Pyro &/or Tony,
Would it be correct to assume these charts are at Sea Level or somewhere around 1000' Pressure Altitude?
I ask because I think it's important for all to remember that as you raise the altitude, atmosphere decreases in density. For example, at 15,000 feet atmospheric density is about 62-63% of Sea Level.
Or am I off target on this?
Range /Ballistics Calculator/ Charted
500 / 2228 / 2210 ~ Equal
600 / 2151 / 2100 ~ 2% increase @ 15k
700 / 2075 / 1970 ~ 5% "
800 / 2001 / 1875 ~ 7% "
900 / 1928 / 1745 ~ 9% "
It would seem that intially the lower air density doesn't affect it that much when comparing the ballistic calculator vs the chart but as range increases it becomes more of a factor.
Just curious.
BTW, Niklas, I ran the 20mm AP 75 numbers through the calculator and it shows the BC as follows for that bullet:
BC (Velocity) Output
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Input Data
Near Velocity: 2610.0 ft/sec
Far Velocity: 2310.0 ft/sec
Distance: 600.000 feet
Temperature: 59.6 °F
Barometric Pressure: 29.92 in Hg
Relative Humidity: 0.0 %
Altitude: 0.0 feet
Air Density: 100 % of Sea Level
--------------------------------------------------------------------------------
Output Data
G1 Ballistic Coefficient: 0.582 Time of Flight: 0.244 sec
[ 07-03-2001: Message edited by: Toad ]