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Document # |
Date Effective |
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LAT-TD-07585-01 |
7 November 2005 |
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Prepared by(s) |
Supersedes |
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Gunther Haller |
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GLAST LAT Technical Note |
Jeffrey S. Ludvik |
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Subsystem/Office |
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Electronics & DAQ Subsystem |
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Document Title |
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SIU Crate Assembly |
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Gamma-ray Large Area Space Telescope (GLAST)
Large Area Telescope (LAT)
Electronics & DAQ Subsystem
Acceptance Test Data Package
SIU Crate Assembly #3
GLAT2527
DOCUMENT APPROVAL
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Prepared by: |
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Jeffrey Ludvik |
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Approved by: |
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Gunther Haller |
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Dave Nelson |
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Leonid Sapozhnikov |
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Joe Cullinan |
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LAT Acceptance
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Dick Horn |
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Pat Hascall |
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Ken Fouts |
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Joe Cullinan |
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Other |
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CHANGE HISTORY LOG
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Revision |
Effective Date |
Description of Changes |
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01 |
7 November 2005 |
Initial Draft |
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1 PURPOSE
The purpose of this Technical Note is to document the contents of the Acceptance Test Data Package (ATDP) for the DAQ Electronics (DAQ) subsystem. The contents of this document have been coordinated between LAT Integration, Test, and Calibration (IT&C), LAT Systems Engineering (SE), and LAT Quality Assurance (QA).
2 Identification
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Item Description:
LAT SIU Crate Assembly #3 Module – GLAT2527 - LAT-DS-01862-53 |
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Identification |
Part/Drawing Number |
Serial Number |
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CPS |
LAT-DS-01669 |
GLAT2238 |
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LCB |
LAT-DS-01679 |
GLAT2226 |
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SIB |
LAT-DS-01674 |
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Backplane |
LAT-DS-02964 |
GLAT2415 |
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Harness |
LAT-DS-02964 |
GLAT2429 |
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RAD750 |
NA |
GLAT2517 #15 |
3 Certificates of Compliance
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MECHANICAL SUMMARY DATA |
Mechanical Lead: Dave Nelson |
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ITEM: |
REMARKS: |
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Structural Analysis reviewed and acceptable |
Report Available |
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Structural Tests reviewed and acceptable |
Report Available |
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Open Items from tests performed or from meetings with SLAC |
None |
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Mass (Measured) The maximum SIU assembly mass allocation is 7.5 kg/16.5 lbs. LAT-PS-05598-02, Sec. 4.1.1 |
6.45 kg, Complies |
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As Run Mass Measurement Procedure |
LAT-PS-07372-01 |
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Mass (Mass Survey) |
Not Performed |
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Mass / Center of Mass Report - Analysis |
Not Performed - Qual only |
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Dimensions |
(to be inserted) 11/18/05 |
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Interface flatness and surface finish |
(to be inserted) 11/18/05 |
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Dimension Inspection Report |
Done at box level assy listed below |
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SIU
base dimensional inspection |
AIDS
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SIU lid dimensional inspection |
AIDS
#xxx |
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Final visual inspection prior to shipping to SLAC. |
Archived at SLAC in Bldg. 33 Flight Store |
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ELECTRICAL SUMMARY DATA
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Electrical Lead: Gunther Haller |
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DESCRIPTION: |
REMARKS: |
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Power consumption (28V, 25 deg C, nominal activity, 20 MHz clock) SIU Crate Unit. |
28 V * 0.66 A = 18.48 W |
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Part List reviewed and acceptable |
Archived at SLAC, Bldg. 33 Flight Store |
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Electrical Test reviewed and acceptable |
Archived at SLAC, Bldg. 33 Flight Store |
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Open Items from previous reviews / meetings / tests |
None |
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Power consumption Report |
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| Start-up Voltage Profile | NA | |
| Start-up Current Profile | NA | |
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PRODUCT ASSURANCE DATA
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Quality Lead Engineer: Joe Cullinan |
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DESCRIPTION: |
REMARKS: |
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Non-conformance report summary |
SIU_CRATE_GLAT2527_SLAC_Summary_Report Archived at SLAC, Bldg. 33 Flight Store |
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Open NCRs |
See NCR List Below |
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Traceability of unit pedigree |
Available in SOW, WO from Aeroflex. Archived at SLAC, Bldg. 33 Flight Store |
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Photographic Record |
Online and Archived at SLAC, Bldg. 33 Flight Store |
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Inspection records |
Archived at SLAC, Bldg. 33 Flight Store |
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Storage, handling, shock records |
Archived at SLAC, Bldg. 33 Flight Store |
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WO list |
WO#1693, WO#1694 |
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All operations, inspections, and tests have been completed per procedures as indicated on WO (signed and dated) |
WOs Archived at SLAC, Bldg. 33 Flight Store |
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All operations performed to released and controlled procedures |
Documents available online in LAT-docs database |
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Chronological history is up-to-date and reflects each major action that has transpired |
WOs Archived at SLAC, Bldg. 33 Flight Store |
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Identity of manufacturers, part numbers, and serial number are correct |
Archived at SLAC, Bldg. 33 Flight Store |
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All Non Conformance Reports, Material Review Board Reports, and failure reports are closed and accepted as per internal procedures |
NCRs Archived at SLAC, Bldg. 33 Flight Store |
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Materials and processes used in the hardware are approved and acceptable |
Archived at SLAC, Bldg. 33 Flight Store |
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Test logbooks, including operating time and cycle records, are complete and meet specified requirements |
Log books and WOs Archived at SLAC, Bldg. 33 Flight Store |
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All test data including deviations have been approved and stamped by the test engineer and Quality Assurance |
WOs and reports Archived at SLAC, Bldg. 33 Flight Store |
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Inspection performed for physical damage (such as scratches or dents) and for cleanliness |
No appreciable damage to interfaces. Unit cleaned prior to shipment. |
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Connectors and pins examined for evidence of damage or contamination |
No evidence of damage or contamination. Refer to Mate/Demate Log |
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All environmental test data and results meet specifications |
No exceptions |
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ENVIRONMENTAL TEST SUMMARY DATA |
System Engineer: Dave Tarkington |
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Vibration Test |
LAT-TD-03648-01, as run available on file |
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Summary Report |
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Requirement |
LAT-SS-00778 Criteria |
Pass / Fail |
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Random Vibration |
Table 27, Section 9.1 |
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Pass |
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ENVIRONMENTAL TEST SUMMARY DATA |
System Engineer: Leonid Sapozhnikov |
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Thermal Cycle |
WO#1694, GLAT2527, as run available on file |
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Summary Report |
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Requirement |
WO#1694, Step 70 |
Pass / Fail |
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Follow Profile |
WO1694, Step 70 |
5 cycles, –40°C to +55 | ||||