CONSERT - Antenna
on Rosetta - S/C
Test Report
Properties
RO-OCN-TR-3002
Issue: 1
Revision: -
16.07.1999
Prepared by:
W.Boogaerts
Approval Sheet
prepared by: W.Boogaerts (signature/date)
approved by: Technical Department W.Engelhardt / J.Wedekind (signature/date)
approved by: Consert antenna Management Dr. Nielsen (signature/date)
____________________________________________________________________________ _
approved by: QA/PA W.Boogaerts (signature/ date)
Document Change Record
Iss./Rev. |
Date |
Pages affected |
Description |
1/- |
16-07-1999 |
all |
|
Distribution Record
Holder |
Issue/Revision |
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Draft |
1/- |
1a |
2 |
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Consert-Documentation MPAE |
C |
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WB |
W.Boogaerts |
A/C |
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LB |
L.Bemman |
C |
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EN |
Dr. Nielsen |
A/C |
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Prof. Hagfors |
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HP |
H.Perplies |
A/C |
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KG |
K.Gräbig |
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WE |
W.Engelhardt |
A/C |
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ESA |
G. Gianfiglio |
C |
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J-P. Goutail |
A/C |
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Legend: A - Approval |
Table of contents
1 General aspects *
1.1 Scope *
1.2 Antenna Folded on Attachment Plate *
1.3 Introduction *
1.4 Applicable Documents *
1.5 Reference Documents *
1.6 Test Equipment *
1.7 Acronyms *
2 Equipment under Test *
3 Test Conditions *
4 Test Requirements *
4.1 Visual Inspection *
Identification Labels *
4.1.2 General Appearance *
4.1.3 Thermal Finish *
4.1.4 Connectors *
4.1.5 Connector Savers *
4.1.6 Protective Covers *
4.1.7 Test Covers *
4.1.8 Harness *
4.1.9 Cleanliness *
4.1.10 Safety Devices *
4.1.11 Handling Provisions *
4.2 I/F Measurements *
4.2.1 Envelope Dimensions *
4.2.2 Support 1 *
4.2.3 Support 2 *
4.2.4 Support 3 *
4.2.5 Support 4 *
4.3 Physical Properties *
4.3.1 Mass Properties *
4.3.2 CoG / MoI *
4.3.3 Natural Frequencies *
4.4 Electrical Verifications *
4.4.1 Deployment Indicators *
4.4.2 Grounding *
4.4.3 Connector Locations ( JA4 / JA1 / JA2 / JA3 *
4.5 Safety Harness : Strings and Red Tag Items *
5 Non-Conformance (NCR) *
6 Procedure Sign Off Sheet *
7 Signatures *
8 Attachments *
List of Figures
Fig. 1 Antenna folded on Attachment plate *
Fig. 2 Antenna Overview *
Fig. 3 Grounding Schematic *
Fig. 4 Connector Location on Support - 1 *
Fig. 5 Connectors JA2 / JA3 on Pyro with Safety Caps on Support 3 *
Fig. 6 Safety Strings and Red Tag Items *
List of Tables
Table 1 Applicable Documents *
Table 2 Reference Documents *
Table 3 Test Equipment *
Table 4 Deployment Indicators *
Table 5 Grounding Values *
Table 6: Open Items *
Table 7 Signatures *
Table 8 Attachments *
This Testprocedure covers Project :
Consert-Antenna (STM) on Rosetta - S/C
Fig. 1 Antenna folded on Attachment plate
The purpose of this test is to determine the properties of the Consert-Antenna i.e. dimensions , reference point , interface pattern measurements , surface flatness of attachment plate, mass , centre of gravity , natural frequencies , electrical verification , etc..
no. |
document name |
document number |
Iss./Rev. |
AD1 |
Consert Orbiter Antenna MICD |
RO-OCN-DW-3001 |
2/E |
AD2 |
General Background on Handling of the Orbiter Antenna and on Terminology Consult |
RO-OCN-DW-3019 |
Version 1.3 |
AD3 |
|||
no. |
document name |
document number |
Iss./Rev. |
RD1 |
EIDA |
RO-EST-RS-3001 |
2/0 |
RD2 |
EIDB |
RO-EST-RS-3001 |
1/0 |
RD3 |
EIDC |
RO-EST-RS-3001 |
1/1 |
RD4 |
Space Engineering |
ECSS-E-10-03 / 5.1.16 |
Draft 01F |
RD5 |
Payload units STM build standard description |
TOS-MMS/1998/550/ln/JCS |
0 |
RD6 |
STM-test objective and built-standard definition |
RO-DSS-TN-1027 |
2 |
Nr. |
Instr. / Equipment Description |
Manufacturer |
Model/Type-Nr. |
Inv. Nr. |
Calibration Last Next |
1 |
Digital Caliper Rule |
Minimax |
K/03 20118 |
94096 |
|
2 |
Knife Edge Straight-Edge |
Hauser |
|||
3 |
Thickness Gauge |
Orion/Germany |
DIN 2275 |
||
4 |
Balance |
Sartorius |
86070100 |
||
5 |
Centre Microscope |
Hensold |
65576 |
||
6 |
X/Y/Z-Digital Table |
Heidenhain |
PT855 |
||
7 |
Multimeter |
Keithly |
90011200 |
||
8 |
Low-Resistance Measurement |
Keithly |
195 |
MPAe Max-Planck-Institut für Aeronomie
STM Structural and Thermal Model
AD Applicable Document
RD Reference Document
FM Flight Model
Hz Hertz
Q-Level Qualification Level
M Mass
mm millimeter
g Acceleration
wrt. with respect to
I/F Interface
URF Unit Reference Frame
The Structural and Thermal Model (STM) of the Consert Antenna is mass and thermal representative of the Consert Antenna (FM). The size of the Antenna is 1135 mm x 100 mm x 125 mm. The Antenna weight is 1.45 kg.
Cleanliness: 100 000
Temperature: 20 ° C
Humidity: < 50 %
|
OK |
|
|
Plasmocer Black and White Iridite ; PUI Black Paint
|
|
|
OK |
|
|
N/A for STM |
|
|
None |
|
|
None |
|
|
See Material List |
|
|
Visible Clean |
|
|
for Pyro-Connection
Supports 2 and 4
|
|
To be handled by hand with gloves in class 100000 clean room |
Step |
Specification |
Actual |
Remarks |
|||
L W H |
1135 mm 100 mm 125 mm |
|||||
|
(Holes -Nr. Clockwise from upside) |
|||||
Position URF
Tol.: ± 0,1 mm |
1 2 3 4(R) |
Xu Yu0 36 36 36 36 0 0 0
|
Xu Yu-0,14 36,13 35,98 36,01 36,12 0,16 0 0
|
|||
|
1 2 3 4 |
4,3 -0/+0,1 mm 4,3 -0/+0,1 mm 4,3 -0/+0,1 mm 4,3 -0/+0,1 mm |
4,24 4,24 4,23 4,23 |
|||
|
1 2 3 4 |
N/A |
||||
Dimensions |
1 2 3 4 |
|||||
|
1 2 3 4 |
4 0/0,1 mm 4 0/0,1 mm 4 0/0,1 mm 4 0/0,1 mm |
4,06 4,04 4,06 4,05 |
|||
Area |
1 2 3 4 |
|||||
|
None |
|||||
|
100 m |
Step |
Specification |
Actual |
Remarks |
||
|
(Holes -Nr. Clockwise from upside) |
||||
Position URF
Tol.: ± 0,1 mm |
1 2 3 4(r) |
Xu Yu 0 41 20 41 20 0 233 -33 |
Xu Yu -0,10 40,99 19,93 40,95 19,99 -0,05 0 0 |
1 – 3 refer to 4(r) 4(r) refer to 4(R) at support 1 |
|
|
1 2 3 4 |
4,3 -0/+0,1 mm 4,3 -0/+0,1 mm 4,3 -0/+0,1 mm 4,3 -0/+0,1 mm |
4,23 4,22 4,23 4,22 |
||
|
1 2 3 4 |
N/A |
|||
Dimensions |
1 2 3 4 |
||||
|
1 2 3 4 |
4 0/0,1 mm 4 0/0,1 mm 4 0/0,1 mm 4 0/0,1 mm |
4,04 4,03 4,06 4,04 |
||
Area |
1 2 3 4 |
||||
|
None |
||||
|
100 m |
Step |
Specification |
Actual |
Remarks |
||
|
(Holes-Nr. Clockwise from upside) |
||||
Position URF
Tol.: ± 0,1 mm |
1 2 3 4(r) |
Xu Yu 0 41 40 41 40 0 578 -33 |
Xu Yu-0,01 41,03 39,98 41,12 40,01 0,07 0 0 |
1 – 3 refer to 4(r) 4(r) refer to 4(R) at support 1 |
|
|
1 2 3 4 |
4,3 -0/+0,1 mm 4,3 -0/+0,1 mm 4,3 -0/+0,1 mm 4,3 -0/+0,1 mm |
4,22 4,23 4,23 4,22 |
||
|
1 2 3 4 |
N/A |
|||
Dimensions |
1 2 3 4 |
||||
|
1 2 3 4 |
4 0/0,1 mm 4 0/0,1 mm 4 0/0,1 mm 4 0/0,1 mm |
4,05 4,07 4,04 4,07 |
||
Area |
1 2 3 4 |
||||
|
None |
||||
|
100 m |
Step |
Specification |
Actual |
Remarks |
||
|
(Holes -Nr. Clockwise from upside) |
||||
Position URF
Tol.: ± 0,1 mm |
1 2 3 4(r) |
Xu Yu0 41 20 41 20 0 908 -33 |
Xu Yu0,06 40,97 19,90 40,98 20,01 0,05 0 0 |
1 – 3 refer to 4(r) 4(r) refer to 4(R) at support 1 |
|
|
1 2 3 4 |
4,3 -0/+0,1 mm 4,3 -0/+0,1 mm 4,3 -0/+0,1 mm 4,3 -0/+0,1 mm |
4,25 4,24 4,24 4,24 |
||
|
1 2 3 4 |
N/A |
|||
Dimensions |
1 2 3 4 |
||||
|
1 2 3 4 |
4 0/0,1 mm 4 0/0,1 mm 4 0/0,1 mm 4 0/0,1 mm |
4,05 4,06 4,08 4,05 |
||
Area |
1 2 3 4 |
||||
|
None |
||||
|
100 m |
Mass Properties
See RO-OCN-DW-3001 |
STM Mass Breakdown (grams) (actuel) |
FM Mass predicted |
Remarks |
1447 |
1450 ± 10 |
With Cabling |
STM Measured |
FM Predicted |
Diff. In % |
|
Total Mass M |
|||
CoG X Y Z |
|
502 mm. -22 mm. 63 mm. |
|
MoI Ixx (wrt. CoG) Iyy Izz |
1.6 x 10-3 Kgm2 1.6 x 10-1 Kgm2 1.6 x 10-1 Kgm2 |
See Vibration report RO-OCN-TR-3021
STM |
Predicted for FM |
|
1st Natural Frequency X-Axis |
320 |
|
1st Natural Frequency Y-Axis |
145 |
|
1st Natural Frequency Z-Axis |
150 |
Each Carpenter-Spring is supplied with an Resistor(R) to provide a deployment-check.
See connector Location 4.4.3
Folded Antenna |
Deployed Antenna (to be measured after Deployment-Test) |
||||
Connector JA4 |
Specification
|
Actual Value |
Specification |
Actual Value |
|
Carpenter Spring 1 |
P 7 P 2 |
R < 50 W |
0.4 |
R > 1 MW |
> 1 MW |
Carpenter Spring 2 |
P9 P4 |
R < 50 W |
0.4 |
R > 1 MW |
> 1 MW |
Description |
Specification |
Actual |
Dipoles / Mast-2 |
£ 25 mW |
|
Mast-2 / Manchet-2 |
£ 25 mW |
|
Mast-2 / Mast-1 |
£ 25 mW |
|
Mast-1 / Manchet-1 |
£ 25 mW |
|
Mast-1 / Support-1 |
£ 25 mW |
|
Support-1 / Spacecraft |
£ 10 mW |
|
Support-2 / Spacecraft |
£ 10 mW |
|
Support-3 / Spacecraft |
£ 10 mW |
|
Support-4 / Spacecraft |
£ 10 mW |
|
Ground Stud /Spacecraft |
£ 2.5 mW |
|
Surfaces / ... |
< 1 kW |
> 1 kW |
Fig. 4 Connector Location on Support - 1
JA4
JA1
Fig. 5 Connectors JA2 / JA3 on Pyro with Safety Caps on Support 3
Fig. 6 Safety Strings and Red Tag Items
Where any out of limits results is obtained during the test , the result shall be annotated clearly as being a test failure and the Non-Conformance-Reporting according to EID A
Issue 1 , Rev. 0 Sec.: 3.3.8 and Section 8.33.1 will be initiated.
A NCR Consert-Formsheet RO-OCN-MPAE-FO-007.doc is attached.
A summery of all out of limits results (NCR-Overview) should be appended to the test report.
A NCR-Overview Consert-Formsheet RO-OCN-MPAE-FO-007_ov.doc is attached.
The identified test item has been successfully tested in accordance with the foregoing procedure and all open items (e.g. NCR's) are closed except those listed below:
No. |
Doc.Nr. |
Title |
Version |
Date |
Remarks |
1 |
RO-OCN-DW-3001 |
MICD |
2/D |
Item # 6 |
|