pCDR - Colorado Space Grant Consortium

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Transcript pCDR - Colorado Space Grant Consortium

Lucas Ibarra Alexis Sutker
Evan Long Jack Oblack
Jaevyn Faulk Dylan Anderson
Devon Connor Eric Hardwick
October 18, 2012

Develop a BalloonSat that will take UV data
and correlate it with NCAR data.
 Used to see changes in UV radiation from last UV
cycle


Prove that there has been an increase in solar
activity causing an increase in UVA and UVB
radiation hitting Earth.
Hypothesize that an increase in solar activity
results in an increase in UVA and UVB
radiation.
Requirement
number
Requirement
Where it comes
from
MS 0.1
The BalloonSat will be able to survive to
near space conditions.
Mission Statement
MS 0.2
The BalloonSat will collect
electromagnetic radiation at UVA and
UVB wavelengths as a function of
altitude.
Mission Statement
MS 0.3
The BalloonSat will measure internal and Mission Statement
external conditions.
MS 0.4
Compare Data with NCAR Data.
Mission Statement
MS 0.5
BalloonSat will take in-flight pictures
Mission Statement
MS 0.6
We will meet all the RFP requirements
Mission Statement
Requirement
number
Requirement
Where it
comes from
MS 1.1
Will fly six UVA sensors and two UVB
photodiodes.
MS 0.2 and
Ms 0.4
MS 1.2
The BalloonSat will be contained within a rigid,
insulated foam core structure.
MS 0.1 and
MS 0.6
MS 1.3
Arduino Uno will be programmed to record all
data to an SD card.
MS 0.4 and
MS 0.3
MS 1.4
BalloonSat will fly two cameras.
MS 0.5 and
MS 0.6
MS 1.5
Will fly pressure sensors, temperature sensors,
acceleration sensors, and humidity sensors.
MS 0.3
Functional
Block
Diagram
Diagram
Resistor
LED
Heater Block
Switch
9V Battery
Camera Battery
9V Battery
9V Battery
9V Battery
9V Battery
Manual
Toggle
Switch
Switch
GoPro Battery
Camera 1
(GoPro)
2GB SD Card
Arduino Uno
GoPro Memory
Accelerometer
2GB SD Card
Camera 2
(Canon A780)
Humidity Sensor
Temp Sensor
(Internal)
Altimeter
Pressure Sensor
UVA Sensors
(6)
Temp Sensor
(External)
UVB Photo Diode
UVA Sensors
GoPro Lens
GoPro HD Hero 3
Arduino Uno
Heater System
9v Batteries
Canon
Powershot
SD780IS
Item
Budget
Source
Item
Budget
Source
UVA Sensor
8 for $24
Sparkfun
SD Shield
provided
Chris
9 V Batteries
10 for $11.00
McGukins
Micro SD Card
provided
Chris
UVB Diode
2 for $100
Boston Electronics
Development Board
provided
Chris
Vibration Sensor
$3.00
Sparkfun
GoPro Hero 3
Donated
Canine Hardware
Foam Core
Provided
Chris
Arduino Uno
$30
Sparkfun
Canon Camera
Provided
Chris
SD Shield
$15
Sparkfun
Heater
Provided
Chris
Batteries
4 Provided
Chris
Aluminum Tape
Provided
Chris
Arduino Uno
Provided
Chris
Micro SD Card
$10
Sparkfun
Temperature sensor
Provided
Chris
Accelerometer
provided
Chris
Humidity Sensor
provided
Chris
Copper Wire
Provided
Chris
Pressure Sensor
provided
Chris
Insulation
Provided
Chris
Item
Weight
Remaining
Weight
Item
Weight
Remaining
Weight
Foam Core
25
1100
SD shield x2
29
611
Canon
200
900
Arduino x2
55
556
Heater
31
800
UVB Sensors x2
30
526
Batteries
233
700
UVA Sensors x6
0.6
525
Plastic Tube
30
770
Plastic Tube
20
505
Aluminum Tape
15
745
Vibration Sensor
5
500
GoPro
Development
board x2
74
671
Humidity Sensor
1
499
31
640
Pressure Sensor
1
498
Accelerometer
1
497
temp sensor
0.2
496.8
Total weight
628.2
496.8
Test Structure
Objective
Payload
Cooler, Payload active, Camera Test, Full
Functionality Test,
Structure
Impact Test, Whip Test
Sensors
UV sensors, Humidity, Temperature,
Pressure, Vibration, Acceleration
Test
Date
Test
Date
Test
Date
Cooler
11/01
Impact
11/01
Temperature 10/30
Payload Active
11/8
Whip
11/01
Pressure
10/25
Camera
10/22
UV sensors
10/30
Vibration
10/25
Full
Functionality
11/25
Humidity
10/30
Acceleration
10/25
Jack Oblack
Team Leader
Budget Management
Systems Support
Alexis Sutker
Test Lead
Eric Hardwick
Systems Lead
Budget Support
C&DH Support
Devon Connor
Software Lead
Dylan Anderson
Design Lead
Jaevyn Faulk
Science Lead
Test Support
Integration Support
Software Support
Evan Long
Integration Lead
Lucas Ibarra
C&DH Lead
Design Support
Science Support




UVA sensors will not be able to function
outside the box
Sensors will not function properly
Trouble communicating with NCAR contact
Programming will work properly




Our Satellite will be able to fly again after
impact
Our sensors will work properly
All systems will communicate and properly
connect to each other.
Data will show UV radiation has increased