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Chelsea Welch Beth Moger Colin Nugen Anthony Cangelosi Tully Baetz Charles Hartman December 1, 2009

Chelsea Welch Beth Moger Colin Nugen Anthony Cangelosi Tully Baetz Charles Hartman December 1, 2009

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Page 1: Chelsea Welch Beth Moger Colin Nugen Anthony Cangelosi Tully Baetz Charles Hartman December 1, 2009

Chelsea WelchBeth MogerColin Nugen

Anthony CangelosiTully Baetz

Charles Hartman

December 1, 2009

Page 2: Chelsea Welch Beth Moger Colin Nugen Anthony Cangelosi Tully Baetz Charles Hartman December 1, 2009

Mission OverviewMission Statement:

The BalloonSat will ascend to an altitude of 30 km carrying a Geiger counter that will detect the amount of radiation in the lower atmosphere as a function of altitude.

What we expect to discover:We expect to discover a significant rise in the amount of beta particles and gamma rays detected within the ozone layer and at the peak of the flight of the BalloonSat, and a significant decrease in particles detected below the ozone layer where most of the harmful radiation has been filtered out.

Page 3: Chelsea Welch Beth Moger Colin Nugen Anthony Cangelosi Tully Baetz Charles Hartman December 1, 2009

•The BalloonSat, Big Bang, is a 16 cm foam core cube. Big Bang carries an AVR Microcontroller, Analog Geiger counter, heater, a HOBO datalogger and a digital Camera.

•The AVR Board and the Geiger counter are secured down with half inch plastic spacers, 1 inch long screws that penetrate through the box, and nuts on the outside. The camera, heater, and HOBO are secured down with industrial strength Velcro. There is insulation on the inside of the structure, and there is aluminum tape and hot glue that secures all of the sides together.

Design Overview

Page 4: Chelsea Welch Beth Moger Colin Nugen Anthony Cangelosi Tully Baetz Charles Hartman December 1, 2009

•The Geiger counter is interfaced with the AVR board via a three pronged header. The three pronged header is attached to 9V power in, ground and digital output on the Geiger counter. The header is integrated into the AVR by soldering the prongs onto the breadboard section. Each prong is bridged to a wire leading to 9V power out, ground and D2 input.

•The AVR is programmed to take data from each instrument every 234 milliseconds. The data from the Geiger counter is taken constantly via an interrupt that performs a counting experiment and empties the count into the AVR when it is called upon and then restarts the count..

Design Overview

Page 5: Chelsea Welch Beth Moger Colin Nugen Anthony Cangelosi Tully Baetz Charles Hartman December 1, 2009
Page 6: Chelsea Welch Beth Moger Colin Nugen Anthony Cangelosi Tully Baetz Charles Hartman December 1, 2009
Page 7: Chelsea Welch Beth Moger Colin Nugen Anthony Cangelosi Tully Baetz Charles Hartman December 1, 2009
Page 8: Chelsea Welch Beth Moger Colin Nugen Anthony Cangelosi Tully Baetz Charles Hartman December 1, 2009

The launch and recovery went according to plan. On November 7th, 2009, approximately 6:50 a.m. Our payload was launched via balloon with no abnormalities. All systems were go and armed prior to launch and then turned on before launch. After flight, the payload landed on a farm near the Colorado Wyoming border northwest of Windsor. Upon recovery, the payload was still counting data, taking pictures and with no electrical failures. The structure of the payload was normal with no scratches, dents, or any damage.

Launch Recap:

Page 9: Chelsea Welch Beth Moger Colin Nugen Anthony Cangelosi Tully Baetz Charles Hartman December 1, 2009

Results and AnalysisTeam Alpha made three predictions about the radiation environment at different altitudes before the flight.

Prediction 1: There would be a steep nonlinear increase in counts of radiation per every 234 milliseconds beginning at ground level that peaks at 15 km

Prediction 2: At 15 km, counts of radiation per every 234 milliseconds should occur 6 to 8 times the amount of counts at the starting elevation.

Prediction 3 and Main Mission Purpose: The amount of radiation would significantly increase once the satellite climbed into the ozone layer at 10 kilometers, indicating that the ozone layer is the main factor in filtering harmful radiation before it hits the ground.

Page 10: Chelsea Welch Beth Moger Colin Nugen Anthony Cangelosi Tully Baetz Charles Hartman December 1, 2009

Prediction 1: There would be a steep nonlinear increase in counts of radiation per every 234 milliseconds beginning at ground level that peaks at 15 km.

It is clear from these graphs that up until approximately 42 minutes, when the satellite had reached 15 km, there was a steep, nonlinear increase in counts of radiation per 234 milliseconds, which then remains constant past 15 km.

Page 11: Chelsea Welch Beth Moger Colin Nugen Anthony Cangelosi Tully Baetz Charles Hartman December 1, 2009

Prediction 2: At 15 km, counts of radiation per every 234 milliseconds should occur 6 to 8 times the amount of counts at the starting elevation.

This graph indicates that the amount of radiation counts does not increase as much as 6 to 8 times the amount at ground level, however, the amount of radiation counts does increase approximately 5 times the amount at ground level, still indicating a significant rise in radiation counts at 15 km compared to the amount on the ground.

Page 12: Chelsea Welch Beth Moger Colin Nugen Anthony Cangelosi Tully Baetz Charles Hartman December 1, 2009

Prediction 3 and Main Mission Purpose: The amount of radiation would significantly increase once the satellite climbed into the ozone layer at 10 kilometers, indicating that the ozone layer is the main factor in filtering harmful radiation before it hits the ground.

From the graph, it is clear that at approximately 10 km, the altitude at which the ozone layer begins, there is a significant increase in the amount of radiation counts, indicating that the ozone layer is our main protection against harmful radiation.

Page 13: Chelsea Welch Beth Moger Colin Nugen Anthony Cangelosi Tully Baetz Charles Hartman December 1, 2009

Main Conclusions:

Team Alpha was able to prove their main mission purpose. The amount of radiation that exists in the ozone layer is significantly higher than the amount of radiation below the ozone layer. This indicates that the ozone layer is our main protection from harmful radiation.

Because of this, we are now aware of how important the ozone layer is to our survival. These results prove that in order for life on earth to continue, the ozone layer must be protected from the pollution that damages it every day. They also prove the need for renewable energy resources are critical to the survival of the ozone layer.

Page 14: Chelsea Welch Beth Moger Colin Nugen Anthony Cangelosi Tully Baetz Charles Hartman December 1, 2009

Our best pictures:

Page 15: Chelsea Welch Beth Moger Colin Nugen Anthony Cangelosi Tully Baetz Charles Hartman December 1, 2009
Page 16: Chelsea Welch Beth Moger Colin Nugen Anthony Cangelosi Tully Baetz Charles Hartman December 1, 2009
Page 17: Chelsea Welch Beth Moger Colin Nugen Anthony Cangelosi Tully Baetz Charles Hartman December 1, 2009
Page 18: Chelsea Welch Beth Moger Colin Nugen Anthony Cangelosi Tully Baetz Charles Hartman December 1, 2009

Internal vs. External Temperature Graph:

Page 19: Chelsea Welch Beth Moger Colin Nugen Anthony Cangelosi Tully Baetz Charles Hartman December 1, 2009

Lessons LearnedThe importance of testing and making sure

every piece of our satellite works correctlyThe process that goes into designing,

building, testing, and launching a satelliteKnowing the pre-launch procedure, as well

as practicing it, is very importantDon’t make your experiment too complexUnderstanding this project overall from the

beginning

Page 20: Chelsea Welch Beth Moger Colin Nugen Anthony Cangelosi Tully Baetz Charles Hartman December 1, 2009

Ready to fly again Replace the batteriesIf storing for more than a week, disconnect or remove

the batteriesErase the AVR memory and Re-arm the payloadErase the pictures on the camera memory and relock

the memory card. Once the batteries are in place reseal the edges of the

cube Immediately prior to launch switch the switches on in

order (1 then 2 or Power then G switch)

Page 21: Chelsea Welch Beth Moger Colin Nugen Anthony Cangelosi Tully Baetz Charles Hartman December 1, 2009

Appendix: RFP RequirementRFP Requirement Compliance

Additional experiments, collection of data, analysis of data

Geiger counter, detecting and recording radiation, analysis with respect to altitude

Analog input not to exceed 5V Geiger counter data to be recorded from 0 to 5 Volts

Interface tube secured and not interfering with flight string

Plastic tube, anti-abrasion washers, and paperclips will be built into structure

Internal temperature remain above -10° C Heater shall regulate temperature

Weight not to exceed 850g Total weight is 844g (Not including HOBO)

Acquire ascent and descent rates of flight string Data found by pressure readings

Design allows for HOBO, external temperature cable, Camera, AVR Microcontroller, heater system, and batteries.

All are incorporated into the BalloonSat design.

BalloonSat shall be made of foam core Incorporated into the design

Part list and budget shall include spare partsAn extra sheet of foam core and an extra plastic tube has been included as well as excess glue, tape, and paper clips. The Geiger counter cannot be replaced.

BalloonSat shall have contact information and an American flag.

This will be incorporated into the design on the outside of the foam core once the satellite has been finished.

All units shall be in metric All units in all design documents are in metric.

No one shall get hurtAll safety procedures and instructions shall be followed.

Page 22: Chelsea Welch Beth Moger Colin Nugen Anthony Cangelosi Tully Baetz Charles Hartman December 1, 2009

Item Weight (grams)HOBO 30g (Not included in final weight budget)

Canon A570IS & 2 AA Batteries 220g

AVR & 2 x 9 Volt Lithium Batteries 150g

Heater & 3 x 9 Volt Alkaline Batteries 100g

Geiger Counter 75g

Plastic Tubing 15g

2 Washers 30g

2 Paperclips 5g

Foam core Structure 24g

Insulation 55g

Aluminum Tape 25g

Velcro 35g

Glue 60g

7 x ½ Inch Long Plastic Spacer 15g

7 x 1 Inch Long Bolt and Nut 20g

2 Switches 15g

Total = 844g

Mass Budget

Page 23: Chelsea Welch Beth Moger Colin Nugen Anthony Cangelosi Tully Baetz Charles Hartman December 1, 2009

ItemWhere Item Will be

Purchased/Ordered FromPrice (U.S. dollars)

Metal/Concrete Epoxy Home Depot $4.99

Dry Ice King Soopers $36.97

Industrial Velcro Home Depot $9.47

Foam Core King Soopers $22.50

9 Volt Alkaline 6 Pack Home Depot $10.97

Plastic Spacers Home Depot $2.24

Nuts and Bolts Home Depot $1.96

3 x 9 Volt 2 Pack Home Depot $14.97

9 Volt Lithium Flight Batteries Plus $7.29

Total = $111.36

Cost Budget

Page 24: Chelsea Welch Beth Moger Colin Nugen Anthony Cangelosi Tully Baetz Charles Hartman December 1, 2009

Message to Next SemesterDon’t underestimate the intensity of the work

you will be taking on, but also don’t be intimidated by the amount of work

Get to know your team. You will be spending a lot of time with them

Be careful with timeThis class may seem overwhelming, but

getting A’s and B’s is not difficultGive this class your all, and it will give back

to you