If M�ller's design assumptions are correct the LM-107 projectile with a calculated G1 BC of 1.02 will offer a supersonic range of H " at a muzzle velocity of under International Standard Atmosphere sea level conditions ( air density ? = 1.225 kg / m 3 ).
42.
At muzzle velocity the " s . S . Patrone " had a maximum range of approximately and retained supersonic velocity up to and past ( V 1000 H " Mach 1.07 ) under ICAO Standard Atmosphere conditions at sea level ( air density ? = 1.225 kg / m 3 ).
43.
The NASA Earth Global Reference Atmospheric Model ( Earth-GRAM ) was developed by the Marshall Space Flight Center to provide a design reference atmosphere that, unlike the standard atmospheres, allows for geographical variability, a wide range of altitudes ( surface to orbital altitudes ), and monthly variability for four different times of day.
44.
At sea level in the International Standard Atmosphere ( ISA ) and at low speeds where air compressibility is negligible ( i . e ., assuming a constant air density ), IAS corresponds to TAS . When the air density or temperature around the aircraft differs from standard sea level conditions, IAS will no longer correspond to TAS, thus it will no longer reflect aircraft performance.
45.
Diethylene glycol dinitrate is a colorless, odorless, viscous, oily liquid, with specific gravity 1.4092 at 0 �C and 1.3846 at 20 �C; freezing point " 11.5 �C under a standard atmosphere; the theoretical boiling point of approximately 197 �C difficult to confirm as the compound begins to decompose and spontaneously inflames at or slightly below this temperature.
46.
Density altitude is the altitude relative to the standard atmosphere conditions ( International Standard Atmosphere ) at which the air density would be equal to the indicated air density at the place of observation, or, in other words, the height when measured in terms of the density of the air rather than the distance from the ground . " Density Altitude " is the pressure altitude adjusted for non-standard temperature.
47.
Density altitude is the altitude relative to the standard atmosphere conditions ( International Standard Atmosphere ) at which the air density would be equal to the indicated air density at the place of observation, or, in other words, the height when measured in terms of the density of the air rather than the distance from the ground . " Density Altitude " is the pressure altitude adjusted for non-standard temperature.
48.
According to JBM Ballistics, using the G7 ballistic coefficient provided by Bryan Litz, the 7.62mm M118 Long Range 7.62?1mm NATO cartridge, when fired at its nominal muzzle velocity of 786 m / s ( 2, 580 ft / s ), should have approximately supersonic range under International Standard Atmosphere conditions at sea level ( air density ? = 1.225 kg / m 3 ).
49.
For a typical . 375 CheyTac chambered gun, shooting 24.30 gram ( 375 gr ) Lost River Ballistic Technologies bullets ( claimed G1 BC = 1.02 ) at 930 m / s ( 3050 ft / s ) muzzle velocity, the supersonic range would be 2230 m ( 2440 yd ) under International Standard Atmosphere sea level conditions ( air density ? = 1.225 kg / m?).
50.
According to JBM Ballistics, using drag coefficients ( C d ) provided by Lapua, the L115A3 has an approximate supersonic range ( speed of sound = 340.3 m / s ) of under International Standard Atmosphere conditions at sea level ( air density ? = 1.225 kg / m 3 ) and at the altitude or elevation ( air density ? = 1.1069 kg / m 3 ) of Musa Qala.
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