea-level reference values, dry-air composition and Sutherland constants, accessed 25 Oct 2026.

All numbers on this page are calculated, not measured here. See the Air General Properties page for the accuracy statements and the cross-check against the U.S. Standard Atmosphere.

Cite This Work