Online references: https://www.grc.nasa.gov/WWW/K-12/airplane/atmosmet.html and https://www.nist.gov/system/files/documents/calibrations/metv29i1p67-2.pdf
Density Published Density
1.183473 1.183472
1.306584 1.306582
1.202410 1.202408
0.694163 0.694162
Exercises from Exterior ballistics, 1935
By Lieutenant Commander Ernest Edward Herrmann
Percentage Differences Exercise 1 Page 41
Percentage Difference [1] = 0.294283%
Percentage Difference [2] = 0.026383%
Percentage Difference [3] = 0.094477%
Percentage Difference [4] = 0.050340%
Percentage Difference [5] = 0.026880%
Percentage Difference [6] = 0.008545%
Percentage Difference [7] = 0.001676%
Percentage Difference [8] = 0.008220%
Three Altitude Related Density Calculations
Rho1 is from Exterior ballistics, 1935
Rho2 is from NASA
Rho3 is from Wikipedia
h ft Rho1 SI Rho2 SI Rho3
0 1.000000 1.226614 1.208993
1000 0.968902 1.215727 1.174010
2000 0.938772 1.204914 1.139806
3000 0.909578 1.194175 1.106369
4000 0.881292 1.183510 1.073689
5000 0.853886 1.172917 1.041752
6000 0.827332 1.162397 1.010547
7000 0.801604 1.151949 0.980062
8000 0.776676 1.141574 0.950286
Three Altitude Related Ballistic Density Calculations
Rho1 is from Exterior ballistics, 1935
Rho2 is from NASA Rho3 is from Wikipedia
STP = Temperature = 59 F Pressure = 29.53 Humidity = 78%
Temp Press h ft Rho1 SI Rho2 SI Rho3
65 29.60 1000 0.968902 1.203134 1.161848
85 29.75 18000 0.566291 0.992155 0.656245
57 30.25 8000 0.776676 1.174418 0.977626
69 29.80 13000 0.663193 1.077573 0.801819
32 30.15 15000 0.622587 1.157366 0.822138
Test Case from Exterior ballistics, 1935
Temperature 84 F Pressure 29.90 In Hg
Density SI = 0.959428 Book Density = 0.960
Altitude 18,000 Feet
Density SI = 0.999439 Book Density = 0.991