Air Density at Altitudes with Calculator
About
Enter an altitude in km, to get the specific air density.
This tool uses the below table of known values and then uses linear interpolation to get an accurate result between the known values.
Original values for air density calculations source:
www.engineeringtoolbox.com
Result
100 % Sea Level Density
1 x Sea Level Density
DISCLAIMER:
The tools on this website are designed to be highly accurate, but we cannot and will not be held responsible should any inaccuracy occur.
Use this tool, or the information on this page, or any of the information on this website at your own risk.
No warranty is given about the accuracy of the results, or the accuracy of the information on this page.
Table values:
Altitude (km) | Air Density (kg/m3) | % Sea Level Density | |
---|---|---|---|
80 | 1.846E-05 | 0.002 % | |
70 | 8.283E-05 | 0.007 % | |
60 | 0.0003097 | 0.025 % | |
50 | 0.001027 | 0.084 % | |
40 | 0.003996 | 0.3 % | |
30 | 0.01841 | 1.5 % | |
25 | 0.04008 | 3.3 % | |
20 | 0.08891 | 7.3 % | |
15 | 0.1948 | 15.9 % | |
10 | 0.4135 | 33.8 % | |
9 | 0.4671 | 38.1 % | |
8 | 0.5258 | 42.9 % | |
7 | 0.59 | 48.2 % | |
6 | 0.6601 | 53.9 % | |
5 | 0.7364 | 60.1 % | |
4 | 0.8194 | 66.9 % | |
3 | 0.9093 | 74.2 % | |
2 | 1.007 | 82.2 % | |
1 | 1.112 | 90.8 % | |
0 | 1.225 | 100 % |
Interpolated values:
Altitude (km) | Air Density (kg/m3) | % Sea Level Density | |
---|---|---|---|
80 | 1.846E-05 | 0.002 % | |
79 | 2.49E-05 | 0.002 % | |
78 | 3.133E-05 | 0.003 % | |
77 | 3.777E-05 | 0.003 % | |
76 | 4.421E-05 | 0.004 % | |
75 | 5.064E-05 | 0.004 % | |
74 | 5.708E-05 | 0.005 % | |
73 | 6.352E-05 | 0.005 % | |
72 | 6.996E-05 | 0.006 % | |
71 | 7.639E-05 | 0.006 % | |
70 | 8.283E-05 | 0.007 % | |
69 | 0.00010552 | 0.009 % | |
68 | 0.0001282 | 0.01 % | |
67 | 0.00015089 | 0.012 % | |
66 | 0.00017358 | 0.014 % | |
65 | 0.00019626 | 0.016 % | |
64 | 0.00021895 | 0.018 % | |
63 | 0.00024164 | 0.02 % | |
62 | 0.00026433 | 0.022 % | |
61 | 0.00028701 | 0.023 % | |
60 | 0.0003097 | 0.025 % | |
59 | 0.00038143 | 0.031 % | |
58 | 0.00045316 | 0.037 % | |
57 | 0.00052489 | 0.043 % | |
56 | 0.00059662 | 0.049 % | |
55 | 0.00066835 | 0.055 % | |
54 | 0.00074008 | 0.06 % | |
53 | 0.00081181 | 0.066 % | |
52 | 0.00088354 | 0.072 % | |
51 | 0.00095527 | 0.078 % | |
50 | 0.001027 | 0.084 % | |
49 | 0.0013239 | 0.1 % | |
48 | 0.0016208 | 0.1 % | |
47 | 0.0019177 | 0.2 % | |
46 | 0.0022146 | 0.2 % | |
45 | 0.0025115 | 0.2 % | |
44 | 0.0028084 | 0.2 % | |
43 | 0.0031053 | 0.3 % | |
42 | 0.0034022 | 0.3 % | |
41 | 0.0036991 | 0.3 % | |
40 | 0.003996 | 0.3 % | |
39 | 0.0054374 | 0.4 % | |
38 | 0.0068788 | 0.6 % | |
37 | 0.0083202 | 0.7 % | |
36 | 0.0097616 | 0.8 % | |
35 | 0.011203 | 0.9 % | |
34 | 0.0126444 | 1 % | |
33 | 0.0140858 | 1.1 % | |
32 | 0.0155272 | 1.3 % | |
31 | 0.0169686 | 1.4 % | |
30 | 0.01841 | 1.5 % | |
29 | 0.022744 | 1.9 % | |
28 | 0.027078 | 2.2 % | |
27 | 0.031412 | 2.6 % | |
26 | 0.035746 | 2.9 % | |
25 | 0.04008 | 3.3 % | |
24 | 0.049846 | 4.1 % | |
23 | 0.059612 | 4.9 % | |
22 | 0.069378 | 5.7 % | |
21 | 0.079144 | 6.5 % | |
20 | 0.08891 | 7.3 % | |
19 | 0.110088 | 9 % | |
18 | 0.131266 | 10.7 % | |
17 | 0.152444 | 12.4 % | |
16 | 0.173622 | 14.2 % | |
15 | 0.1948 | 15.9 % | |
14 | 0.23854 | 19.5 % | |
13 | 0.28228 | 23 % | |
12 | 0.32602 | 26.6 % | |
11 | 0.36976 | 30.2 % | |
10 | 0.4135 | 33.8 % | |
9 | 0.4671 | 38.1 % | |
8 | 0.5258 | 42.9 % | |
7 | 0.59 | 48.2 % | |
6 | 0.6601 | 53.9 % | |
5 | 0.7364 | 60.1 % | |
4 | 0.8194 | 66.9 % | |
3 | 0.9093 | 74.2 % | |
2 | 1.007 | 82.2 % | |
1 | 1.112 | 90.8 % | |
0 | 1.225 | 100 % |