BUSAT: Taylor Universitys Involvement - PowerPoint PPT Presentation

1 / 27
About This Presentation
Title:

BUSAT: Taylor Universitys Involvement

Description:

Above: a view of an aurora, caused by collisions of charged particles in the ... Emissions and ionization (diffuse aurora) Important for M-I coupling (L0-1) ... – PowerPoint PPT presentation

Number of Views:27
Avg rating:3.0/5.0
Slides: 28
Provided by: zachp3
Category:

less

Transcript and Presenter's Notes

Title: BUSAT: Taylor Universitys Involvement


1
BUSAT Taylor Universitys Involvement
  • Presented by
  • Zach Palmer
  • David Patterson
  • July 9, 2008

2
About BUSAT
  • Boston University Student satellite for
    Application and Training
  • Competing in the USAF Nanosat 5 competition

3
Stated Mission Overview
Perform measurements of the precipitating
energetic electron fluxes from low Earth orbit
over the high latitude auroral zones and to
simultaneously image the auroral emissions caused
by these electrons in order to better understand
the coupling between the Earths Magnetosphere
and Ionosphere (L0-1) and to construct a modular
subsystem bus design allowing for standardized
mechanical and electrical interfaces (L0-2)
4
BUSAT mission, simplified
  • To provide an opportunity for undergraduate
    research and design
  • To collect important data useful for space
    weather forecasting

5
Space weather
The magnetic field of the Earth protects us from
energetic charged particles emitted from the sun
during period of solar activity.
6
Space weather
Below a view of the suns corona, taken during a
total solar eclipse
Above a view of an aurora, caused by collisions
of charged particles in the Earths upper
atmosphere
7
Space weather
Below Particle populations in the inner
Magnetosphere (from NASA-RBSP website)
Above Large-scale magneto-spheric current
systems (from NCAR website)
8
BUSAT Instrumentation
1. Auroral Imager A CCD camera-based system
that can image the aurora in multiple
wavelengths (L1-1) 2. Imaging Electron
Spectrometer a heritage instrument that
measures energetic electrons (30 keV to 500 keV)
and can resolve the particles pitch angle
(L1-2) 3. Langmuir Plasma Probe Measures low
energy, thermal electrons (0 to 6 eV) (L1-2) 4.
Very Low Frequency Receiver Integrates VLF
power in six separate frequency bands providing
knowledge of VLF waves (L1-3) 5. Magnetometer
The magnetometer is able to sample in three axes
(L1-4). Measures Birkeland currents.
9
Taylors Responsibility for BUSAT
  • Plasma Probe
  • VLF Receiver
  • Comm. System

10
Comm. System (David Patterson)
11
TUSat1 Satellite
  • Project from 2001-02
  • Prominently featured spherical Langmuir Plasma
    Probe

12
Deus Ex Satellite
  • 07-08 Eng. Phys. Senior Design Project
  • Included both Plasma Probe and VLF Receiver
  • Equipment being adapted for use with BUSAT

13
Langmuir Plasma Probe
  • Purpose Measures low energy, thermal electrons
    (0 to 6 eV) (L1-2)
  • Explanation Will tell us the densities of
    electrons and ions along the path of the
    satellite, and information can also be used to
    find the electron temperatures.
  • Original (Deus Ex) Design by Dan Brinks

14
Theory of Operation
  • Bias the probe to a given voltage relative to the
    surrounding plasma
  • Measure the resulting current flowing from the
    plasma to the probe

15
Expected Measurements Plasma Probe
Taken from Measurement Techniques in Space Plasmas
Taken from Satellite Observations of
Lightning-Induced Electron Precipitation
16
Design Plasma Probe
  • Measure electron densities ranging from 102 to
    108 e-/cm3
  • Software programmable bias voltage ranging from
    -9V to 9V
  • Logarithmic current amplifier using matched
    transistors (provides 6 orders of dynamic range)
  • Temperature measurements of transistors for
    compensation
  • 12 bit ADC
  • Calibration circuitry
  • Voltage sweep capable

Taken from Measurement Techniques in Space Plasmas
17
LPP Software Block Diagram
18
Collector/Boom Design Plasma Probe
For the LP to correctly gather data, it cannot be
within the Debye sheath. Hence, the deployment
length must be greater than the Debye length. In
the Ionosphere, the Debye length is roughly 1 cm.
  • Design
  • Spherical, aluminum collector
  • Tri-axial cable
  • Boom

Taken from Measurement Techniques in Space Plasmas
19
(No Transcript)
20
Very Low Frequency Receiver
  • Whistler waves - ducted EM plasma waves.
  • Produced by
  • lightning in the atmosphere
  • magnetospheric processes
  • Energize particles
  • Particles enter loss cone
  • precipitation (L0-1)
  • Emissions and ionization (diffuse aurora)
  • Important for M-I coupling (L0-1)

Whistler wave propagation (from
www.astronomie.be/radioastronomie/vlf.htm)
21
Very Low Frequency Receiver
  • Detect whistler waves
  • Low pass front end
  • Amplification
  • Band-pass filters
  • AC to DC Conversion
  • Sample data
  • Data transmission

22
Status of VLF
  • Indeterminate
  • Possibility of handing project off to Jeff
    Dailey, a professional engineer out of Fort Wayne
  • May need to be de-scoped entirely

23
Original Plan
24
Current Plan
25
Benefits of splitting the projects up
  • Lets me focus on getting one system board
    design operational, instead of three.
  • Less chance of a system failure knocking out both
    systems.
  • Ability to de-scope either project independently
    of the other one, based on progress.

26
Rest of the summer
  • Finish revised board design for the Langmuir
    Plasma Probe instrument
  • Populate flight board
  • TESTING DEBUGGING
  • Balloon Flight Test (SuperLaunch)
  • Coding

27
Acknowledgements
  • Dan Brinks Plasma Probe
  • Jeff Moore VLF Receiver
  • Jeff Dailey Comm System
  • BU nanosatellite team
  • Dr. Hank Voss
  • Dr. Will Holmes
  • Dr. Joel Gegner
Write a Comment
User Comments (0)
About PowerShow.com