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MEP Functional Requirements Provide Packaging for 9 different Board Assemblies in common box – LNPS1, LNPS2, MAGo, MAGi, RFS/DCB, DFB, AEB (2x), TDS Modular box arrangement allows individual boxes to be built up independently and taken apart a/r Design/Coordinate/Fab Box Frames with responsible groups – UCB/MN/LASP/GSFC.060” thick Aluminum walls for Radiation Shielding One plane mounting interface to Spacecraft Adequate Structure Integrity (Strength, Dynamics) Optimal thermal path to Spacecraft Electrical Ground to S/C 318 NOV 2014 B. Donakowski
Citation preview
1
SPP FIELDS MEPMain Electronics Package
Peer Review
Bill [email protected]
UCB/SSL18 NOV 2014 MAVEN PFDPU
Flight UnitSPP MEP
Baseline Design
B. Donakowski
SPP MEPEM Hardware
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MEP PDR Overview
• Requirements• Design Heritage• Design Overview• Interlocking Frame Design Details• Daughter Board Details• Thermal Design• FEM Design Analysis• Mass Properties• Vibration Testing • Ongoing Issues18 NOV 2014 B. Donakowski
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MEP Functional Requirements
• Provide Packaging for 9 different Board Assemblies in common box– LNPS1, LNPS2, MAGo, MAGi, RFS/DCB, DFB, AEB (2x), TDS
• Modular box arrangement allows individual boxes to be built up independently and taken apart a/r
• Design/Coordinate/Fab Box Frames with responsible groups– UCB/MN/LASP/GSFC
• .060” thick Aluminum walls for Radiation Shielding • One plane mounting interface to Spacecraft• Adequate Structure Integrity (Strength, Dynamics)• Optimal thermal path to Spacecraft• Electrical Ground to S/C18 NOV 2014 B. Donakowski
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MEP Project Requirements
• Requirements per EDTRD, 7434-9039• Analysis/Design
– Materials selection, dynamics analysis, structural analysis, venting, EMI/EMC, grounding
• Testing/Verification– Mass Properties, Vibration, TVAC, Bakeout,
Cleanliness
18 NOV 2014 B. Donakowski
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MEP Box Overview
Attach surface to Spacecraft Panel
18 NOV 2014
10”6.85”
8.25”
B. Donakowski
6
MAVEN Design Heritage
6x Skewers
Top EMI Shield over Card-Card Harnesses
S/C Bracket
Box Vents
Connectors on 3 sides of box
MAVEN Electronics Box• 11 Separate Cards sharing common Frame
details• Bolted to S/C Bracket on one Box face
Box Size: 8.1” Wide x 6.2” Tall x 9.3” Long
SPP FIELDS Electronics Box• 9 Separate Cards sharing common Frame
details• Bolted to S/C on one Box face
10x Attach feet to S/C(every other Frame)#8 Fasteners
(no shear panels)
Box Size: 9.4” wide x 6.5” Tall x 8.0” long
2x Skewers
Connectors on 3 sides of box
B. Donakowski
2 Shear Panels
18 NOV 2014
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MEP Typ Box Frame Assy
Frame Instrument Connectors
EMI Shield
Mounting Surface to Spacecraft
Intrabox Connectors
Screws and Custom Inserts at PCB perimeter
Card PWA6.2” x 9.2”
Daughter Board (DCB, DFB, TDS)
18 NOV 2014 B. Donakowski
2X Center Posts
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Box Machined Open Frame Design
Box Frame walls .060”
Multiple PCB attach screws to Frame to increase PWB stiffness and provide good thermal conduction path
Machined 6061 T6 Al Alloy Machined Frame.85” Pitch (Frame to Frame)
Feet for attachment to S/C
LNPS Boxes are 5-sided
6X Skewers (#8 Threaded Rod)(OPEN)
B. Donakowski18 NOV 2014
9
Interlocking Frames Design
Individual Frames bolted together with 6X skewers
Detail showing Frame Interlocking
Features
Each Box can be Pulled From Stack
B. Donakowski18 NOV 2014
10
Daughter Board Details• DB Module to be designed/built by SSL• Large Chip (RJEX4000 CCGA) at Center• Used on DCB, TDS, DFB
Custom threaded tool thru threaded inserts applies gentle force at corners to remove DB from MB
4X Custom Tools
EM Hardware built and working wellB. Donakowski18 NOV 2014
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Thermal Design
• S/C environment is hot—testing at 75 C• Boards screwed to Frames at perimeter• 2X Screws at PCB center to EMI shield w/ integral posts• Attachment frame wet mounted to S/C (TBC)• All Exterior Walls painted with Black Paint (Aeroglaze Z307)• Black Anodize Interior Walls• Alodine 600 Treatment at Box interfaces (to PCB, SC, other Frames)
S/C
S/C
S/CPCB screwed to EMI Shield (2x)
B. Donakowski18 NOV 2014
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PWB Thermal Design• Consider entire heat path• Component To Board
– All components dissipating more than 50 mW should be looked at by thermal engineer
• Thermal / Ground / Power Planes– Board dissipated power needs to travel to the frame via
conduction in thermal (or ground) planes, then to the frame• Board Mounting to Box
– Need a good path from thermal planes to standoffs / box lip /
– 2 Oz Copper Layers
B. Donakowski18 NOV 2014
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MEP FEM Dynamic Analysis
B. Donakowski18 NOV 2014
Component Requirement Analysis Test Results RemarksBox Structure Fn > 100 Hz 600 Hz 450 Hz MEP EM HardwareMother Board (DCB)
Adequate (2X) Separation from Structure
195 Hz 210 Hz (MAVEN)
235 Hz (DFB)
• MAVEN Board similar in design
• DFB test run by LASP on EM (NOV 2014)
Daughter Board (DCB)
Adequate (2X) Separation from MB
850 Hz TBD Sine Survey Test DEC 2014
Modal Analysis, Axis Perpendicular to PCBs
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FEM Analysis• PCB/Spacers/EMI Shield
Assy• Fixed at Perimeters (to
Frame)• Fn=195 Hz
• Entire MEP Box Assy• (PCBs/Frames)• Fixed at Attach Feet (to S/C)• Fn > 600 Hz
B. Donakowski18 NOV 2014
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Mass Properties• Current Estimate: 7.081 Kg• Contingency (20%): 1.416 Kg
• Current Best Estimate: 8.497 Kg
– (Intrabox Cables included, S/C cables not included)
B. Donakowski18 NOV 2014
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MEP Status and Schedule• EM Hardware
– All Mechanical hardware fabrication complete– Hardware In-house and part of box build-up
• Required Design Changes for FLIGHT (not incorporated in EM design)
– Change in connectors due to survival heater scheme change • All Drawing changes complete
– Increase in TDS Box width due to component height increases below board• All Drawing Changes complete
– LASP request for taller components below DFB Board• Design under evaluation/ Appears to be simple change
• Final FEM Analysis– December 2014
• EM Testing– Fit checks of Frames/Weighing PWA– Some limited Thermal Vac Testing, December 2014– If hardware allows, vibration (sine sweep) test, January 2014
B. Donakowski18 NOV 2014
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MEP Status and Schedule• S/C Interface
– SSL has approved APL’s baseline spacecraft panel inserts design
B. Donakowski18 NOV 2014
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Backup Slides
B. Donakowski18 NOV 2014
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Electronics Board Layout Control Drawing
Drawing Maintained by SSLDistributed to Electronics DesignersMain Document for Design Consistency between EE and ME aspects
B. Donakowski18 NOV 2014
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Connectors Fastening
UCB Custom Connector Nutplate
• Easier than nuts to assemble • no need to get wrench to hold nuts
during jackpost torquing• Standoffs can be removed one-by-
one
D-Connector
OTS Jackposts
Spiralock tapped holes
Desirement: Allow Jackposts to be Removed from outside of Box without opening box
Material: 6061 T6 Aluminum
B. Donakowski18 NOV 2014
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PCB Attach Method
• Custom UCB designed insert• Stainless Steel, Silver Plated• Spiralock Threads provide
Locking Device• Insert soldered to PCB Traces• UCB will provide to outside
groups
B. Donakowski18 NOV 2014