1. A method for producing synchrotron radiation, comprising: providing a liner having a first end, a second end, a liner axis, and a lumen extending along the liner axis and being bound by interior reflective walls of the liner; introducing charged particle beam into the first end of the liner such that the beam propagates through the lumen from the first end to the second end as the beam reflects multiple times from the interior walls of the liner; and applying an implosive force to the liner as the beam propagates through the lumen of the liner, the implosive force serving to compress the interior walls implosively toward the liner axis in a manner that produces synchrotron radiation as the beam propagates through the lumen of the imploding liner.
2. The method of claim 1 , wherein: the charged particle beam is an electron beam; reflection of the electron beam from the interior walls produces a beam of synchrotron radiation that propagates through the liner.
3. The method of claim 2 , wherein electrons of the electron beam are reflected from the interior walls by inducing image currents in the interior walls.
4. The method of claim 1 , wherein the implosive force is applied by application of electric pulse power to the liner.
5. The method of claim 1 , wherein the implosive force achieves a Z-pinch of the liner as the implosive force compresses the interior walls of the liner.
6. The method of claim 1 , wherein the implosive force is applied by irradiating the liner with electromagnetic radiation.
7. The method of claim 1 , wherein the implosive force is applied by applying an ablative implosion force to the liner.
8. The method of claim 1 , wherein the implosive force is applied by application of a hypervelocity impact force to the liner.
9. The method of claim 1 , wherein the beam is introduced into the lumen of the liner such that at least some of the reflections of the beam from the interior walls are at glancing angles of incidence.
10. The method of claim 1 , wherein the implosive force is applied in a manner by which one portion of the liner implodes at a greater velocity than another portion of the liner.
11. The method of claim 1 , wherein: the liner is wound in an axially compact manner; and the implosive force is applied by placing the axially compact liner in a hohlraum and applying an indirectly induced implosive force to the liner.
12. The method of claim 1 , further comprising: adding to the lumen a gas capable, when pumped, of exhibiting laser action; and pumping the gas in the lumen with the synchrotron radiation to produce second-stage light by optical amplification.
13. The method of claim 1 , further comprising adding to the lumen a gas exhibiting a non-linear dependence of refractive index (n) on laser-light intensity, resulting in n□1, so as to increase a ratio of implosion velocity over the velocity of light c/n by n.
14. The method of claim 1 , wherein the interior reflective walls are coated with a resonant fluorescent layer having a refractive index n>1.
15. The method of claim 1 , wherein the implosive force is applied to the liner in a manner that provides the lumen with convergence or divergence that progresses from the first end to the second end as the liner is being implosively compressed.
16. The method of claim 1 , wherein the beam, while being introduced into the lumen, is provided with a large azimuthal velocity component.
17. The method of claim 1 , wherein the implosive force is applied to the liner uniformly radially inward toward the axis.
18. The method of claim 1 , wherein the implosive force is applied to the liner in a manner in which a greater force is applied in one direction toward the axis than in another direction toward the axis.
19. The method of claim 1 , further comprising: placing multiple shells around the liner; and before or while applying the implosive force, placing the liner and shells in an axial magnetic field to form a cushion between the shells during implosion.
20. An apparatus for producing synchrotron radiation, comprising: a liner comprising a first end, a second end, and walls that include interior surfaces defining a lumen extending along an axis, the interior surfaces being reflective to a charged particle beam; means for introducing a charged particle beam into the first end of the liner such that the beam propagates through the lumen from the first end to the second end as the beam reflects multiple times from the interior surfaces; and implosion means for applying an implosive force to the liner as the beam propagates through the lumen, the implosive force being sufficient to compress the walls toward the axis in a manner that produces synchrotron radiation as the beam propagates through the lumen.
21. The apparatus of claim 20 , wherein the lumen has a cylindrical transverse profile before compression.
22. The apparatus of claim 20 , wherein the lumen has a non-circular transverse section before compression.
23. The apparatus of claim 22 , wherein the transverse section is lenticular.
24. The apparatus of claim 20 , wherein the lumen is configured to exhibit, during compression of the liner, divergence or convergence from the first end to the second end.
25. The apparatus of claim 20 , wherein the liner comprises at least one surrounding shell that is compressed, along with the liner, by the implosion force applied by the implosion means.
26. The apparatus of claim 20 , wherein the liner is axially compacted.
27. The apparatus of claim 26 , wherein the liner has a helical configuration.
28. The apparatus of claim 27 , wherein the implosion means comprises: a hohlraum, into which the liner is placed for application of the implosive force; and means for applying a burst of radiation to the liner in the hohlraum.
29. The apparatus of claim 20 , wherein the lumen is configured to exploit a shape-change effect during implosion of the liner.
30. The apparatus of claim 20 , wherein the liner comprises at least one metal.
31. The apparatus of claim 20 , wherein the liner lumen contains a gas having a non-linear dependence of refractive index (n) on the laser-light intensity, resulting in n□1.
32. The apparatus of claim 20 , wherein the interior surfaces of the liner are coated with a reflection-enhancing substance.
33. The apparatus of claim 32 , wherein the reflection-enhancing substance is a resonant fluorescent material having a refractive index n>1.
34. The apparatus of claim 20 , wherein the walls of the liner, including the interior surfaces, are screw-shaped.
35. The apparatus of claim 20 , further comprising a hohlraum containing the liner and into which the implosion means applies the implosive force to the liner.
36. The apparatus of claim 20 , wherein the implosion means applies a Z-pinch implosive force to the liner.
37. The apparatus of claim 20 , wherein the implosion means comprises means for ablatively imploding the liner.
38. The apparatus of claim 37 , wherein the means for ablatively imploding the liner comprises a hohlraum and means for producing in the hohlraum a burst of black-body radiation directed to the liner.
39. The apparatus of claim 20 , wherein the implosion means comprises: means for producing the implosive force; and means for coupling the implosive force to the liner.
40. The apparatus of claim 39 , wherein the means for coupling is configured to achieve a direct-drive coupling of the implosive force to the liner.
41. The apparatus of claim 40 , wherein the direct-drive coupling produces a Z-pinch of the liner.
42. The apparatus of claim 39 , wherein the means for coupling is configured to achieve an indirect-drive coupling of the implosive force to the liner.
43. The apparatus of claim 42 , wherein the indirect-drive coupling produces ablative implosion of the liner.
44. A method for igniting a fusion target, comprising: providing a liner having a first end, a second end, a liner axis, and a lumen extending along the liner axis and being bound by interior reflective walls of the liner; introducing a charged particle beam into the first end of the liner such that the beam propagates through the lumen from the first end to the second end as the beam reflects multiple times from the interior walls of the liner; applying an implosive force to the liner as the beam propagates through the lumen of the liner, the implosive force serving to compress the interior walls implosively toward the liner axis in a manner that produces synchrotron radiation as the beam propagates through the lumen of the imploding liner, thereby producing a synchrotron radiation beam; and directing the synchrotron radiation beam to the fusion target.
45. The method of claim 44 , wherein the target is an inertial-confinement fusion target.
46. An apparatus for igniting a fusion target, comprising: a liner comprising a first end, a second end, and walls that include interior surfaces defining a lumen extending along an axis, the interior surfaces being reflective to an energy beam; means for introducing a charged particle beam into the first end of the liner such that the beam propagates through the lumen from the first end to the second end as the beam reflects multiple times from the interior surfaces; implosion means for applying an implosive force to the liner as the beam propagates through the lumen, the implosive force being sufficient to compress the walls toward the axis in a manner that produces synchrotron radiation as the beam propagates through the lumen, thereby producing a synchrotron radiation beam; and means for directing the synchrotron radiation beam to a fusion target.
47. The apparatus of claim 46 , wherein the fusion target is an inertial-confinement fusion target.
48. The apparatus of claim 46 , further comprising a hohlraum, wherein both the liner and the fusion target are imploded in the hohlraum.
49. A method for producing synchrotron radiation, comprising: injecting a charged particle beam into a liner; imploding the liner as the beam propagates through the liner; and allowing the beam, as the beam propagates through the imploding liner, to undergo multiple reflections inside the liner, the reflections serving to produce synchrotron radiation.
