Preliminary Design Review

Slides:



Advertisements
Similar presentations
Jan. 15, Safety Board Review (Rev D) Safety Board PCB Review (Rev D) Eric Warmbier.
Advertisements

Objective of the Lecture Describe a basic electric circuit, which may be drawn as a circuit schematic or constructed with actual components.
Instrument TrainingIDPU - 1 UCB, Dec 6, 2006 THEMIS INSTRUMENT TRAINING IDPU.
GLAST LAT ProjectPDU/GASU MRR, February 3, DAQ & FSWV1 1 GLAST Large Area Telescope: B. Estey, G. Haller SLAC xxxx LAT Quality Engineer
Solar Probe Plus FIELDS Monthly Management Telecom Sep 17, 2012.
Selda HeavnerFIELDS iPDR – Antenna Electronics Board Solar Probe Plus FIELDS Instrument PDR Antenna Electronics Board Selda S. Heavner U.C. Berkeley
Presentation of the DriveLab Board Opal-RT Real-time institute 2009.
THEMIS Instrument PDR 1 UCB, October 15-16, 2003 IDPU Mechanical / Thermal Preliminary Design Review Heath Bersch University of California - Berkeley.
TIM Phase A 1 SSL, 8/15/2007 Electric Field and Waves Instrument (EFW) Technical Interchange Meeting EFW Digital Electronics Digital Control Board (DCB)
GLAST LAT ProjectDelta PDR/Baseline Review July 29-August 1, 2002 Section 7.3 AntiCoincidnce Detector Technical Status 1 GLAST Large Area Telescope: AntiCoincidence.
THEMIS Engineering Peer Review 1 UCB, October 15-16, 2003 Electric Field Instrument (EFI) Electrical Fabrication and Test.
TRIO-CINEMA 1 UCB, 2/08/2010 Instrument Interface Board Dorothy Gordon CINEMA - EE Team Space Sciences Laboratory University of California, Berkeley.
THEMIS Instrument CDR 1 UCB, April 19-20, 2004 Boom Electronics Board (BEB) Engineering Peer Review Apr. 20, 2004 Hilary Richard.
THEMIS Instrument CDR 1 UCB, April 19-20, 2004 Boom Electronics Board (BEB) Engineering Peer Review Apr. 20, 2004 Hilary Richard.
ITAR Restricted Data THEMIS Power Subsystem CDR Peer Review 6/14/04 Probe and Probe Carrier Harness Dave Manges (301)
RBSP Radiation Belt Storm Probes RBSP Radiation Belt Storm Probes 3-4 Sept. 2008EFW INST+SOC PDR217 RBSP Electric Field and Waves Instrument (EFW) Instrument.
Sept. 2008EFW INST+SOC PDR IDPU Chassis Mechanical Design and Development Bill Donakowski Mechanical Engineer UCB/SSL
RBSP Radiation Belt Storm Probes RBSP Radiation Belt Storm Probes RBSP/EFW I-PER 21 January EFW Overview and Status Keith Goetz University of Minnesota.
THEMIS SUITE PRE-ENVIRONMENTAL REVIEW 1 UCB May 2, 2005 THEMIS Pre-Environmental Review Instrument Verification Overview Ellen Taylor University of California.
SDR 7 Jun Associated Electronics Package (AEP) Curtis Ingraham.
THEMIS INSTRUMENT CDR Peer ReviewSYSTEM- 1 UCB, April 19, 2004 TITLE: Test Flow RFA CODE: UCB-10 REQUESTED BY: Preble SPECIFIC REQUEST: We recommend that.
RBSP Radiation Belt Storm Probes RBSP Radiation Belt Storm Probes RBSP/EFW CDR /30-10/1 213 Low Voltage Power Supply & Power Controller Board Peter.
RBSP Radiation Belt Storm Probes RBSP Radiation Belt Storm Probes LVPS+PCB Peter BergRBSP/EFW CDR /30-10/1 IDPU LVPS AND PCB Critical Design Review.
FGM peer PDR I/F - 1 Braunschweig, October 8-9, 2003 Digital Interface (I/F) Aris Valavanoglou Institut für Weltraumforschung (IWF) Austrian Academy of.
THEMIS Instrument PDRGSE- 1 UCB, October 15-16, 2003 IDPU Ground Support Equipment Preliminary Design Review F. Harvey University of California - Berkeley.
NameFIELDS iPDR – Subject Solar Probe Plus FIELDS Instrument PDR Antenna Electronics Box Selda S. Heavner U.C. Berkeley 1.
THEMIS MISSION PDRINSTRUMENT OVERVIEW- 1 UCB, November, 2003 THEMIS INSTRUMENT PAYLOAD SYSTEM OVERVIEW Dr. Ellen Taylor University of California - Berkeley.
FGM peer CDR GSE - 1 Berlin, April 6, 2004 Ground Support Equipment Concept (GSE) Werner Magnes Institut für Weltraumforschung (IWF) Austrian Academy of.
FGM peer PDR GSE - 1 Braunschweig, October 8-9, 2003 Ground Support Equipment Concept (GSE) Werner Magnes Institut für Weltraumforschung (IWF) Austrian.
RBSP Radiation Belt Storm Probes RBSP Radiation Belt Storm Probes 3-4 Sept. 2008EFW INST+SOC PDR447 Command, Telemetry, and Ground Support Equipment (CTG)
TRIO-CINEMA 1 UCB, 2/08/2010 LVPS & Switching Dave Curtis UCB/SSL Space Sciences Laboratory University of California, Berkeley.
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.
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.
THEMIS Instrument Pre-Environmental Review 1 UCB 5/02/2005 THEMIS Instrument Pre-Environmental Review Project Status May 2, 2005 Peter R. Harvey THEMIS.
THEMIS Instrument PDR 1 UCB, October 15-16, 2003 ESA & SST (ETC) Interface Board Preliminary Design Review Robert Abiad University of California - Berkeley.
RBSP Radiation Belt Storm Probes RBSP Radiation Belt Storm Probes RBSP/EFW I-PER 21 January EFW Systems Engineering Michael Ludlam Space Sciences.
Pre-Ship IIRT Telecon EFI 1 Telecon, Dec. 5, 2006 THEMIS Pre-Ship IIRT Telecon EFI Preamp Current Consumption John Bonnell EFI Lead University of California.
THEMIS Instrument CDR 1 UCB, April 20, 2004 ESA & SST (ETC) Interface Board Critical Design Review Robert Abiad University of California - Berkeley.
TRIO-CINEMA 1 UCB, 2/08/2010 ClydeSpace Electronic Power System Yashraj Khaitan Space Sciences Laboratory University of California, Berkeley.
THEMIS IDPU PDRPCB- 1 UCB, October 16, 2003 IDPU Power Control Board (PCB) Peter Berg University of California - Berkeley.
RBSP Radiation Belt Storm Probes RBSP Radiation Belt Storm Probes RBSP/EFW CDR /30-10/1 647 Ground Support Equipment Will Rachelson University of.
TRIO-CINEMA 1 UCB, 2/08/2010 System Design Dave Curtis UCB/SSL Space Sciences Laboratory University of California, Berkeley.
BonnellFIELDS iCDR – AEB Solar Probe Plus FIELDS Instrument CDR Antenna Electronics Board AEB J. Bonnell, D. Seitz UC Berkeley, SSL
Power Philip Luers NASA/GSFC Code 561 August 16-17, 2005.
DATA PROCESSING UNIT (IDPU)
GLAST Large Area Telescope:
Particles and Fields Package (PFP) SWEA Pre-CDR Peer Review
FGM CDR FGM Electronics (FGE) Ronald Kroth MAGSON GmbH Berlin Germany.
University of California - Berkeley
INSTRUMENT DATA PROCESSING UNIT (IDPU) REQUIREMENTS
Calorimeter Mu2e Development electronics Front-end Review
Preliminary PCB Design
Liquid LVs propellant consumption control terminal system
Bill Donakowski Mechanical Engineer UCB/SSL
INSTRUMENT DATA PROCESSING UNIT (IDPU)
ESA GSE.
Electric Field and Waves Instrument (EFW)
Instrument Data Processing Unit (IDPU)
Mars Atmosphere and Volatile EvolutioN (MAVEN) Mission
Boom Electronics Board (BEB)
THEMIS FM4/FM5 INSTRUMENT SUITE
Low Voltage Power Supply & Power Controller Board
University of California, Berkeley
The Electric Circuit.
Preliminary PCB Layout and Design: Team 16
CrystaLatchTM 1x8 Fiberoptic Switch
CrystaLatchTM Mini 1x3,1x4 Solid State Fiberoptic Switch
CrystaLatchTM 1x4 Fiberoptic PM Switch
CrystaLatchTM Mini 1x3,1x4 Solid State Fiberoptic Switch
CrystaLatchTM 1x3,1x4 Solid State Fiberoptic Switch
Presentation transcript:

Preliminary Design Review IDPU Backplane Preliminary Design Review Peter Berg University of California - Berkeley

Overview Backplane Overview Requirements Specifications Design Mass and Power Schedule Issues

Requirements Fault Protection IN.BKP-1. The IDPU BKP shall allow route power independently to instrument electronics allowing for autonomous fault protection features to ensure the health and safety of the instruments (ref IN.DPU-11) Commands/Telemetry IN.BKP-2. The IDPU BKP shall transport instrument data between instrument cards and the DCB.(ref IN.DPU-15) IN.BKP-3. The IDPU BKP shall transport engineering telemetry sufficient to safely turn-on and operate all instruments (temperatures, currents, voltages, and bi-levels) as defined in Instrument-IDPU ICDs(ref IN.DPU-16) IN.BKP-4. The IDPU BKP shall transport operational commands and test programs for all instruments as detailed in the Instrument-IDPU ICDs (ref IN.DPU-17) IN.BKP-5. The IDPU BKP shall transport initialization parameters to the Instruments as detailed in the Instrument-IDPU ICDs(ref IN.DPU-18)

Requirements Power Timing Signals IN.BKP-6. The IDPU BKP shall distribute a 2^23 Hz Clock from the DCB to the DFB and FGM(ref IN.DPU-23) IN.BKP-7. The IDPU BKP shall distribute a 1 Pulse Per Second (1PPS) to the DFB and the FGM(ref IN.DPU-25) IN.BKP-8. The IDPU BKP shall distribute a once-per-spin reference pulse (SRP) to the SST and ESA(ref IN.DPU-27) IN.BKP-9. The IDPU BKP shall distribute a Spin Sector Clock with 2^14 phase pulses per spin to the ESA and SST (synchronized with the SRP) (ref IN.DPU-28) IN.BKP-10. The IDPU BKP shall provide ESA and SST synchronization by distributing spin count data from the DCB to these systems. (ref IN.DPU-34) Power IN.BKP-11. The IDPU BKP shall transport Instrument regulated, switched and current-limited voltages as detailed in the Instrument-IDPU ICDs(ref IN.DPU-44) IN.BKP-12. The IDPU BKP shall transport LV transient power to actuators as detailed in the Instrument-IDPU ICDs(ref IN.DPU-45) Mechanical IN.BKP-13. The IDPU BKP shall accommodate at least five 6U VME cards(ref IN.DPU-51a)

Electrical Specification Specifications Electrical Specification Captured in THM_IDPU_001 revision H Details Interface Requirements for Each Board SST : Solid State Telescope Analog-to-Digital Conversion BEB : Boom Electronics Board DFB : Digital Fields Board FGE-PCB: Fluxgate Electronics and Power Control Board DCB-ETC: Data Controller Board and Esa-ssT Circuit LVPS : Low Voltage Power Supply connector

Electro-Mechanical Specifications Connectors VME standard connectors 3x32 format M55302 (Class1) Mate/Demate Cycles >500 Dielectric isolation >1000V (need 200V) J1 Location only Allows use of commercial backplanes for testing Female connectors (standard) to all boards except LVPS Male connector to LVPS Board-to-board Separation Current Spacing is 0.585” Driven by Board Heights Dependent upon tallest parts (e.g. large caps) Dependent upon electrical shielding Preliminary height has been checked by board designers

Design Considerations Grounds 5 Digital 8 Analog 7 Power Digital and Analog Signal Separation Digital Signals A1-C8 Analog & Power A9-C32 Voltage Capabilities Worst Case Floating Voltages +/-100V Isolation >1000V Current Capabilities Worst Case Current Req – Actuators @ 2A Pin Capabilities @ 3A

Design PINOUT (THM_IDPU_001H)

Design PINOUT (THM_IDPU_001H)

Design PINOUT (THM_IDPU_001H)

Design PINOUT (THM_IDPU_001H)

Specifications Connector Specifications (Board Interface)

Specifications Connector Specifications (LVPS Interface)

Mass & Power Power Mass Unterminated Backplane No power dissipation Assuming 0.585” board-to-board pitch Allocation 250 grams

Schedule Development Plan Use Commercial Backplanes DIN41612 for boards Allow FLT Board Dimensions to Define Spacing as needed Allow Chassis Fab/Assy Details to Define BKP features Layout and MIL-55110 PWB Fabrication Jan 2004 Coupon Checks at GSFC for Flight Backplanes

Issues Issues Board Design, Selection of Components Impact BKP Any of 5 boards can change BKP dimensions Recent Addition of SST reduced BKP pin margin to 8% If Necessary, can reduce Ground pins Board Height Impacts IDPU ICD Footprint