Defense Intelligence Reference Document Advanced Nuclear Propulsion For Manned Deep Space Missions

UNCLASSIFIED//P&I\ &I I ICIAL USE 014Lf
For a conductor with a radius of )._ ~10m = 103 cm, an example for a small starship
configuration, one can reach a voltage on the order of EA ~ 6 x 109 volts.
INDUCTIVE CHARGING
To charge the spacecraft to the required gigavolt potentials, we choose for its
architecture a large but hollow cylinder, which at the same time acts as a large
magnetic field coil. If thermionic electron emitters are placed inside this coil and the
w w
magnetic field of the coil rises in time, Maxwell's equation Vx E = -(1/r)OB/at induces
an azimuthal electric field inside the coil:
r •
E ~--B-
¢ 2c ' (2)
where B = Bz is directed along the z-axis, with r the radial distance from the axis of the
coil. In combination with the axial magnetic field, the electrons from the thermionic
emitters make a radial inward-directed motion
E,p r B_
l' =C-=----
' B_ 2 B (3)
By Maxwell's equation div if= 41Z11e'JP, this leads to the buildup of an electron cloud inside
the cylinder, resulting in the radial electric field
E,. = 2mier (4)
This radial electric field leads to an additional azimuthal drift motion
(5)
superimposed on the radially directed inward drift motion vr.
For the newly formed electron cloud to be stable, its maximum electron number density
must be below the Brillouin limit:
n < nmax = 8 2/ 4n mc:2
where mc2 = 8.2 x 10- 7 erg is the electron rest mass energy. For B = 2x 104G, one
finds that nmax z 4x 1013 cm· 3 . To reach with a cylindrical electron cloud of radius Ra
4
UNCLASSIFIED/;«F81it 8FFIIIAI!: 1!181! &••1::Y
( 6)