1 SPP FIELDS MEP Main Electronics Package Peer Review Bill Donakowski UCB/SSL 18 NOV 2014 MAVEN PFDPU Flight Unit SPP MEP Baseline.

Slides:



Advertisements
Similar presentations
Fischer Manufacturing is an electrical fabrication company based in New Brighton, MN. We specialize in building to engineering specified requirements.
Advertisements

Mech Systems Proposed EMI Modifications Marc Campell 9/2/03.
J. H. ChrzanowskiNSTX TF Flag Joint Design Review1 NSTX TF Flag Joint Design Review Fabrication and Assembly April 10, 2003 By: James H. Chrzanowski.
A. Bross Imperial College – 9/04 Status of VLPC Cryo-Cooler Cryostat Design Russ Rucinski (Alan Bross) Fermilab.
GLAST LAT Project I&T Meeting – Jan 29,2004 E. Gawehn 1 GLAST Large Area Telescope: MGSE Status Report Eric Gawehn SU-SLAC I&T MGSE Engineer
Status of VLPC Cryo-Cooler Cryostat Design Russ Rucinski (Alan Bross) Fermilab.
Knowledge to Shape Your Future Electric / Gas / Water Information collection, analysis and application MekElekItroniks Design Review Battery Charger Project.
GLAST LAT ProjectDecember 2, 2003 R. Johnson Engineering Meeting 1 GLAST Large Area Telescope: Tracker Subsystem WBS Tracker EM Vibration Test Status.
B. Donakowski UCB/SSLFIELDS iCDR – MEP Mechanical 1 SPP FIELDS MEP Main Electronics Package Mechanical Packaging Bill Donakowski
Solar Probe Plus FIELDS Monthly Management Telecom Sep 17, 2012.
MEP configuration pros/cons
Observatory - Overview July 13 & 14, 2010MMS I&T Pre-CDR Peer Review 1 Single Observatory Stowed.
SPP FIELDS V5 Antenna Mechanical Peer Review David Glaser, Paul Turin, Jeremy McCauley, John Bonnell, Dennis Seitz SSL UCB 7/17/13.
SPP FIELDS V5 Antenna Mechanical Peer Review Draft 2 David Glaser, Paul Turin, Jeremy McCauley, John Bonnell, Dennis Seitz SSL UCB 7/17/13.
3-4 Sept. 2008EFW INST+SOC PDR141 Electric Field and Waves (EFW) Spin Plane Boom (SPB) Gregory Dalton Space Sciences Laboratory University of California.
Selda HeavnerFIELDS iPDR – Antenna Electronics Board Solar Probe Plus FIELDS Instrument PDR Antenna Electronics Board Selda S. Heavner U.C. Berkeley
C osmic R Ay T elescope for the E ffects of R adiation Telescope Mechanical Design Albert Lin The Aerospace Corporation Mechanical Engineer (310)
26 April 2013 Immanuel Gfall (HEPHY Vienna) Belle II SVD Overview.
GLAST LAT ProjectDOE/NASA Mechanical Systems Peer Review, March 27, 2003 Section Mechanical Systems X-LAT Assy1 GLAST Large Area Telescope: Mechanical.
GLAST LAT ProjectDOE/NASA Mechanical Systems Peer Review, March 27, 2003 Document: LAT-PR-0XXXX Section 5.1 Grid Box Design 1 GLAST Large Area Telescope:
D. GordonFIELDS iCDR – DCB Solar Probe Plus FIELDS Instrument CDR DCB Dorothy Gordon Space Sciences Lab, UC Berkeley 1.
1 PFP Peer iCDR /9-11 Particles and Fields Package (PFP) Peer Instrument Critical Design Review SWIA Mechanical Gregory Dalton Gregory Johnson UCB-SSL.
Design Progress Allen Ellis 18-September
1 Structure (STR) Subsystem Overview Jonah White – STR Co-Lead.
Marc Anduze – 09/09/2008 Report on EUDET Mechanics - Global Design and composite structures: Marc Anduze - Integration Slab and thermal measurements: Aboud.
10c-1 MAVEN IPER May 22-23, 2012 Particles and Fields Package Pre-Environmental Review May , c - Board Analysis Update Christopher Smith Mars.
1 SPP FIELDS MEP Main Electronics Package Preliminary Design Review Bill Donakowski UCB/SSL 13/14 NOVEMBER 2013 MAVEN PFDPU Flight.
Cosmic Test Rig  Mechanical structure to hold 4 PCBs  Minimise inter-sensor spacing  Rigid during ~weeks test run  Mounting for scintillators above/below.
Sept. 2008EFW INST+SOC PDR IDPU Chassis Mechanical Design and Development Bill Donakowski Mechanical Engineer UCB/SSL
Mechatronics Task Force, 26-nov-02 Olivier Teller, CERN EP-CMA1 Cooling Mechatronics Schedule.
Main Electronics Package
For Official Use Only; Information herein NOT Approved for Export; Contains Proprietary Protected Information; NOT for Public Release 1 WIPER PDR Stanford,
SPP FIELDS DFB Quarterly June 16, 2015 Solar Probe Plus FIELDS Instrument Quarterly Q Digital Fields Board (DFB) 1.
AEP Mechanical and Power System H. Heetderks. CDR July, 2001NCKU UCB Tohoku AEP Mechanical and Power System H. Heetderks 2 AEP Mechanical Design System.
1 PFDPU Mechanical Packaging PEER REVIEW MAVEN PFDPU Particle and Fields Data Processing Unit Mechanical Packaging and Design Overview May 09, 2011 Bill.
RICH2 support and cooling mechanics status update Massimo Benettoni July 30,
GLAST LAT ProjectCAL Peer Design Review, Mar 17-18, 2003 P. Dizon Naval Research Lab Washington DC GLAST Large Area Telescope Calorimeter Subsystem Gamma-ray.
APAR LRU Brick Mechanical Design EOL APAR Team (Jim Ranson – EOL Design and Fabrication Services presenting) EOL APAR Advisory Panel March 2015.
109-IDPU-Chassis-Donakowski 1 30 Sep – 01 Oct 2009DRAFT RBSP EFW ICDR 109-IDPU-Chassis-Donakowski IDPU Chassis Mechanical Design and Development Bill Donakowski.
STEREO IMPACT SEP Critical Design Review 2002-Nov-21/22 TvR1 SEP Mechanical Design Sandy Shuman, GSFC ) Tycho.
RBSP Radiation Belt Storm Probes RBSP Radiation Belt Storm Probes RBSP/EFW CDR /30-10/1 535 IDPU Chassis Bill Donakowski Mechanical Engineer UCB/SSL.
17-1 MAVEN IPER May 22-23, 2012 Particles and Fields Package Pre-Environmental Review May , PFDPU D. Gordon / W. Donakowski PFDPU Team.
GLAST LAT ProjectDOE/NASA Mechanical Systems Peer Review, March 27, 2003 Document: LAT-PR-0XXXX Section 5.3 Fab & Assy Plans 1 GLAST Large Area Telescope:
RBSP Radiation Belt Storm Probes RBSP Radiation Belt Storm Probes RBSP/EFW CDR /30-10/1 Thermal Design Christopher Smith RBSP Thermal Engineer Space.
1 GLAST LAT ProjectMechanical Systems Mechanical Systems November 2003 GSFC Status Marc Campell, Subsystem Manager.
SPP FIELDS DFB Quarterly November 21, 2014 Solar Probe Plus FIELDS Instrument Quarterly Digital Fields Board (DFB) 1.
20-1 MAVEN iPSR Oct 30-31, 2012 Particles and Fields Package Pre-Ship Review October 30-31, PFDPU D. Gordon, W. Donakowski & PFDPU Team Mars.
Cloudland Instruments Hawkeye Mechanical Design Snapshot Compiled April 8th, 2016.
Status of EPS Battery configuration finalized Solar panel layout –finalized Solar panel Substrate is ready for bonding EM – fabricated and Completed the.
USCMS Pixel PMG, Nov 29, Mechanics Status Disks, ½ Service Cylinders Installation USCMS FPIX FNAL PMG Joe Howell Bruno Gobbi Nov. 29, 2006.
24 September 2012 Immanuel Gfall (HEPHY Vienna) SVD Status of Mechanics PXD-SVD Meeting Göttingen.
BonnellFIELDS iCDR – AEB Solar Probe Plus FIELDS Instrument CDR Antenna Electronics Board AEB J. Bonnell, D. Seitz UC Berkeley, SSL
Solar Probe Plus FIELDS V1234 Mechanical Pre-Ship Review May 26, 2017
Rose Navarro HMI Lead Thermal Engineer
FIELDS MEP Thermal Vacuum Cycling iPER
Baby-MIND Modules & Services
Gayle K. Martin November 14, 2016
Bill Donakowski Mechanical Engineer UCB/SSL
Hawkeye Mechanical Design Snapshot
University of California, Berkeley
Design of Distribution Feedbox at LHC P7
Spacecraft Structures
Matthew Smith (617) June 27, 2006 Mechanical Design, CRaTER Assembly and Electronics Assembly Critical Design Review Matthew.
GLAST Large Area Telescope
1. Introduction and Overview
ATL-IC-ES new version available - approval starts
Structures March 13, 2004.
GLAST Large Area Telescope:
Bunker Wall Design Wall ESS
Manufacturing Processes
Presentation transcript:

1 SPP FIELDS MEP Main Electronics Package Peer Review Bill Donakowski UCB/SSL 18 NOV 2014 MAVEN PFDPU Flight Unit SPP MEP Baseline Design B. Donakowski SPP MEP EM Hardware

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 Issues 218 NOV 2014 B. Donakowski

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

MEP Project Requirements Requirements per EDTRD, Analysis/Design – Materials selection, dynamics analysis, structural analysis, venting, EMI/EMC, grounding Testing/Verification – Mass Properties, Vibration, TVAC, Bakeout, Cleanliness 418 NOV 2014 B. Donakowski

MEP Box Overview 5 Attach surface to Spacecraft Panel 18 NOV ” 6.85” 8.25” B. Donakowski

MAVEN Design Heritage 6 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

MEP Typ Box Frame Assy 7 FrameInstrument Connectors EMI Shield Mounting Surface to Spacecraft Intrabox Connectors Screws and Custom Inserts at PCB perimeter Card PWA 6.2” x 9.2” Daughter Board (DCB, DFB, TDS) 18 NOV 2014 B. Donakowski 2X Center Posts

Box Machined Open Frame Design 8 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. Donakowski 18 NOV 2014

Interlocking Frames Design 9 Individual Frames bolted together with 6X skewers Detail showing Frame Interlocking Features Each Box can be Pulled From Stack B. Donakowski 18 NOV 2014

Daughter Board Details DB Module to be designed/built by SSL Large Chip (RJEX4000 CCGA) at Center Used on DCB, TDS, DFB 10 Custom threaded tool thru threaded inserts applies gentle force at corners to remove DB from MB 4X Custom Tools EM Hardware built and working well B. Donakowski 18 NOV 2014

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) 11 S/C PCB screwed to EMI Shield (2x) B. Donakowski 18 NOV 2014

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 12 B. Donakowski 18 NOV 2014

MEP FEM Dynamic Analysis 13 B. Donakowski 18 NOV 2014 ComponentRequirementAnalysisTest ResultsRemarks Box StructureFn > 100 Hz600 Hz450 HzMEP EM Hardware Mother Board (DCB) Adequate (2X) Separation from Structure 195 Hz210 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 HzTBDSine Survey Test DEC 2014 Modal Analysis, Axis Perpendicular to PCBs

FEM Analysis 14 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. Donakowski 18 NOV 2014

Mass Properties Current Estimate: Kg Contingency (20%): Kg Current Best Estimate: Kg – (Intrabox Cables included, S/C cables not included) 15 B. Donakowski 18 NOV 2014

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 B. Donakowski 18 NOV 2014

MEP Status and Schedule S/C Interface – SSL has approved APL’s baseline spacecraft panel inserts design 17 B. Donakowski 18 NOV 2014

Backup Slides 18 B. Donakowski 18 NOV 2014

Electronics Board Layout Control Drawing 19 Drawing Maintained by SSL Distributed to Electronics Designers Main Document for Design Consistency between EE and ME aspects B. Donakowski 18 NOV 2014

Connectors Fastening 20 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. Donakowski 18 NOV 2014

PCB Attach Method 21 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. Donakowski 18 NOV 2014