EagleSat’s Electronic Power Subsystem

Slides:

Advertisements

Similar presentations

Supercapacitor Energy Storage System for PV Power Generation

Advertisements

Solar Cell Efficiency Flight Readiness Review Teddy Bounds Angela Dunn Joel Sasser.

Week 3 Electrical Circuits and Components. It’s a Radio!

University of Kansas EPS of KUTEsat Pathfinder Leon S. Searl April 5, 2006 AE256 Satellite Electrical Power Systems.

Critical Design Review VST Vigilant Sensing Technologies Joel Keesecker, Mark Kien, Pat Hauser.

Introduction to Space Systems and Spacecraft Design Space Systems Design Power Systems Design -I.

Acknowledgments Summary of MAVs Design Criteria Design Solution Conclusions and Future Work Energy Harvesting for Micro-Air Vehicles Testing Harvesting.

RC Circuit Experiment 1. Set up three different RC circuits using the components supplied. 2. Measure the voltage across the capacitor as a function of.

1 Electrical Power System By Aziatun Burhan. 2 Overview Design goal requirements throughout mission operation: Energy source generates enough electrical.

TE-MPE-EE, 02-Apr CLIQ Power supply design J. Mourao TE-MPE-EE.

Electronic Component Functions What is this component doing my in electronic device?

EUSO BALLOON Battery Power Pack (PWP) RIKEN/UAH Héctor Prieto, Katsuhiko Tsuno, Marco Casolino.

TE-MPE-EE, 16-Apr CLIQ Power supply design J. Mourao TE-MPE-EE.

My Chapter 18 Lecture Outline.

COMS Transceiver – RF DataTech LRT470 Frequency: MHz Operation: Half-Duplex Max. RF Transmit Power: 750mW Typical Power Draw at 750mW RF: 3.5W Bandwidth:

Power System David Riddle. Overview Power Board Energy Budget of ERAU Eagle Satellite TASC Solar Panel Test TrisolX Soler Cells.

KUMU A’O CUBESAT Amy Blas. Background 2 What is CubeSat?  10x10x10 centimeter cube  Launched in lower earth orbit (LEO)  The project started last.

Xin Jin Zelun Tie Ranmin Chen Hang Xie. Outline  Project overview  Project-specific success criteria  Block diagram  Component selection rationale.

ENERGY SCAVENGING SYSTEM ABSTRACT On a daily basis, energy is constantly being wasted in both large and small scales. In the U.S alone, 56% of energy produced.

Electrical Rules and Components

Morehead State University Morehead, KY Prof. Bob Twiggs Power Systems Design

Cells in Series and Parallel (page 310) Cells in Series and Parallel Dry cells can be connected together into two basic types of circuits: series.

General Purposes Input/ Output Daughter board for Univ Eval Rev B Julien Cercillieux University of Hawaii

The energy change in a thermocouple is : 1.E E to E H 2.E S to E E 3.E L to E E 4.E H to E E :20.

LDO or Switcher? …That is the Question Choosing between an LDO or DC/DC Converter Frank De Stasi Texas Instruments.

Parts of An Electric Circuit Recall: a circuit is a closed path Electric circuit: closed path that flowing charge follows Constructing an electric circuit:

Electronic Components Circuit/Schematic Symbols. RESISTOR Resistors restrict the flow of electric current, for example a resistor is placed in series.

Do now! Can you continue the sheet you started last lesson? (“Another current model”)

Hybrid Power Controller (HPC) Final Presentation Senior Design II.

Twenty Questions Electronics. Twenty Questions

Critical Design Review The University of Northern Colorado GoGreenSAT Jessica Gage, Max Woods, Brent Hill, Ryan Marshall, Zach Sears Feb

Hybrid Power Controller (HPC) Mid-Semester Presentation Senior Design II.

EUSO BALLOON Battery Power Pack (PWP) RIKEN/UAH Héctor Prieto, Katsuhiko Tsuno, Marco Casolino 1.

18240 Element two - Components INPUTS OUTPUTS PURPOSE TYPICAL USE.

Series and Parallel Circuits. Series Circuits ► Are the simplest type of circuits. ► Series circuits – all the components (lamps, cells, switches, etc.)

What we will do today: Introduce the new topic on Electronic Components. Identify the three main parts of any electronic system. Give examples of output.

K UMU A ’ O C UBESAT Amy Blas March 7, W HAT IS C UBE S AT ? 10x10x10 centimeter cube Launched in lower earth orbit (LEO) Started last semester.

Solar Power Charge Controller. Solar Power Charge Controller Introduction  A charge controller, or charge regulator is basically.

TRIO-CINEMA 1 UCB, 2/08/2010 ClydeSpace Electronic Power System Yashraj Khaitan Space Sciences Laboratory University of California, Berkeley.

 uAzyzK4&feature=related.

6.2 ELECTRONICS. CAPACITOR An electrical device used to store electrical charge.

Ashan Perera Senior Design Project - Electronic System for Remote Water Quality Monitoring.

OBC Shawn Thompson Demi Vis 1. OBC Outline Requirements Concept of Operations Subsystem Description Development Environment/Tools Theory of Operations.

Front End. Charge pre-amp and detector Voltage regulator. TOP side. Detector linear voltage regulator BOTTOM side. Charge pre-amp.

COMP541 Transistors and all that… a brief overview

Solar Energy Generator: Design Rendering Description

Planetary Lander PDR Team Name

CHARGE AND LOAD PROTECTION IN SOLAR POWER MANAGEMENT

Electronic Devices Ninth Edition Floyd Chapter 17.

음향 시스템 사양서 POWER SUPLY WITH 3.5 PHOENIX CONNECTOR AMX: PSN6.5

Electricity How & where it’s used Review of the atom

POWER AMPLIFIERS E 5:4 LAB.GRUPPEN NAME MODEL 제조사 General

Check you understanding:

Graduation Project-II submitted to:

Circuit Circuit – A complete path along which electrons flow (negative to positive) 3 basic types Series Parallel Series-Parallel Combo.

Photovoltaic (PV) Systems

Cell Phone Charger Project

Data Distribution Board

FIGURE 12-1 A Leyden jar can be used to store an electrical charge.

SOLAR POWER CHARGE CONTROLLER

Series 5300 Lithium Cell Formation System

COMP541 Transistors and all that… a brief overview

Mitsuru Imaizumi Space Solar Cells -- I -- HTV-6

Team Icarus Brandon Scott Bosomworth Edgar Alejandro Flores

Linear Technology Corporation

Radhabai Kale mahila mahavidyalaya,ahmednagar Department of Physics

Solar Cooler Team 7 Karim El-Najjar Hanfei Deng Kunjie Zhao.

BIRDS-4 Computer Aided Drawing (CAD)

Lecture 2 Electrical and Electronics Circuits. After you study, and apply ideas in this Lecture, you will: Understand differences among resistance, capacitance,

Presentation transcript:

EagleSat’s Electronic Power Subsystem Jon Lowe

Electronic Power Subsystem (EPS) Outline Requirements EPS Description Power Flow Solar Cells/Panels EPS components Energy Budget

EPS Requirements Launch Power Activity No electronics active during launch Deployment Switch Deployment switch on standoff rail disconnects all power while depressed Access Port Locations All connectors located in designated areas Remove Before Flight Pin Will have a remove before flight pin EPS EPS will manage all power distribution Solar Panels Solar panels will provide sufficient power to fulfill EagleSat’s power need

EPS Description Collects power for EagleSat using solar panels Super capacitors store energy Vcc Batt powers Radio, Regulator Regulator powers Vcc Sys Vcc Sys powers OBC, Temperature sensors, Modem, GPS OBC determines standby/off

Power Flow Solar Panels Voltage Regulator OBC Modem GPS Temperature Sensors Super Capacitors VCC BATT VCC SYS Radio

Solar Cells TriSolX Solar Wings 28% Efficient InGaP/GaAs/Ge Triple Junction Solar Cells: Type- T01 Voltage (Open circuit) 2.62 V Voltage (Max Power) 2.33 V Current (Max Power) 14.6 mA Power (Max Power) 34 mW Dimensions: 26.3mm x 10mm

Solar Panels Side Panels (±Y) Top Panel (-Z) Front Panel (+X)

Supercapacitors Eaton HV1030-2R7106-R 10F (3V) Supercapacitors UL Listing: BBBG2.MH46887 5 per series bank (15V) 2 banks in parallel providing 4F 1125J total charge at max power

Deployment Switches 3 Total switches 2 on standoff rails 1 remove before flight pin Power disconnected when switches depressed and remove before flight pin present

Voltage Regulator RECOM R-78E3.3-0.5 Input Range: 4V-28V Output Voltage: 3.3V Output Current: 500mA

Temperature Sensor Microchip TC1047A Input Voltage 2.5V to 5.5V, 7V absolute max Temperature Range: -40℃ to 125℃ Output Voltage: 0.1V to 1.75V

Temperature Sensor Vout = (10mV/℃)(Temperature ℃) + 500mV

Cumulative Energy Budget

Cumulative Energy Budget

EPS Summary All requirements are met No electronics shall be active at launch Deployment switches prevent EagleSat from being powered when switches are depressed Access ports are present and allow access to connectors while in P- POD RBF pin prevents EagleSat from being powered until removed EPS manages EagleSat’s power distribution Solar Panels provide sufficient power for EagleSat to function properly

Questions?

Backup Slides

EPS Board Schematic

Temperature Sensor Schematic

Remaining Solar Panels Back Panel (-X) Bottom Panel (+Z)

Perfect Energy Budget

Worst Case Scenario Energy Budget