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Revision 1 as of 2017-02-11 21:58:59
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Revision 2 as of 2017-02-11 23:19:17
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||<-2:> '''Metglas 2605SA1''' ||
|| Curie temperature || 395C / 668K ||
|| saturation induction || 1.56 Tesla ||
|| resistivity || 1.3 μΩ-m ||
||
thickness || 23 μm ||
|| density || 7.18 g/m³ ||
|| Tensile Strength || 1 GPa ||
|| Elastic Modulus || 100 GPa ||
|| Thermal Expansion || 7.6 ppm/°C ||
||
Iron || 85 to 95% ||
|| Silicon || 5 to 10% ||
|| Boron || 1 to 5% ||
||<-2> 60 Hz and 1.4 T ||
|| Induction at 80 A/m || ≥1.35 T ||
|| Core Loss || ≤0.17 W/kg ||
||Exciting Apparent Power* || 1.1 (VA/kg) ||
||<-5:> '''Metglas 2605SA1'''                                               ||
|| Curie temperature || 395C / 668K || || saturation induction || 1.56 Tesla ||
|| thickness || 23 μm || || density || 7.18 g/cm³ ||
|| Thermal Expansion || 7.6 ppm/°C || ||<-2> ||
|| Tensile Strength || 1 GPa || || Elastic Modulus || 100 GPa ||
|| Iron || 85 to 95% || || [[ https://www.cdc.gov/niosh/npg/npgd0344.html | IDLH Fe₂O₃]] || 2.5g/m³ ||
|| Silicon || 5 to 10% || || [[ https://www.cdc.gov/niosh/npg/npgd0552.html | IDLH SiO₂]] || 3.0g/m³ ||
|| Boron || 1 to 5% || || [[ https://www.cdc.gov/niosh/idlh/1303862.html | IDLH B₂O₃]] || 2,0g/m³ ||
|| resistivity || 1.3 μΩ-m || ||<-2>                                     ||
||<-2>
60 Hz and 1.4 T || || Induction at 80 A/m || ≥1.35 T ||
|| Core Loss || ≤0.17 W/kg || ||Exciting Apparent Power* || 1.1 (VA/kg) ||
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Rotor Lamination

Laminated launch loop rotors will have good magnetic properties and will rapidly disperse and oxidize in the atmosphere after a rotor-release catastrophe.

Metglas 2605SA1

Curie temperature

395C / 668K

saturation induction

1.56 Tesla

|| thickness || 23 μm || || density || 7.18 g/cm³ ||

Thermal Expansion

7.6 ppm/°C

Tensile Strength

1 GPa

Elastic Modulus

100 GPa

Iron

85 to 95%

IDLH Fe₂O₃

2.5g/m³

Silicon

5 to 10%

IDLH SiO₂

3.0g/m³

Boron

1 to 5%

IDLH B₂O₃

2,0g/m³

resistivity

1.3 μΩ-m

60 Hz and 1.4 T

Induction at 80 A/m

≥1.35 T

Core Loss

≤0.17 W/kg

Exciting Apparent Power*

1.1 (VA/kg)

The core loss appears proportional to (frequency × flux )² .

RotorLamination (last edited 2017-10-21 17:03:39 by KeithLofstrom)