External ballistics is the part of the science of ballistics that deals with the behaviour of a non-powered projectile in flight. Ballistics ( gr βάλλειν ('ba'llein' "throw" is the science of Mechanics that deals with the motion behavior and effects of Projectiles External ballistics is frequently associated with firearms, and deals with the behaviour of the bullet after it exits the barrel and before it hits the target. A firearm is a Tool that projects either single or multiple Projectiles at high velocity through a controlled explosion A bullet is a solid Projectile propelled by a Firearm or Air gun and is normally made from metal (usually Lead) For the fictional characters see Gunbarrel (Transformers. A gun barrel is the tube usually Metal, through which a controlled Explosion When in flight, the main forces acting on the projectile are gravity and air resistance. In Physics, a force is whatever can cause an object with Mass to Accelerate. A projectile is any object propelled through space by the exertion of a force which ceases after launch Gravitation is a natural Phenomenon by which objects with Mass attract one another In Fluid dynamics, drag (sometimes called fluid resistance) is the force that resists the movement of a Solid object through a Fluid (a
Gravity imparts a downward acceleration on the projectile, causing it to drop from the line of sight, and the air resistance decelerates the projectile with a force proportional to the square of the velocity (or cube, or even higher powers of v, depending on the speed of the projectile). Line-of-sight propagation refers to Electro-magnetic radiation including light emissions traveling in a straight line Over long periods of flight, these forces have a major impact on the path of the projectile, and must be accounted for when predicting where the projectile will travel.
Target shooters must be very aware of the external ballistics of their bullets. When shooting at long ranges, bullet drop can be measured in tens of feet within the accurate range of many rifle cartridges, so knowledge of the flight characteristics of the bullet and the distance to the target are essential for accurate long range shooting. Bullet drop is the name given to the tendency of a Bullet to drop in flight due to the effect of gravity A rifle is a Firearm designed to be fired from the shoulder with a barrel that has a helical groove or pattern of grooves ("rifling" cut into the barrel walls At extremely long ranges, artillery must fire projectiles along trajectories that are not even approximately straight; they are closer to parabolic, although air resistance affects this. Artillery (from French artillerie) is a military Combat Arm which employs any apparātus machine In Mathematics, the parabola (pəˈræbələ from the Greek παραβολή) is a Conic section, the intersection of a right circular For the longer ranges and flight times, the Coriolis effect becomes important. In physics the Coriolis effect is an apparent deflection of moving objects when they are viewed from a Rotating frame of reference. In the case of ballistic missiles, the altitudes involved have a significant effect as well, with part of the flight taking place in a near-vacuum. A ballistic missile is a Missile that follows a Sub-orbital ballistic flightpath with the objective of delivering a warhead to a predetermined target
Mathematical models for calculating the effects of air resistance are quite complex and for the simpler mathematical models not very reliable beyond 500 m (500 yd), so the most reliable method of establishing trajectories is still by empirical measurement. Note The term model has a different meaning in Model theory, a branch of Mathematical logic. Trajectory is the path a moving object follows through space The object might be a Projectile or a Satellite, for example
Use of ballistics tables or ballistics software based on the Siacci/Mayevski G1 drag model, introduced in 1881, are the most common method used to work with external ballistics. Bullets are described by a ballistic coefficient, or BC, which combines the air resistance of the bullet shape (the drag coefficient) and its sectional density (a function of mass and bullet diameter). The ballistic coefficient ( BC) of a body is a measure of its ability to overcome air resistance in flight The drag coefficient ( Cd, Cx or Cw) is a Dimensionless quantity that describes how streamlined an Sectional density is the ratio of an object's weight to its cross-sectional area
The deceleration due to drag that a projectile with mass m, velocity v, and diameter d will experience is proportional to BC, 1/m, v² and d². In Fluid dynamics, drag (sometimes called fluid resistance) is the force that resists the movement of a Solid object through a Fluid (a The BC gives the ratio of ballistic efficiency compared to the standard G1 projectile, which is a 1 pound (454 g), 1 inch (25. 4 mm) diameter bullet with a flat base, a length of 3 inches (76. 2 mm), and a 2 inch (50. 8 mm) radius tangential curve for the point.
Sporting bullets, with a calibre d ranging from 0. The term caliber or calibre designates the interior Diameter of a tube or the exterior diameter of a wire or rod 177 to 0. 50 inches (4. 50 to 12.7 mm), have BC’s in the range 0. 12 to slightly over 1. 00, with 1. 00 being the most aerodynamic, and 0. 12 being the least. Very-low-drag bullets with BC's ≥ 1. Very-low-drag bullets (VLD are primarily a Small arms Ballistics development of the 1980s–1990s driven by shooters' desire for bullets that will give a higher degree 10 can be designed and produced on CNC precision lathes out of mono-metal rods, but they often have to be fired from custom made full bore rifles with special barrels[1].
Sectional density is a very important aspect of a bullet, and is the ratio of frontal surface area (half the bullet diameter squared, times pi) to bullet mass. Sectional density is the ratio of an object's weight to its cross-sectional area IMPORTANT NOTICE Please note that Wikipedia is not a database to store the millions of digits of π please refrain from adding those to Wikipedia as it could cause technical problems Since, for a given bullet shape, frontal surface increases as the square of the calibre, and mass increases as the cube of the diameter, then sectional density grows linearly with bore diameter. Since BC combines shape and sectional density, a half scale model of the G1 projectile will have a BC of 0. A scale model is a representation or copy of an object that is larger or smaller than the actual size of the object. 5, and a quarter scale model will have a BC of 0. 25.
Since different projectile shapes will respond differently to changes in velocity (particularly between supersonic and subsonic velocities), a BC provided by a bullet manufacturer will be an average BC that represents the common range of velocities for that bullet. For other uses see Supersonic. The term supersonic is used to define a speed that is over the Speed of sound ( Mach 1 For rifle bullets, this will probably be a supersonic velocity, for pistol bullets it will be probably be subsonic. A rifle is a Firearm designed to be fired from the shoulder with a barrel that has a helical groove or pattern of grooves ("rifling" cut into the barrel walls For other uses see Supersonic. The term supersonic is used to define a speed that is over the Speed of sound ( Mach 1 For projectiles that travel through the supersonic, transonic and subsonic flight regimes BC is not well approximated by a single constant, but is considered to be a function BC(M) of the Mach number M; here M equals the projectile velocity divided by the speed of sound. For other uses see Supersonic. The term supersonic is used to define a speed that is over the Speed of sound ( Mach 1 Transonic is an Aeronautics term referring to a range of velocities just below and above the Speed of sound (about mach 0 The Mathematical concept of a function expresses dependence between two quantities one of which is given (the independent variable, argument of the function Mach number (\mathrm{Ma} or M (generally ˈmɑːk sometimes /ˈmɑːx/ or /ˈmæk/ is the speed of an object moving through air or any Fluid Sound is a vibration that travels through an elastic medium as a Wave. During the flight of the projectile the M will decrease, and therefore (in most cases) the BC will also decrease.
Most ballistic tables or software takes for granted that one specific drag function correctly describes the drag and hence the flight characteristics of a bullet related to its ballistics coefficient. Those models do not differentiate between flat-based, spitzer, boat-tail, very-low-drag, etc. Very-low-drag bullets (VLD are primarily a Small arms Ballistics development of the 1980s–1990s driven by shooters' desire for bullets that will give a higher degree bullet types. They assume one invariable drag function as indicated by the published BC. These resulting drag curve models are referred to as the Ingalls, G1 (by far the most popular), G2, G5, G6, G7, G8, GI and GL drag curves.
How different speed regimes affect . 338 calibre rifle bullets can be seen in the . 338 Lapua Magnum product brochure which states Doppler radar established BC data. [2] The reason for publishing data like in this brochure is that the Siacci/Mayevski G1 model can not be tuned for the drag behaviour of a specific projectile. Some ballistic software designers, who based their programs on the Siacci/Mayevski G1 model, give the user the possibility to enter several different BC constants for different speed regimes to calculate ballistic predictions that closer match a bullets flight behaviour at longer ranges compared to calculations that use only one BC constant.
Besides the traditional Siacci/Mayevski G1 drag model other more advanced drag models exist. The most prominent alternative ballistic model is probably the model presented in 1980 by Prof. Dr. Arthur J. Pejsa. Mr. Pejsa claims on his website that his method was consistently capable of predicting (supersonic) rifle bullet trajectories within 2. 54 mm (0. 1 in) and bullet velocities within 0. 3048 m/s (1 ft/s) out to 914. 4 m (1000 yd) when compared to dozens of actual measurements. [3]
The Pejsa model is an analytic closed-form solution that does not use any tables or fixed drag curves generated for standard-shaped projectiles. The Pejsa method uses the G1-based ballistic coefficient as published, and incorporates this in a Pejsa retardation coefficient function in order to model the retardation behaviour of the specific projectile. Since it effectively uses an analytic function (drag coefficient modelled as a function of the Mach number) in order to match the drag behaviour of the specific bullet the Pesja method does not need to rely on any prefixed assumption. The drag coefficient ( Cd, Cx or Cw) is a Dimensionless quantity that describes how streamlined an Mach number (\mathrm{Ma} or M (generally ˈmɑːk sometimes /ˈmɑːx/ or /ˈmæk/ is the speed of an object moving through air or any Fluid
Besides the mathematical retardation coefficient function, Pejsa added an extra slope constant factor that accounts for the more subtle change in retardation rate downrange of different bullet shapes and sizes. It ranges from 0. 1 (flat-nose bullets) to 0. 9 (very-low-drag bullets). Very-low-drag bullets (VLD are primarily a Small arms Ballistics development of the 1980s–1990s driven by shooters' desire for bullets that will give a higher degree If this deceleration constant factor is unknown a default value of 0. 5 will predict the flight behaviour of most modern spitzer-type rifle bullets quite well. With the help of test firing measurements the slope constant for a particular bullet/rifle system/shooter combination can be determined. These test firings should preferably be executed at 60% and for extreme long range ballistic predictions also at 80% to 90% of the supersonic range of the projectiles of interest, staying away from erratic transonic effects. With this the Pejsa model can easily be tuned for the specific drag behaviour of a specific projectile, making significant better ballistic predictions for ranges beyond 500 m (547 yd) possible.
Some software developers offer commercial software which is based on the Pejsa drag model enhanced and improved with refinements to account for normally minor effects (Coriolis, gyroscopic drift, etc. ) that come in to play at long range. The developers of these enhanced Pejsa models designed these programs for ballistic predictions beyond 1000 m (1094 yd). [4][5]
There are also advanced professional ballistic models like PRODAS available. These are based on 6 Degrees Of Freedom (6 DOF) calculations. 6 DOF modelling needs such elaborate input, knowledge of the employed projectiles and long calculation time on computers that it is unpractical for non-professional ballisticians and field use where calculations generally have to be done on the fly on PDA's with relatively modest computing power. 6 DOF is generally used by military organizations that study the ballistic behaviour of a limited number of (intended) military issue projectiles. Calculated 6 DOF trends can be incorporated as correction tables in more conventional ballistic software applications.
For the precise establishment of BC's or maybe scientifically better expressed drag coefficients Doppler radar-measurements are required. The drag coefficient ( Cd, Cx or Cw) is a Dimensionless quantity that describes how streamlined an A doppler radar is a Radar using the Doppler effect of the returned echoes from targets to measure their Radial velocity. Weibel 1000e Doppler radars are used by governments, professional ballisticians, defence forces and a few ammunition manufacturers to obtain real world data of the flight behaviour of projectiles of their interest. A doppler radar is a Radar using the Doppler effect of the returned echoes from targets to measure their Radial velocity. Correctly established state of the art Doppler radar measurements can determine the flight behaviour of projectiles as small as airgun pellets in three-dimensional space to within a few millimetres accuracy.
Doppler radar measurement results for a lathe turned monolithic solid . 50 BMG very-low-drag bullet (Lost River J40 . Very-low-drag bullets (VLD are primarily a Small arms Ballistics development of the 1980s–1990s driven by shooters' desire for bullets that will give a higher degree 510-773 grain monolithic solid bullet / twist rate 1:15 in) look like this:
| Range (m) | 500 | 600 | 700 | 800 | 900 | 1000 | 1100 | 1200 | 1300 | 1400 | 1500 | 1600 | 1700 | 1800 | 1900 | 2000 |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| Ballistic coefficient | 1. 040 | 1. 051 | 1. 057 | 1. 063 | 1. 064 | 1. 067 | 1. 068 | 1. 068 | 1. 068 | 1. 066 | 1. 064 | 1. 060 | 1. 056 | 1. 050 | 1. 042 | 1. 032 |
The initial rise in the BC value is attributed to a projectiles always present yaw and precession out of the bore. The test results were obtained from many shots not just a single shot. The bullet was assigned 1. 062 for its BC number by the bullet's manufacturer Lost River Ballistic Technologies.
In general, a pointed bullet will have a better ballistic coefficient (BC) than a round nosed bullet, and a round nosed bullet will have a better BC than a flat point bullet. The ballistic coefficient ( BC) of a body is a measure of its ability to overcome air resistance in flight Large radius curves, resulting in a shallower point angle, will produce lower drags, particularly at supersonic velocities. Hollow point bullets behave much like a flat point of the same point diameter. A hollow point is a Bullet that has a pit or hollowed out shape in its tip generally intended to cause the bullet to expand upon entering a target in order to decrease Bullets designed for supersonic use often have a slight taper at the rear, called a boat tail, which further reduces drag. Cannelures, which are recessed rings around the bullet used to crimp the bullet securely into the case, will cause an increase in drag.
When the velocity of a rifle bullet fired at supersonic muzzle velocity approaches the speed of sound it enters the transonic region. For other uses see Supersonic. The term supersonic is used to define a speed that is over the Speed of sound ( Mach 1 Transonic is an Aeronautics term referring to a range of velocities just below and above the Speed of sound (about mach 0 In the transonic region, an important thing that happens to most bullets, is that the centre of pressure (CP) shifts forward as the bullet decelerates. That CP shift affects the (dynamic) stability of the bullet. If the bullet is not well stabilized, it can not remain pointing forward through the transonic region (the bullets starts to exhibit an unwanted coneing motion that, if not dampened out, can eventually end in uncontrollable tumbling along the length axis). However, even if the bullet has sufficient stability (static and dynamic) to be able to fly through the transonic region and stays pointing forward, it is still affected. The erratic and sudden CP shift and (temporary) decrease of dynamic stability can cause significant dispersion (and hence significant accuracy decay), even if the bullet's flight becomes well behaved again when it enters the subsonic region. This makes accurately predicting the ballistic behaviour of bullets in the transonic region very hard. Because of this marksmen normally restrict themselves to engaging targets within the supersonic range of the bullet used. [6]
Ballistic prediction computer programs intended for (extreme) long ranges can be evaluated by conducting field tests at the supersonic to subsonic transition range (the last 10 to 20 % of the supersonic range of the rifle/cartridge/bullet combination). For a typical . 338 Lapua Magnum rifle for example, shooting standard 16. 2 gram (250 gr) Lapua Scenar GB488 bullets at 905 m/s (2969 ft/s) muzzle velocity, field testing of the software should be done at ≈ 1200 - 1300 meters (1312 - 1422 yd) under International Standard Atmosphere sea level conditions (air density ρ = 1. The International Standard Atmosphere (ISA is an atmospheric model of how the Pressure, Temperature, Density, and Viscosity The density of air, ρ (Greek rho (air density is the mass per unit volume of Earth's atmosphere, and is a useful value in Aeronautics. 225 kg/m³). To check how well the software predicts the trajectory at shorter to medium ranges field tests at 20, 40 and 60% of the supersonic range have to be conducted. At those shorter to medium ranges transsonic problems and hence unbehaved bullet flight should not occur and the BC is less likely to be very transient. Testing the predicative qualities of software at (extreme) long ranges is expensive because it consumes quite some ammunition and the actual muzzle velocity of all shots fired has to be measured to be able to make statistically dependable statements. Sample groups of less than 24 shots do not obtain statistically dependable enough data.
Governments, professional ballisticians, defence forces and a few ammunition manufacturers can use Doppler radars to obtain exact real world data regarding the flight behaviour of the specific projectiles of their interest and thereupon compare the gathered real world data against the predictions calculated by ballistic computer programs. The normal shooting or aerodynamics enthusiast however has no access to such expensive professional measurement devices and authorities and projectile manufacturers are generally reluctant to share the results of Doppler radar tests and the test derived drag coefficients of projectiles with the general public. The drag coefficient ( Cd, Cx or Cw) is a Dimensionless quantity that describes how streamlined an
Wind has a range of effects, the first being the effect of making the bullet deviate to the side. From a scientific perspective, the "wind pushing on the side of the bullet" is not what causes wind drift. What causes wind drift is drag. Drag makes the bullet turn into the wind, keeping the centre of air pressure on its nose. This causes the nose to be cocked (from your perspective) into the wind, the base is cocked (from your perspective) "downwind. " So, (again from your perspective), the drag is pushing the bullet downwind making bullets follow the wind. A somewhat less obvious effect is caused by head or tailwinds. A headwind will slightly increase the relative velocity of the projectile, and increase drag and the corresponding drop. In Kinematics, relative velocity is the vector difference between the velocities of two objects as evaluated in terms of a single Coordinate A tailwind will reduce the drag and the bullet drop. In the real world pure head or tailwinds are rare, since wind seldom is constant in force and direction and normally interacts with the terrain it is blowing over. This often makes ultra long range shooting in head or tailwind conditions hard.
Air temperature, pressure, altitude and humidity variations make up the ambient air density. Temperature is a physical property of a system that underlies the common notions of hot and cold something that is hotter generally has the greater temperature Pressure (symbol 'p' is the force per unit Area applied to an object in a direction perpendicular to the surface Altitude is the Elevation of a point or object from a known level or datum (plural data Humidity is the amount of water vapor in the air In daily language the term "humidity" is normally taken to mean Relative humidity. The density of air, ρ (Greek rho (air density is the mass per unit volume of Earth's atmosphere, and is a useful value in Aeronautics. Decreased air density will result in a decrease in drag, and increased air density will result in a rise in drag. Humidity has a counter intuitive impact. Since water vapor has a density of 0. General properties of water vapor Evaporation/sublimation Whenever a water molecule leaves a surface it is said to have evaporated 8 grams per litre, while dry air averages about 1. 225 grams per litre, higher humidity actually decreases the air density, and therefore decreases the drag.
The vertical angle (or elevation) of a shot will also affect the trajectory of the shot. pair of Angles is said to be vertical (US English or opposite (British English if the angles share the same vertex and are bounded by the same pair of For other senses of this word see Elevation (disambiguation. In Ballistics, the elevation is the Angle between the Ballistic tables for small calibre projectiles (fired from pistols or rifles) assume that gravity is acting nearly perpendicular to the bullet path. If the angle is up or down, then the perpendicular acceleration will actually be less. The effect of the path wise acceleration component will be negligible, so shooting up or downhill will both result in a similar decrease in bullet drop.
Even in complete calm air, with no sideways air movement at all, a bullet will experience a spin induced sideways component. For a right hand (clockwise) direction of rotation this component will always be to the right. This is because the bullet's longitudinal axis and the direction of the velocity of the center of gravity (CG) deviate by a small angle, which is said to be the equilibrium yaw or the yaw of repose. Flight dynamics is the science of air and space vehicle orientation and control in three dimensions For right-handed (clockwise) spin bullets, the bullet's axis of symmetry generally points to the right and a little bit upward with respect to the direction of the velocity vector. As an effect of this small inclination, there is a continuous air stream, which tends to deflect the bullet to the right. Thus the occurrence of the yaw of repose is the reason for bullet drift to the right (for right-handed spin) or to the left (for left-handed spin). This means that the bullet is "skidding" sideways at any given moment, and thus experiencing a sideways component. [7]
Spin stabilized projectiles are affected by the Magnus effect, whereby the spin of the bullet creates a force acting either up or down, perpendicular to the sideways vector of the wind. The Magnus effect is the phenomenon whereby a spinning object flying in a Fluid creates a Whirlpool of fluid around itself and experiences a force perpendicular In the simple case of horizontal wind, and a right hand (clockwise) direction of rotation, the Magnus effect induced pressure differences around the bullet cause a downward force to act on the projectile, affecting its point of impact. [8]
The Magnus effect has a significant role in bullet stability because the Magnus force does not act upon the bullet's center of gravity, but the center of pressure affecting the yaw of the bullet. The Magnus effect will act as a destabilizing force on any bullet with a center of pressure located ahead of the center of gravity, while conversely acting as a stabilizing force on any bullet with the center of pressure located behind the center of gravity. The location of the center of pressure depends on the flow field structure, in other words, depending on whether the bullet is in supersonic, transonic or subsonic flight. What this means in practice depends on the shape and other attributes of the bullet, in any case the Magnus force greatly affects stability because it tries to "twist" the bullet along its flight path. [9][10]
Paradoxically very-low-drag bullets due to their length have a tendency to exhibit greater Magnus errors because they have a greater surface area to present to the oncoming air they are travelling through, thereby reducing their BC value. Very-low-drag bullets (VLD are primarily a Small arms Ballistics development of the 1980s–1990s driven by shooters' desire for bullets that will give a higher degree This subtle effect is one of the reasons why a calculated BC based on shape and sectional density is of limited use.
Another minor cause of drift, which depends on the nose of the projectile being above the trajectory, is the Poisson Effect. This, if it occurs at all, acts in the same direction as the gyroscopic drift and is even less important than the Magnus drift. It supposes that the uptilted nose of the projectile causes an air cushion to build up underneath it. It further supposes that there is an increase of friction between this cushion and the projectile so that the latter, with its spin, will tend to roll off the cushion and move sideways.
This simple explanation is quite popular. There is, however, no evidence to show that increased pressure means increased friction and unless this is so, there can be no effect. Even if it does exist it must be quite insignificant compared with the gyroscopic and Coriolis drifts.
Both the Poisson and Magnus Effects will reverse their directions of drift if the nose falls below the trajectory. When the nose is off to one side, as in equilibrium yaw, these effects will make minute alterations in range.
The coordinate system that is used to specify the location of the point of firing and the location of the target is the system of latitudes and longitudes, which is in fact a rotating coordinate system, since the Earth is rotating. In Mathematics and its applications a coordinate system is a system for assigning an n - Tuple of Numbers or scalars to each point For small arms, this rotation is generally insignificant, but for ballistic projectiles with long flight times, such as extreme long-range rifle projectiles, artillery and intercontinental ballistic missiles, it is a significant factor in calculating the trajectory. Small arms is a term used by the Armed forces to refer to Infantry Weapons such as the Firearms that an individual soldier can carry Artillery (from French artillerie) is a military Combat Arm which employs any apparātus machine During its flight, the projectile moves in a straight line (not counting gravitation and air resistance for now). Since the target is co-rotating with the Earth, it is in fact a moving target, relative to the projectile, so in order to hit it the gun must be aimed to the point where the projectile and the target will arrive simultaneously.
When the straight path of the projectile is plotted in the rotating coordinate system that is used, then this path appears as curvilinear. Curvilinear coordinates are a Coordinate system for the Euclidean space based on some transformation that converts the standard Cartesian coordinate system to a coordinate The fact that the coordinate system is rotating must be taken into account, and this is achieved by adding terms for a "centrifugal force" and a "Coriolis effect" to the equations of motion. In physics the Coriolis effect is an apparent deflection of moving objects when they are viewed from a Rotating frame of reference. When the appropriate Coriolis term is added to the equation of motion the predicted path with respect to the rotating coordinate system is curvilinear, corresponding to the actual straight line motion of the projectile.
For an observer with his frame of reference in the northern hemisphere Coriolis makes the projectile appear to curve over to the right. Actually it is not the projectile swinging to the right but the earth (frame of reference) swinging to the left which produces this result. The opposite will seem to happen in the southern hemisphere. The Coriolis effect is latitude dependent and is at its maximum at the poles and negligible at the equator of the Earth. Latitude, usually denoted symbolically by the Greek letter phi ( Φ) gives the location of a place on Earth (or other planetary body north or south of the The equator (sometimes referred to colloquially as "the Line") is the intersection of the Earth 's surface with the plane perpendicular to the EARTH was a short-lived Japanese vocal trio which released 6 singles and 1 album between 2000 and 2001 The reason for this is that the Coriolis effect depends on the vector of the angular velocity of the earth´s rotation with respect to xyz - coordinate system (frame of reference).
Lateral jump is caused by a slight lateral and rotational movement of the barrel at the instant of firing. It has the effect of a small error in bearing. The effect is ignored, since it is small and varies from round to round.
The maximum practical range[11] of all small arms and especially high-powered sniper rifles depends mainly on the aerodynamic or ballistic efficiency of the spin stabilised projectiles used. In Military and Law enforcement terminology a sniper rifle is a Rifle used to ensure Accurate placement of Bullets at longer Long-range shooters must also collect relevant information to calculate elevation and windage corrections to be able to achieve first shot strikes. The data to calculate these fire control corrections has a long list of variables including[12]:
The ambient air density is at its maximum at Arctic sea level conditions. Temperature is a physical property of a system that underlies the common notions of hot and cold something that is hotter generally has the greater temperature Pressure (symbol 'p' is the force per unit Area applied to an object in a direction perpendicular to the surface Altitude is the Elevation of a point or object from a known level or datum (plural data Humidity is the amount of water vapor in the air In daily language the term "humidity" is normally taken to mean Relative humidity. The density of air, ρ (Greek rho (air density is the mass per unit volume of Earth's atmosphere, and is a useful value in Aeronautics. Earth's gravity, denoted by g, refers to the Gravitational attraction that the Earth exerts on objects on or near its surface Latitude, usually denoted symbolically by the Greek letter phi ( Φ) gives the location of a place on Earth (or other planetary body north or south of the Altitude is the Elevation of a point or object from a known level or datum (plural data A gyroscope is a device for measuring or maintaining orientation, based on the principles of Angular momentum. The Magnus effect is the phenomenon whereby a spinning object flying in a Fluid creates a Whirlpool of fluid around itself and experiences a force perpendicular In physics the Coriolis effect is an apparent deflection of moving objects when they are viewed from a Rotating frame of reference. Latitude, usually denoted symbolically by the Greek letter phi ( Φ) gives the location of a place on Earth (or other planetary body north or south of the Cold gunpowder also produces lower pressures and hence lower muzzle velocities than warm powder. Gunpowder is a an explosive mixture of Sulfur, Charcoal and Potassium nitrate (also known as saltpetre/saltpeter that burns rapidly producing volumes This means that the maximum practical range of rifles will be at it shortest at Arctic sea level conditions.
The ability to hit a target at great range has a lot to do with the ability to tackle environmental and meteorological factors and a good understanding of exterior ballistics and the limitations of equipment. Without computer support and highly accurate laser range-finders and meteorological measuring equipment as aids to calculate ballistic solutions, long-range shooting beyond 1000 m (1100 yd) becomes guesswork for even the most expert long-range marksmen. [13]
Interesting further reading: Marksmanship Wikibook
Here is an example of a ballistic table for a . 30 calibre Speer 169 grain (11 g) pointed boat tail match bullet, with a BC of 0. 480. It assumes sights 1. 5 inches (38 mm) above the bore line, and sights adjusted to result in point of aim and point of impact matching 200 yards (183 m) and 300 yards (274 m) respectively. Point of Impact is a 1993 Thriller novel by award-winning author Stephen Hunter.
| Range | 0 | 100 yd (91 m) |
200 yd (183 m) |
300 yd (274 m) |
400 yd (366 m) |
500 yd (457 m) |
|
|---|---|---|---|---|---|---|---|
| Velocity | ft/s | 2700 | 2512 | 2331 | 2158 | 1992 | 1834 |
| m/s | 823 | 766 | 710 | 658 | 607 | 559 | |
| Zeroed for 200 yards (184 m) | |||||||
| Height | in | -1. The foot per second (plural feet per second) is a unit of both Speed (scalar and Velocity (vector quantity which includes direction Inches redirects here To see the Les Savy Fav album see Inches. 5 | 2. 0 | 0 | -8. 4 | -24. 3 | -49. 0 |
| mm | -38 | 51 | 0 | -213 | -617 | -1245 | |
| Zeroed for 300 yards (274 m) | |||||||
| Height | in | -1. 5 | 4. 8 | 5. 6 | 0 | -13. 1 | -35. 0 |
| mm | -38 | 122 | 142 | 0 | -333 | -889 | |
This table demonstrates that, even with a very aerodynamic bullet fired at high velocity, the "bullet drop" or change in the point of impact is significant. This change in point of impact has two important implications. Firstly, estimating the distance to the target is critical at longer ranges, because the difference in the point of impact between 400 and 500 yd (460 m) is 25–32 in (depending on zero), in other words if the shooter estimates that the target is 400 yd away when it is in fact 500 yd away the shot will impact 25–32 in (635–813 mm) below where it was aimed, possibly missing the target completely. Secondly, the rifle should be zeroed to a distance appropriate to the typical range of targets, because the shooter might have to aim so far above the target to compensate for a large bullet drop that he may lose sight of the target completely (for instance being outside the field of view of a telescopic site). In the example of the rifle zeroed at 200 yd (180 m), the shooter would have to aim 49 in or more than 4 ft (1. 2 m) above the point of impact for a target at 500 yd.
accurateshooter.com Ballistics section links to / hosts these 4 freeware external ballistics computer programs:
General external ballistics
Small arms external ballistics
Artillery external ballistics
Doppler radar tracking systems