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Echo Final Presentation. Andrew Berg, Shawn Carroll, Cody Humbargar, Jade Nelson, Jared Russell, Austin Williamson 12-05-06. Mission Overview. Main Science Mission- Test the effect of air pressure on sound waves. Compare sounding data to EOSS pressure data. Secondary Science Mission- - PowerPoint PPT Presentation
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Echo Final Presentation
Andrew Berg, Shawn Carroll, Cody Humbargar, Jade Nelson, Jared Russell, Austin Williamson
12-05-06
Mission Overview
Main Science Mission-
• Test the effect of air pressure on sound waves.
• Compare sounding data to EOSS pressure data.
Secondary Science Mission-
• HOBO data logger used to measure internal and external temperature during flight
• HOBO also used to test humidity levels inside balloon-satellite.
Non-Science Mission-
• Using main imaging hardware to take photographs during flight.
• Secondary imaging hardware will using ultraviolet / infrared filters to take photographs.
Design
• Balloon satellite measuring 150mm x 145mm x 100mm.
• Cameras face same direction
-Primary ELF
-Secondary 35mm IR Photography
• Main science system will be shock mounted
• Compact internal arrangement
• Atmospheric venting through desiccant
Science Signal Flow
HOBO
Rectifier/Limiter
Microphone
Driver
Oscillator
Design Pictures
RFP Satisfaction
Payload will be ready to fly by the end of the week
Mass and financial budget were not exceeded
Other RFP requirements met
Results and Analysis
•Expected Results–Linear correlation–Possible correlation with temperature
•Data Analysis–EOSS Pressure Data–Derived pressure based on altitude (General Case)–Running average of voltage data
Voltage vs. Time
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7:17:41 AM7:22:41 AM7:27:41 AM7:32:41 AM7:37:41 AM7:42:41 AM7:47:41 AM7:52:41 AM7:57:41 AM8:02:41 AM8:07:41 AM8:12:41 AM8:17:41 AM8:22:41 AM8:27:41 AM8:32:41 AM8:37:41 AM8:42:41 AM8:47:41 AM8:52:41 AM8:57:41 AM9:02:41 AM9:07:41 AM9:12:41 AM9:17:41 AM9:22:41 AM9:27:41 AM9:32:41 AM9:37:41 AM9:42:41 AM9:47:41 AM9:52:41 AM9:57:41 AM10:02:41 AM10:07:41 AM10:12:41 AM10:17:41 AM10:22:41 AM10:27:41 AM10:32:41 AMTime (H/M/S)
Voltage (V)
Pressure and Altitude
y = 1070.1e -4E-05x
R2 = 0.9989
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Altitude (feet)
Pressure (millibars)
Alt V. Pressure
Expon. (Alt V. Pressure)
Barometric Pressure Vs. Voltage
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7:25:477:29:477:33:477:37:477:41:477:45:477:49:477:53:477:57:478:01:478:05:478:09:478:13:478:17:478:21:478:25:478:29:478:33:478:37:478:41:478:45:478:49:478:53:478:57:479:01:479:05:479:09:479:13:479:17:479:21:479:25:479:29:479:33:479:37:479:41:479:45:479:49:479:53:479:57:4710:01:4710:05:4710:09:4710:13:4710:17:4710:21:4710:25:4710:29:4710:33:47
Time
Pressure (millibars)
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Average Voltage
Barometric PressureVoltage
Data Conclusions
•Definite Correlation, but not linear as expected.
•More trials (launches) are needed to reach more specific conclusions.
-Data could be inaccurate due to equalization lag
-Need accurate pressure sensor
•Sources of error
-Equalization lag
-Pressure sensor accuracy
Altitude and pressure
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7:25:477:31:177:36:477:42:177:47:477:53:177:58:478:04:178:09:478:15:178:20:478:26:178:31:478:37:178:42:478:48:178:53:478:59:179:04:479:10:179:15:479:21:179:26:479:32:179:37:479:43:179:48:479:54:179:59:4710:05:1710:10:4710:16:1710:21:4710:27:1710:32:47Time
Altitude
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Pressure (millibars)
Altitude
Pressure
Ascent
y = 2E-09x3 - 4E-06x2 + 0.003x - 0.1867
R2 = 0.934
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Pressure
Voltage
Flight Statistics
•Max ascent rate: 1501.313 ft/min
•Max descent rate: 9944.23 ft/min
•Launch: 7:28:47 11/11/2006
•Landing: 9:54:17 11/11/2006
•Max altitude: 98832.02 ft at 9:23:17
Ready To Fly Again
Final preflight too complicated
-Camera power on main switch
-Resolve film issues
Camera failure due to battery enclosure
-Fixed battery enclosure
-Could switch timer relay to DPST
Low peak voltage at sensor
-Modified sound tube
Sound Experiment
Experiment As Flown Modified Experiment
Round Two Pre-Flight
Store the payload,closed, in a cool, dry place
•Replace Consumables
-Modify IR film canister
-Clean IR filter
•Activation
-Power on cameras
-Set flash
-Activate timing circuit
Conclusions
• The correlation between sound transmission and pressure could be linear, but additional flights are needed for surety.
• Given the data, sound does not conduct as well at higher altitudes compared to lower altitudes.
Lessons Learned
All parts of the craft need equal attention
Activation should not require the craft to be open
Tape is ineffective in near-space
Message To Next Semester
Don’t be afraid to ask for help
Take your problems one at a time
Keep your experiment simple, but try something challenging
Test thoroughly
Leave plenty of time for problems