Abaqus-Distribution-inp.File

[bschmu]

Hallo,
ich habe versucht eine *Distribution für Materialien (*Elastc, Type= Lamina)zu erstellen. Leider kommt hier immer die Fehlermeldung:

The job "Job-1" has been created.
The job input file "Job-1.inp" has been submitted for analysis.
Error in job Job-1: THERE ARE TOO FEW DATA CARDS TO DEFINE THIS MATERIAL OPTION
Job Job-1: Analysis Input File Processor aborted due to errors.
Error in job Job-1: Analysis Input File Processor exited with an error.
Job Job-1 aborted due to errors.

Das ist mein input-File:
*Heading
** Job name: Shell_Edge_Load Model name: Model-1
** Generated by: Abaqus/CAE 6.11-2
*Preprint, echo=NO, model=NO, history=NO, contact=NO
**
** PARTS
**
*Part, name=Part-1
*Node
1, 20., 20., 0.
2, 0., 20., 0.
3, -20., 20., 0.
4, 20., 0., 0.
5, 0., 0., 0.
6, -20., 0., 0.
7, 20., -20., 0.
8, 0., -20., 0.
9, -20., -20., 0.
*Element, type=S4R
1, 1, 2, 5, 4
2, 2, 3, 6, 5
3, 4, 5, 8, 7
4, 5, 6, 9, 8

*Distribution, name=Angle-Ori-1-DiscOrient_0, location=ELEMENT, Table=Angle-Ori-1-DiscOrient_Table
** Description: Distribution generated from Discrete Orientation
1, 45.12
2, 45.10
3, 45.09
4, 45.05
*Distribution, name=Thickness-Ori-1-DiscOrient_0, location=ELEMENT, Table=Thickness-Ori-1-DiscOrient_Table
** Description: Distribution generated from Discrete Orientation
, 0.2
1, 0.21
2, 0.20
3, 0.19
4, 0.20
*Distribution, name=Mat-Ori-1-DiscOrient_0, location=ELEMENT, Table=Mat-Ori-1-DiscOrient_Table
** Description: Distribution generated from Discrete Orientation
, 177840, 10379, 0.272, 5327, 5327, 4909
1, 177840, 10379, 0.272, 5327, 5327, 4909
2, 177840, 10379, 0.272, 5327, 5327, 4909
3, 177840, 10379, 0.272, 5327, 5327, 4909
4, 177840, 10379, 0.272, 5327, 5327, 4909
** Region: (CompositeLayup-1-1: Generated From Layup)
*Elset, elset=CompositeLayup-1-1, generate
1, 4, 1
** Section: CompositeLayup-1-1
*Shell Section, elset=CompositeLayup-1-1, composite, layup=CompositeLayup-1
Thickness-Ori-1-DiscOrient_0, 3, CFK1, Angle-Ori-1-DiscOrient_0, Ply-1
*End Part
**
**
** ASSEMBLY
**
*Assembly, name=Assembly
**
*Instance, name=Part-1-1, part=Part-1
*End Instance
**
*Nset, nset=_PickedSet12, internal, instance=Part-1-1, generate
3, 9, 3
*Elset, elset=_PickedSet12, internal, instance=Part-1-1
2, 4
*Nset, nset=_PickedSet13, internal, instance=Part-1-1
1, 2, 3, 7, 8, 9
*Elset, elset=_PickedSet13, internal, instance=Part-1-1, generate
1, 4, 1
*Elset, elset=__PickedSurf15_E4, internal, instance=Part-1-1
1, 3
*Surface, type=ELEMENT, name=_PickedSurf15, internal
__PickedSurf15_E4, E4
*Elset, elset=__PickedSurf16_SPOS, internal, instance=Part-1-1, generate
1, 4, 1
*Surface, type=ELEMENT, name=_PickedSurf16, internal
__PickedSurf16_SPOS, SPOS
*End Assembly
*Distribution Table, name=Angle-Ori-1-DiscOrient_Table
ANGLE
*Distribution Table, name=Thickness-Ori-1-DiscOrient_Table
LENGTH
*Distribution Table, name=Mat-Ori-1-DiscOrient_Table
MODULUS, MODULUS, RATIO, MODULUS, MODULUS, MODULUS
** MATERIALS
**
*Material, name=CFK1
*ELASTIC, TYPE=LAMINA
Mat-Ori-1-DiscOrient_0
** ----------------------------------------------------------------
**
** STEP: Step-1
**
*Step, name=Step-1
*Static
1., 1., 1e-05, 1.
**
** BOUNDARY CONDITIONS
**
** Name: BC-1 Type: Displacement/Rotation
*Boundary
_PickedSet12, 2, 2
_PickedSet12, 4, 4
_PickedSet12, 6, 6
** Name: BC-2 Type: Displacement/Rotation
*Boundary
_PickedSet13, 1, 1
_PickedSet13, 3, 3
**
** LOADS
**
** Name: Load-1 Type: Shell edge load
*Dsload
_PickedSurf15, EDNOR, 1000.
**
** OUTPUT REQUESTS
**
*Restart, write, frequency=0
**
** FIELD OUTPUT: F-Output-1
**
*Output, field, variable=PRESELECT
**
** HISTORY OUTPUT: H-Output-1
**
*Output, history, variable=PRESELECT
*End Step

Jetzt meine Frage, was ich ändern muss, damit das passt
Ich wäre euch sehr dankbar, weil ich das dringend für meine Bachelor Arbeit benötige und leider nach Stunden des Rumprobierens und Manual lesen einfach nicht weiter komme.
Vielen vielen Dank für eure Mühe!!