I appears that Nitrochemie do not offer powders for reloaders any more. I will try and verify that tomorrow though. I have calculated two loads for the .338 Federal and the .338 RCM (which I had to fudge on the basis of the .300 RSAUM, since my QuickLoad doesn't have that cartridge yet).
**** Input data: Date: 4-Oct-2009 Time: 13:25:07
Cartridge................. = .338 RCM Fudge II - from .300 RSAUM
Projectile type........... = 8.58, 9., Möller 8,5 mm KJG S with boattail
Max.avg.pressure(Piezo SAA)= 448 MPa Shot start / init pressure = 15 MPa
Projectile weight (g)= 9.01 Groove caliber (mm)= 8.59
Length of cartridge (mm)= 71.76 Length of case (mm)= 50.88
Case capacity (cu.cm)= 4.67 Length of projectile (mm)= 30.48
Length of barrel (mm)= 560
**** Values calculated:
Seating depth (mm)= 9.6 Volume displaced (cu.cm)= 0.55
Comb.chamber volume (cu.cm)= 4.12 Projectile travel (cm)= 51.87
**** Input data:
Propellant type........... = IMR 4895
Charge weight...........(g)= 3.731 Load density......(g/cu.cm)= 0.905
Heat of Explosion (kJ/kg)= 3860 Ratio of spec. heats cp/cv = 1.2431
Solid density (g/cu.cm)= 1.58 Weighting factor...........= 0.50
Burning rate factor Ba(1/s)= 0.61 Pro-/degressivity factor a = -0.15
Burning limit ......... z1 = 0.6 Combust.Chamber Vb(m³)= 4.121772E-6
Factor.................. b = 1.6 X-S.Area of Bore A(m²)= 4.7291E-5
Bulk density (g/cu.cm)= 0.890 Projectile mass mp(kg)= 9.007E-3
Loading ratio (%)= 101.7 Projectile travel x(m)= 5.1871E-1
**** Results calculated:
Maximum pressure ........ = 430 MPa Way of projectile at Pmax = 43.5 mm
Muzzle velocity ......Ve = 978 m/s Muzzle pressure .......Pe = 71 MPa
Project. energy at muzzle = 4310 J Fraction of powder burnt = 99.9 %
Projectile travel time from 10% Pmax to muzzle = 0.96 ms
and
**** Input data: Date: 4-Oct-2009 Time: 13:25:07
Cartridge................. = .338 RCM Fudge II - from .300 RSAUM
Projectile type........... = 8.58, 9., Möller 8,5 mm KJG S with boattail
Max.avg.pressure(Piezo Wil)= 440 MPa Shot start / init pressure = 15 MPa
Projectile weight (g)= 9.01 Groove caliber (mm)= 8.59
Length of cartridge (mm)= 71.12 Length of case (mm)= 51.16
Case capacity (cu.cm)= 4.67 Length of projectile (mm)= 30.48
Length of barrel (mm)= 560
**** Values calculated:
Seating depth (mm)= 10.51 Volume displaced (cu.cm)= 0.55
Comb.chamber volume (cu.cm)= 4.12 Projectile travel (cm)= 51.93
**** Input data:
Propellant type........... = Norma 200
Charge weight...........(g)= 3.031 Load density......(g/cu.cm)= 0.969
Heat of Explosion (kJ/kg)= 3850 Ratio of spec. heats cp/cv = 1.239
Solid density (g/cu.cm)= 1.58 Weighting factor...........= 0.50
Burning rate factor Ba(1/s)= 0.555 Pro-/degressivity factor a = 6.5
Burning limit ......... z1 = 0.3 Combust.Chamber Vb(m³)= 3.126928E-6
Factor.................. b = 2.2 X-S.Area of Bore A(m²)= 5.695E-5
Bulk density (g/cu.cm)= 0.952 Projectile mass mp(kg)= 9.007E-3
Loading ratio (%)= 101.8 Projectile travel x(m)= 5.1934E-1
**** Results calculated:
Maximum pressure ........ = 430 MPa Way of projectile at Pmax = 32.1 mm
Muzzle velocity ......Ve = 948 m/s Muzzle pressure .......Pe = 46 MPa
Project. energy at muzzle = 4047 J Fraction of powder burnt = 100 %
Projectile travel time from 10% Pmax to muzzle = 0.92 ms
So this is pretty much 30m/s more muzzle velocity in exchange for a bigger cartridge, possible problems with sound moderation and maybe greater difficulties getting a licence. OTOH this increases the usable range of the KJG from 200m to just over 250m.
**** Input data: Date: 4-Oct-2009 Time: 13:25:07
Cartridge................. = .338 RCM Fudge II - from .300 RSAUM
Projectile type........... = 8.58, 9., Möller 8,5 mm KJG S with boattail
Max.avg.pressure(Piezo SAA)= 448 MPa Shot start / init pressure = 15 MPa
Projectile weight (g)= 9.01 Groove caliber (mm)= 8.59
Length of cartridge (mm)= 71.76 Length of case (mm)= 50.88
Case capacity (cu.cm)= 4.67 Length of projectile (mm)= 30.48
Length of barrel (mm)= 560
**** Values calculated:
Seating depth (mm)= 9.6 Volume displaced (cu.cm)= 0.55
Comb.chamber volume (cu.cm)= 4.12 Projectile travel (cm)= 51.87
**** Input data:
Propellant type........... = IMR 4895
Charge weight...........(g)= 3.731 Load density......(g/cu.cm)= 0.905
Heat of Explosion (kJ/kg)= 3860 Ratio of spec. heats cp/cv = 1.2431
Solid density (g/cu.cm)= 1.58 Weighting factor...........= 0.50
Burning rate factor Ba(1/s)= 0.61 Pro-/degressivity factor a = -0.15
Burning limit ......... z1 = 0.6 Combust.Chamber Vb(m³)= 4.121772E-6
Factor.................. b = 1.6 X-S.Area of Bore A(m²)= 4.7291E-5
Bulk density (g/cu.cm)= 0.890 Projectile mass mp(kg)= 9.007E-3
Loading ratio (%)= 101.7 Projectile travel x(m)= 5.1871E-1
**** Results calculated:
Maximum pressure ........ = 430 MPa Way of projectile at Pmax = 43.5 mm
Muzzle velocity ......Ve = 978 m/s Muzzle pressure .......Pe = 71 MPa
Project. energy at muzzle = 4310 J Fraction of powder burnt = 99.9 %
Projectile travel time from 10% Pmax to muzzle = 0.96 ms
and
**** Input data: Date: 4-Oct-2009 Time: 13:25:07
Cartridge................. = .338 RCM Fudge II - from .300 RSAUM
Projectile type........... = 8.58, 9., Möller 8,5 mm KJG S with boattail
Max.avg.pressure(Piezo Wil)= 440 MPa Shot start / init pressure = 15 MPa
Projectile weight (g)= 9.01 Groove caliber (mm)= 8.59
Length of cartridge (mm)= 71.12 Length of case (mm)= 51.16
Case capacity (cu.cm)= 4.67 Length of projectile (mm)= 30.48
Length of barrel (mm)= 560
**** Values calculated:
Seating depth (mm)= 10.51 Volume displaced (cu.cm)= 0.55
Comb.chamber volume (cu.cm)= 4.12 Projectile travel (cm)= 51.93
**** Input data:
Propellant type........... = Norma 200
Charge weight...........(g)= 3.031 Load density......(g/cu.cm)= 0.969
Heat of Explosion (kJ/kg)= 3850 Ratio of spec. heats cp/cv = 1.239
Solid density (g/cu.cm)= 1.58 Weighting factor...........= 0.50
Burning rate factor Ba(1/s)= 0.555 Pro-/degressivity factor a = 6.5
Burning limit ......... z1 = 0.3 Combust.Chamber Vb(m³)= 3.126928E-6
Factor.................. b = 2.2 X-S.Area of Bore A(m²)= 5.695E-5
Bulk density (g/cu.cm)= 0.952 Projectile mass mp(kg)= 9.007E-3
Loading ratio (%)= 101.8 Projectile travel x(m)= 5.1934E-1
**** Results calculated:
Maximum pressure ........ = 430 MPa Way of projectile at Pmax = 32.1 mm
Muzzle velocity ......Ve = 948 m/s Muzzle pressure .......Pe = 46 MPa
Project. energy at muzzle = 4047 J Fraction of powder burnt = 100 %
Projectile travel time from 10% Pmax to muzzle = 0.92 ms
So this is pretty much 30m/s more muzzle velocity in exchange for a bigger cartridge, possible problems with sound moderation and maybe greater difficulties getting a licence. OTOH this increases the usable range of the KJG from 200m to just over 250m.
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