dat input file for DRAGON5
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* typge, nbfo, node, elem, macr, nreg,    z, mac2
      9,    0,     5,    10,     1,    5,     0,     1
* index  kindex
      0       0  1
*     eps    eps0
  1.000000E-05   1.000000E-05
*   flux region number per geometry region (mesh)
   1,   2,   3,   4,   5
*   names of macros
mac
*   macro order number per flux region
5*1
   elements
* ELEM  1  line segment
 1, 0, 5
*
  -0.785219, 0.000000, 0.392610, -0.680020
* ELEM  2  line segment
 1, 0, 5
*
  -0.392610, 0.680020, -0.392610, -0.680020
* ELEM  3  line segment
 1, 0, 5
*
  -0.392610, -0.680020, 0.785219, -0.000000
* ELEM  4  circle
 2, 1, 2
*
  0.000000, 0.000000, 0.100000, 0.0
* ELEM  5  circle
 2, 2, 3
*
  0.000000, 0.000000, 0.450000, 0.0
* ELEM  6  circle
 2, 3, 4
*
  0.000000, 0.000000, 0.465000, 0.0
* ELEM  7  circle
 2, 4, 5
*
  0.000000, 0.000000, 0.525000, 0.0
* ELEM  8  line segment
 1, 0, 5
*
  0.392610, 0.680020, -0.785219, 0.000000
* ELEM  9  line segment
 1, 0, 5
*
  0.392610, -0.680020, 0.392610, 0.680020
* ELEM  10  line segment
 1, 0, 5
*
  0.785219, 0.000000, -0.392610, 0.680020
* boundaries conditions: defaul nbbcda allsur
  0, 6, 0
* albedo
  1.0
* type  number of elements
  2, 1
*   elements
1
* tx, ty, angle
  1.177829 0.680020 0.000000
* type  number of elements
  2, 1
*   elements
2
* tx, ty, angle
  1.177829 -0.680020 0.000000
* type  number of elements
  2, 1
*   elements
3
* tx, ty, angle
  0.000000 1.360040 0.000000
* type  number of elements
  2, 1
*   elements
8
* tx, ty, angle
  0.000000 -1.360040 0.000000
* type  number of elements
  2, 1
*   elements
9
* tx, ty, angle
  -1.177829 0.680020 0.000000
* type  number of elements
  2, 1
*   elements
10
* tx, ty, angle
  -1.177829 -0.680020 0.000000
#  6 - HOLLOW
#  3 - MOX
#  6 - GAP
#  7 - CLADDING
#  8 - COOLANT
* medium number per region
  6
  3
  6
  7
  8
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   this is the last line generated by conversion