|
CRICKETSAT and Beyond |
||
|
|
||
|
|
||
|
UVM and Milton High School students performed the design and
build work during this past year. |
||
![]() |
Profile of the Atmosphere
|
|
|
Flight Objectives: MHS-1 |
||
![]() |
● Fly three daytime flights - Temperature - Pressure (altitude) - Humidity ● Fly two nighttime flights - Temperature - Pressure (altitude) ● Improve upon previous best results - Reception range of 15 miles - Lowest temperature of +45 F - Altitude of ~11,000 feet |
|
|
MHS_1: Flight Results |
||
|
|
||
![]() ![]() |
||
|
First BalloonSat Flight MHS-2 |
||
|
● Teamwork: - Collaborative effort with Medgar Evers College (CUNY) Their CONDOR-2 BallonSat flight ● Objectives: - Collect real-time temperature measurements inside the CUNY flight bag containing the radio/GPS payload - Determine if temperature may be a factor with the loss of GPS tracking data - Determine if CricketSat system can coexist with a BalloonSat payload without causing radio interference |
|
|
|
|
||
|
MHS-2: Flight Results |
||
|
|
||
|
|
||
![]() ![]() |
||
|
Second Balloon Flight: MHS-3 |
||
|
● Objectives: |
||
|
Milton High School Design Task |
||
|
Problem |
||
![]() |
||
![]() |
||
![]()
This circuit uses a common BASIC Stamp II microcontroller
|
||
|
Software Development: Pseudo Code |
||
|
● Define and initialize variables ● LOOP : - For Sensor = 1 to 5 ● Turn CricketSat sensor on for 11 seconds, then off ● Flash the strobe light ● Wait 1/2 second - Next Sensor - If five minutes have elapsed ● Take a picture - Wait three seconds ● GOTO LOOP |
||
![]() |
||
|
Power Sequencing Controller |
||
|
|
||
|
MHS-3 Flight Results: Temperatures During Flight |
||
|
|
||
|
MHS-3 Flight Results: Temperature vs. Altitude |
||
|
|
||
|
MHS-3 Flight Results: Altimeter Correlation |
||
|
|
||
|
MHS-3 Flight Results |
||
|
|
||
![]() ![]() |
||
|
CricketSat / BalloonSat Compatibility Results |
||
● Validated methodology and effectiveness of time-based sequencing ● Temperature and altitude results correlated to known NOAA and GPS for most values ● Redesign work needed for both devices to meet full requirements ● Data reception range works well for 51 miles ● System does not appear to have any RF interference issues with the BalloonSat VHF transmitter |
||
|
Future Work |
||
|
● Improvements to CricketSat temperature and pressure sensors ● Fly the CricketSat Array System solo ● Low cost, expendable ● Alternative to BalloonSat ● Develop future system with Dr. Neal Brown ● BASIC Stamp based design ● Recoverable system with GPS onboard ● Multiple sensors / single transmitter ● Convert data to proper units onboard ● Transmit results in Morse Code |
||
|
Thanks!
|
||
|
|
||
|
|
||
|
|
||
|
Mapping (Click to enlarge) |
||
|
05 BaloonSAT Launch CricketSAT 04 CricketSAT Data CricketSAT History
|
||