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Team Parro

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Shawn Mullins Thermal Design / Construction. Josh Hignight ... Tim Butler Software Design. Project Proposal. Using a humidity, UV, and temperature sensor, ... – PowerPoint PPT presentation

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Title: Team Parro


1
Team Parro
  • Project HUSP

2
Team Members
  • Jason Rollins Project Manager / Electrical
    Design
  • Shawn Mullins Thermal Design / Construction
  • Josh Hignight Mechanical Design / Construction
  • Tim Butler Software Design

3
Project Proposal
  • Using a humidity, UV, and temperature sensor,
    Team Parro will plot a graph of humidity vs.
    altitude, UV vs. altitude, UV vs humidity, and
    attempt to determine the height of the region
    know as the ozone layer.

4
Humidity
Humidity and Temperature Dependence
NASAs UARS Project
Present Data on Humidity vs. Altitude
5
Humidity Sensor
Honeywell Sensors
6
UV Sensor
  • No specific sensor chosen
  • Issues such as plastic film availability must be
    addressed
  • Will the plastic affect the amount of UV that
    reaches the sensor?
  • A plastic window may not be a viable option. If
    so, a UV sensor more resistant to temperature
    will need to be acquired

7
Design
  • The payload will consist of two boxes, a UV
    sensor, humidity sensor, temperature sensor,
    balloon sat circuit board (includes EEPROM chip,
    and processor), an analog to digital converter,
    and a plastic window.
  • The balloon sat circuit board will reside in the
    smaller box and connect to the sensors through
    the ADC. Humidity and temperature sensors will
    be outside of both the inner and outer box, while
    the UV sensor will remain inside the larger box.
  • Hand warmers will be placed inside the larger box
    to keep the temperature above the electronics
    operating temperature

8
Basic Electrical Design
A VERY basic design of the board and sensor
interface
9
Payload Construction
  • Once a UV sensor is agreed upon and the total
    power is checked, all parts needed will be
    ordered.
  • Tim will immediately begin working on software
    development.
  • Once parts begin to come in Josh and Sean will
    modify already constructed boxes to fit the needs
    of the sensors.
  • Jason will then work on interfacing sensors with
    the balloon sat and testing sensors

10
Mission Operations
  • The software will be run and the box sealed. The
    sensors will then begin collecting data and will
    continue to do so until the flight is completed
    when the battery power or memory will run out.
    The payload will then be recovered and the data
    collected from the EEPROM chip via a serial
    connection.

11
Data Acquisition and Analysis
  • All data from the flight will be recorded on the
    EEPROM chip that will be located on the main
    Balloon Sat circuit board. Care has been taken
    to ensure that the EEPROM is sufficient for this
    job. Because all data is stored inside the
    payload it self, the payload will have to be
    recovered after the flight is completed. The
    data will then be taken off of the EEPROM and put
    on a computer where it will be plotted against
    altitude using MathCAD software.

12
Project Management
  • Jason Rollins responsible for electrical work
    including power consumption, sensor interfacing,
    electrical design, and balloon sat testing
  • Sean Mullins Thermal design and acquisition of
    parts for thermal needs, as well as thermal
    testing
  • Josh Hignight Box construction and overall
    mechanical design
  • Tim Butler All things software, including RTC
    operation, sensor data testing and data
    recovering and ploting

13
Schedule
  • Task Will be completed by
  • Box Construction Complete
  • Board Construction Complete
  • Sensor Acquisition Complete
  • Battery Testing Complete
  • Sensor/Parts Testing April 8th 2005
  • 5 Meter Impact Test April 15th 2005
  • Interface Sensors w/ Board April 22nd 2005
  • Software Debug/test April 29th 2005
  • CDR TBA
  • FFR TBA

14
Budget
Weight Budget
Expense Budget
Object Weight(g) Electronics 67 Inner
Box 78.5 Outer Box 112.75 Hand
Warmers 66 Battery 20 Sensors Negligible Tota
l Weight 344.25
Object
Price
Foam Board 5 Hand Warmers 10 Sensors 125
Electronics Provided Wire
10 Plastic
10 Batteries 10 Total 160
Max allowable 500
Weight Left 155.75
15
Sources for Facts and Figures
  • Sensor
  • http//content.honeywell.com/sensing/prodinfo/humi
    ditymoisture/009012_2.pdf
  • http//www.sensorsmag.com/articles/0701/54/main.sh
    tml
  • Science
  • http//www.igac.noaa.gov/newsletter/21/measurement
    s.php
  • http//www.es.lancs.ac.uk/casestud/case13.htm
  • http//www.indiana.edu/climate/g470/Lectures/Humi
    dity/MoistAir.html
  • http//www.indiana.edu/climate/g470/Lectures/Humi
    dity/MoistAir.html
  • http//www.grida.no/climate/ipcc_tar/wg1/080.htm
  • NASA related projects and info
  • http//svs.gsfc.nasa.gov/stories/humidity_20040315
    /index.html
  • http//msis.jsc.nasa.gov/sections/section05.htm
  • http//science.hq.nasa.gov/missions/satellite_25.h
    tm
  • http//aqua.gsfc.nasa.gov/
  • http//earthobservatory.nasa.gov/
  • http//www.nasa.gov/home/hqnews/2003/dec/HQ_03394_
    water_map.html
  • http//www.nasa.gov/home/hqnews/2004/mar/HQ_04090_
    satellite_finds_warming.html

16
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