I get more muzzle velocity out of less powder:
**** Input data: Date: 4-Oct-2009 Time: 15:46:16
Cartridge................. = .338-06 A-Square
Projectile type........... = 8.58, 9., Möller 8,5 mm KJG S with boattail
Max.avg.pressure(Piezo A-S)= 448 MPa Shot start / init pressure = 15 MPa
Projectile weight (g)= 9.007 Groove caliber (mm)= 8.59
Length of cartridge (mm)= 84.84 Length of case (mm)= 63.35
Case capacity (cu.cm)= 4.48 Length of projectile (mm)= 30.48
Length of barrel (mm)= 560
**** Values calculated:
Seating depth (mm)= 8.99 Volume displaced (cu.cm)= 0.52
Comb.chamber volume (cu.cm)= 3.96 Projectile travel (cm)= 50.56
**** Input data:
Propellant type........... = ADI AR 2219
Charge weight...........(g)= 3.732 Load density......(g/cu.cm)= 0.942
Heat of Explosion (kJ/kg)= 4000 Ratio of spec. heats cp/cv = 1.231
Solid density (g/cu.cm)= 1.57 Weighting factor...........= 0.50
Burning rate factor Ba(1/s)= 0.67 Pro-/degressivity factor a = 0.4497
Burning limit ......... z1 = 0.5 Combust.Chamber Vb(m³)= 3.962779E-6
Factor.................. b = 1.6 X-S.Area of Bore A(m²)= 5.695E-5
Bulk density (g/cu.cm)= 0.950 Projectile mass mp(kg)= 9.007E-3
Loading ratio (%)= 99.1 Projectile travel x(m)= 5.0563E-1
**** Results calculated:
Maximum pressure ........ = 430 MPa Way of projectile at Pmax = 37.1 mm
Muzzle velocity ......Ve = 999 m/s Muzzle pressure .......Pe = 60 MPa
Project. energy at muzzle = 4493 J Fraction of powder burnt = 99.7 %
Projectile travel time from 10% Pmax to muzzle = 0.88 ms
**** Input data: Date: 4-Oct-2009 Time: 15:46:16
Cartridge................. = .338-06 A-Square
Projectile type........... = 8.58, 9., Möller 8,5 mm KJG S with boattail
Max.avg.pressure(Piezo A-S)= 448 MPa Shot start / init pressure = 15 MPa
Projectile weight (g)= 9.007 Groove caliber (mm)= 8.59
Length of cartridge (mm)= 84.84 Length of case (mm)= 63.35
Case capacity (cu.cm)= 4.48 Length of projectile (mm)= 30.48
Length of barrel (mm)= 560
**** Values calculated:
Seating depth (mm)= 8.99 Volume displaced (cu.cm)= 0.52
Comb.chamber volume (cu.cm)= 3.96 Projectile travel (cm)= 50.56
**** Input data:
Propellant type........... = ADI AR 2219
Charge weight...........(g)= 3.732 Load density......(g/cu.cm)= 0.942
Heat of Explosion (kJ/kg)= 4000 Ratio of spec. heats cp/cv = 1.231
Solid density (g/cu.cm)= 1.57 Weighting factor...........= 0.50
Burning rate factor Ba(1/s)= 0.67 Pro-/degressivity factor a = 0.4497
Burning limit ......... z1 = 0.5 Combust.Chamber Vb(m³)= 3.962779E-6
Factor.................. b = 1.6 X-S.Area of Bore A(m²)= 5.695E-5
Bulk density (g/cu.cm)= 0.950 Projectile mass mp(kg)= 9.007E-3
Loading ratio (%)= 99.1 Projectile travel x(m)= 5.0563E-1
**** Results calculated:
Maximum pressure ........ = 430 MPa Way of projectile at Pmax = 37.1 mm
Muzzle velocity ......Ve = 999 m/s Muzzle pressure .......Pe = 60 MPa
Project. energy at muzzle = 4493 J Fraction of powder burnt = 99.7 %
Projectile travel time from 10% Pmax to muzzle = 0.88 ms
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