STAR Public
  • Space Technologies and Rocketry
  • Quick Links
  • Member Info
    • Membership Requirements
    • Elections
  • Current Projects
    • ALULA: First Leap
      • Project Objectives
      • High-Level System Parameters
      • Propulsion
      • Avionics
      • Airframe
      • Recovery
    • Caldera: IREC 2024
      • Airframe
      • Avionics
      • Airbrakes
      • Recovery
      • Staging
      • KELSE-Y (Payload)
  • Previous Projects
    • CalVistor: IREC 2023
      • Recovery (CalVistor)
      • Airframe (CalVistor)
      • Airbrakes (CalVistor)
      • Payload (CalVistor)
    • ELLIE
      • ELLIE Overview
      • Timeline
      • Physical System
      • Electrical and Software
      • Ongoing Research
    • MINDI
      • Airframe
      • Recovery
    • PinkBeary
      • Altimeter Wiring Update
      • Airframe Diameter
      • Fin Sizing
      • Pyro Bolts
      • Electronics
    • CAS
      • CAS Overview
      • Core Module
      • Radio Module
      • Pyro Module
      • Prop Module
      • CAS Core Revised
      • CAS Radio Revised
    • DAVE
      • Summary of DAVE
      • FAQ's
      • DAVE Blog
    • Bear Force One: IREC 2020/2021
      • Airframe
      • Recovery
        • Parachute Harness
        • Avionics Bay
          • Avionics Bay Glossary
          • Avionics Bay Assembly
        • Black Powder Holders
        • Payload
          • Payload Subsystem Report
          • IRIS
            • Peripherals Diagram
            • Pinout Diagram
            • Power Flow Diagram
          • MFC (2020)
          • Stabilization
          • Structures
          • Cameras
          • Muons - Archived
          • IRIS Legacy - Archived
    • Arctos
    • AirBears
  • Frequently Asked Questions
  • Tutorials
    • Media
      • How to make a decent video
    • RFS Safety Training
    • Submitting Reimbursements
    • Software Setup
      • SolidWorks Installation
      • VMware/Boot Camp setup
      • [In-Progress] SolidWorks PDM Setup
      • ANSYS Installation and Setup
      • Solidworks Assemblies Basics
      • OpenRocket Installation
      • Deprecated Software
        • [deprecated] Getting Started With GrabCAD Workbench
        • [deprecated] Using GrabCAD Workbench in SolidWorks
        • [deprecated] Connecting to CalSTAR's Server
        • [deprecated] Installing and Licensing Converge CFD
    • General Tutorials
      • How to Use SolidWorks Templates
      • [In Progress] Digikey Ordering Guide
      • SolidWorks Training Session
      • SolidWorks Training Tutorials
    • Enery Systems
    • Manufacturing
      • Material Properties and Uses
      • 3D Printing (FDM)
      • Laser Cutting
      • FabLight: Metal Laser Cutter
      • Milling
        • Othermill
        • [Empty] Manual Mills
      • Tolerancing
      • Fasteners
      • Suppliers
      • Composite Materials and Best Practices
      • 8020 Extrusions
    • Airframe
      • Airframe Components
      • Tube Attachement
      • OpenRocket
      • Tube Winding
      • Sizing Fins
      • Attaching Fins
      • Rail Buttons
      • Motor Retention
      • Painting Rockets
    • Avionics
      • KiCad
      • Git
      • Project Management
      • Firmware Development Environment
      • Ground Station Software
      • Intro to Embedded C Programming
      • Schematic and Layout Review
      • Board Design Reference
      • Using Lab Equipment
      • Reflow Oven
      • Soldering
      • Debugging Tips/Testing
      • Ham Radio Basics
      • Component Selection
      • High Temperature Batteries
    • Outreach Activities
      • Straw Rocketry
      • Spacecraft Structures
      • Alka Seltzer Rockets
      • Paper Airplane Launcher
      • Coding Workshop
    • Operations
      • SolidWorks file conventions
      • Style Guidelines
      • LaTeX
    • Payload
    • Propulsion
      • Feed System Types
      • Rocket Propulsion Analysis Tutorial
      • Ignition Devices
      • Creating a Piping and Instrumentation Diagram P&ID
      • Pipes, Fittings, and Components
      • Injectors
    • Recovery
      • Parachute Sizing
      • Avionics Sled
      • [in progress] Altimeters
      • Wire Design and Routing
    • Simulations
      • FEA Simulation Tutorial using ANSYS
      • Getting Started with CONVERGE (2.4)
      • [Empty] Simulation Methods
      • Mathematical Models
      • SimScale
        • SimScale 3D CFD
      • Using ANSYS
      • ANSYS 19.2 2D CFD Tutorial
      • ANSYS 19.2 3D CFD Tutorial
    • Administrative
      • Azure Server
    • Page 1
  • Reference
    • Reference
    • Glossaries
      • Propulsion
      • Common Acronyms and Definitions
    • Brand Guidelines
    • Legal
    • High Power Rocketry (HPR)
      • NASA HPR Reference
      • L1 and L2 Certification Tips & Tricks
      • HPR Kits
      • HPR Design
      • HPR Suppliers
      • STAR HPR Certification
    • Ham Operators
    • X-Winder Update Log
    • Safety
      • Materials
      • Tools
      • Electrical
      • Range Safety
  • Testing
    • Test Forms
    • Damage Report Forms
    • Airframe Tests
    • Recovery Tests
      • Ground Ejection Test
  • Onboarding
    • Intro Projects
      • Airframe
      • Avionics
        • PCB Design Mini-Project
      • Operations
      • Payload
      • Propulsion
      • Outreach
      • Recovery
      • Media
      • Safety
      • Simulations
      • Old Intro Projects
        • Payload 2020 Intro Project
        • Propulsion Fall 2019
        • Avionics 2018
        • Recovery 2018
        • Avionics (new intro project Fall 2021)
  • Project Management
  • History of the Team
    • Early Years
    • Executive History
    • Launch History
      • 2022-12-03 MINDI First Flight
      • 2022-09-17 Pinkbeary First Flight
      • 2019-11-16 AirBears First Flight
      • 2018-03-24 Final flight for Arktos
      • 2017-04-08 Competition Launch, NASA SL 2017
      • 2017-03-25 FRR Re-Re-Flight, NASA SL 2017
      • 2017-03-12 FRR Re-Flight, NASA SL 2017
      • 2017-03-04 FRR Flight, NASA SL 2017
      • 2016-12-04 CDR Subscale Flight, NASA SL 2017
    • Fleet
  • How to use GitBook
Powered by GitBook
On this page
  • Perfectflite StratoLoggerCF
  • Altus Metrum EasyMega
  • Eggtimer Quantum
Export as PDF
  1. Previous Projects
  2. PinkBeary

Electronics

Electronics used for SSEP

PreviousPyro BoltsNextCAS

Last updated 1 year ago

Perfectflite StratoLoggerCF

This altimeter will be used in both the upper stage main and drogue parachute deployment.

Purpose (Upper Stage Main): Dual Side, Dual Deploy Entails: Pyro leads to main and drogue (redundant), deployment based on elevation and velocity.

Purpose (Lower Stage Main): Single Side, Single Deploy Entails: Pyro leads to main (redundant), deployment based on elevation and velocity.

Specs:

  • Works to 100,000 feet MSL, audibly reports peak altitude and maximum velocity after flight.

  • Stores 16 flights of 18 minutes each (altitude, temp­erature, and battery voltage at 20 samples per second) for download to a computer with the optional DT4U USB interface. Hi-speed sampling and storage of battery voltage serves as a useful aid in diagnosing intermittent problems with your battery, switch, and wiring. All data are preserved with power off.

  • Deploys drogue and main chutes with audible ematch continuity check.

  • Outputs capable of 5A current for 1 full second to allow use with nearly any ematch or ematch substitute. Reverse polarity protection prevents spontaneous firing if battery is connected backwards.

  • Main chute deployment altitude is adjustable from 100 feet to 9,999 feet in 1 foot increments. 9 presets allow for quick change in the field.

  • No mach delay necessary for mach+ flights: Automatic MachLock assures proper operation with any flight.

  • Brownout protection will tolerate 2 second power loss in flight – no need for multiple batteries.

  • Precision sensor & 24 bit ADC yield superb 0.1% accuracy.

  • Built-in voltmeter reports battery voltage on powerup – no more guessing about battery condition.

  • Post flight locator siren aids in locating your rocket.

  • Confusion-free individual terminal blocks – unreliable multiple wires per terminal are not necessary. Dedicated switch terminal block eliminates the need for splicing switch into battery wire.

  • Highly resistant to false trigger from wind gusts; tested in 100+ MPH winds!

  • Selectable apogee delay for dual altimeter setups prevents overpressure from simultaneous charge firing.

  • Low power design runs for weeks on a standard 9V alkaline battery. Post-flight locator siren will run for months, giving you multiple “second chances” to find a lost rocket.

  • Telemetry output for real-time data in flight with your RF link.

  • Rugged SMD construction, stringent QC testing, and internal self-diagnostics assure uncompromising reliability.

  • Wide operating temperature range of -40F to +185F.

  • Measures just 2.0"L x 0.84"W x 0.5"H, fits 24mm tube, weighs just 0.38 oz.

Altus Metrum EasyMega

The Altus unit comes at a hefty cost, but has the advantage of being able to provide angle caculations. using two different altimeters for the same deployment is not advised since it would require two different switches.

Purpose: Lower Stage Parachutes (Drogue and Main, DSDD), Separation Mechanism Entails: 3 additional programmable pyro events for separation mechanism (redundant).

Specs:

  • 2.25 x 1.25 inch board designed to fit inside 38mm airframe coupler tube

  • Supports dual deployment and 4 additional pyro events.

  • Pyro events are configurable and can be based on time and various flight events and status, including angle from vertical (for safety in staging and air start flights).

  • Barometric pressure sensor good to 100k feet MSL

  • 1-axis 105-g accelerometer for motor characterization

  • 3-axis 16-g accelerometer for gyro calibration

  • 3-axis 2000 deg/sec gyros

  • 3-axis magnetic sensor

  • On-board non-volatile memory for flight data storage

  • USB for power, configuration, and data recovery

  • Integrated support for LiPo rechargeable batteries

  • User choice of pyro battery configuration, can use primary LiPo or any customer-chosen separate pyro battery up to 12 volts nominal.

  • IMPORTANT! Easy Megas must be wired BACKWARDS (i.e. a custom JST connector must be assembled to plug the negative battery terminal into the "positive" end and vice versa) due to manufacturer decision.

Eggtimer Quantum

Purpose: Airstart (Motor Ignition)

Entails: Single lead to motor ignitor

Specs:

  • 66mm x 25mm, weight ~12 grams

  • Dual-ended output - pyro igniter is dead until near deployment for safety

  • Records altitude up to 60,000 AGL

  • Drogue programmable 0-3 seconds after noseover, main programmable from 100-2000 feet

  • Wifi compatible - arm via phone

  • Polarity-independent

  • Comes in a kit - must be soldered and assembled

Manual:

Manual:

http://www.perfectflite.com/Downloads/StratoLoggerCF%20manual.pdf
https://altusmetrum.org/AltOS/doc/altusmetrum.pdf