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Laminated launch loop rotors will have good magnetic properties and will rapidly disperse and oxidize in the atmosphere after a rotor-release catastrophe. Laminated launch loop rotors will have good magnetic properties and will rapidly disperse and oxidize in the atmosphere after a rotor-release catastrophe.  Worst case, thin flakes survive and cut.
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The core loss appears proportional to (frequency × flux )² . || [[attachment:2605SA1_coreloss.jpg | {{attachment:2605SA1_coreloss.jpg}}]] || The core loss appears proportional to (frequency × flux )² . ]]

Iron vaporizes at 3140K

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. Worst case, thin flakes survive and cut.

Metglas 2605SA1 looks good, higher temperature than 2605HB1M. datasheet downloaded 2017/02/11

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)

|| attachment:2605SA1_coreloss.jpg || The core loss appears proportional to (frequency × flux )² . ]]

Iron vaporizes at 3140K

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