1 Thermal Investigation for Accurate Temperature Measurement Team TCTJ Truc Le Cedric Toguem Jonathan Newman
Feb 14, 2016
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Thermal Investigation for Accurate Temperature Measurement
Team TCTJTruc Le
Cedric ToguemJonathan Newman
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Overview•Mission Goal•Objectives•Science Background•Technical Background •Payload Design
• Electrical• Software
• Mechanical•Payload Development
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Mission GoalThe goal is to determine why previous LaACES payloads failed to correctly measure temperature in comparison to NOAA.
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ObjectivesDetermine the effect of the thermal boundary layer on temperature measurementsDetermine the effects of material and coating of temperature sensors on temperature measurementHave the measurements of the control temperature sensor be similar to NOAA measurements
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Temperature change in the Atmosphere
• Troposphere (0 to 12km) : lowermost atmosphere where temperature decreases from 30 to -80°C• Stratosphere (12 to 48km): second lowermost part of the atmosphere where temperature increases from -80 to 0°C
http://apollo.lsc.vsc.edu/classes/met130/notes/chapter1/vert_temp_all.html
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Boundary LayerThin layer of fluid in contact with a solid
body that flows more slowly than the rest of the fluid
As the payload gains altitude in fluid air, the boundary layer around it will be affected by heat transfer processes
http://apollo.lsc.vsc.edu/classes/met130/notes/chapter1/vert_temp_all.html
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Heat Transfer ModesHeat can be transferred in three
different ways:- Conduction- Convection- Radiation
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RadiationElectromagnetic radiation emitted from the
surface of an object in the form of heat due to the objects temperature
If an object is warmer than its surrounding environment, it will emit more radiation in the form of heat into the surrounding environment than it will absorb in order to attain thermal equilibrium
http://www.tsc.com/irgen/Image7.gif
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Test 1: Radiation Test 1Radiation test:
Sun →Electromagnetic radiation → Space →Sensors
The test will consist of different color shielding to reflect the electromagnetic radiation from the sun
http://image.tutorvista.com/content/dispersion
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Test 2: Radiation Test 2Radiation Test:The payload circuitry will emit radiation
to the sensor.Distance from the radiation source will
determine the amount of heat dissipated
http://images.google.com/imgres?imgurl=http://www.uos.harvard.edu/images/ehs/radiation
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Test 3: Boundary Layer Test
Sensors are placed at different distance from the exterior surface of the payload
Determine how much effect the boundary layer has on the measured temperature
http://www.google.com/imgres?imgurl=http://www.engineering.leeds
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Sensors7 temperature sensorsModel: 44003RC Precision Epoxy NTC Thermistor -80 °C to 50 ° C 1kΩat 25 ° C
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Sensors 1µA constant current from LM134Output voltage will then vary from
1mV to 190.8mV (Value based on device’s datasheet – Resistance V. Temperature Table)
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Sensor InterfacingSensors’ output voltage will vary
from 1mV to 190.8 mV
Payload ADC, from 0 to 3V
Will use AD820 op-amp to amplify each sensors’ output
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Sensor Interface
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Sensor Interface
Vref = 1V, R6 = 1kΩR4 = 0.94MΩR5 = 14.806kΩ
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Control Electronics
Program from Basic Stamp
Editor
Basic Stamp
Sensors Op-Amp ADC EEPROM
Control Electronics
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Power Supply6 x 1.5V Energizer L92 Ultimate
Lithium (AAA)9V to BalloonSat 9V to Op-Amps pin 7 1V from BalloonSat’s Voltage
regulator to Op-Amp Vref9V Current sources positive
voltage terminal
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Power Supply
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Power budget
Component Current (mA) Duration CapacityBalloonSat 51 (measured) 4 204mA-hThermistors (x7)
≤ 0.7 (desired) 4 2.8mA-h
AD820 op-amp (x7)
≤ 25 E-9 4 0.001mA-h
LM134 ≤0.7 (desired) 4 2.8mA-hMax Total 53.4 4 213.6mA-h
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Data Format TableDescription ByteExtra variables 2Time-Hour 1Time-Minute 1Time-Seconds 1Sensor-Inside wall 1Sensor-Outside wall 1Sensor-Control sensor 1Sensor-Inside B.L. 1Sensor-Outside B.L. 1Sensor-Black coating 1Sensor-White coating 1Total per Loop 12Total Estimated Bytes 2880 bytes
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Flight and Post-Flight Software
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Programming Flow Chart
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Flow Chart During Flight
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Exterior Mechanical Design
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Interior Mechanical Design
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Weight BudgetComponent Weight (g)Batteries ~91BalloonSat 60.4Op amp Board ~30.2Foamular structure 64.1BalloonSat/Op-amp board attachments ~9
Wiring ~10Booms (Plexiglas Straws) ~20Boom attachments ~25Sensors ~1.5Total ~311.2
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Payload Development PlanMechanical
Thermal TestingBoom TestingAttachment prototypingImpact test to find best design to
store componentsMaintain payload within regulation
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Payload Development PlanElectrical
Design the circuitry of the systemDetermine how well the components
will function in flight climateDetermine methods of calibration of
the sensors
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Payload Development PlanSoftware
Determine if extra memory will be needed and how to access it
Determine how to access ADC Determine methods of calibration
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Reference1. Clavius: Environment - heat transfer.
http://www.xmission.com/~jwindley/heatxfer.html. November 24, 2009
2. Anne E. Egger "Earth's Atmosphere: Composition and Structure," Visionlearning Vol. EAS 2003. http://www.visionlearning.com/library/module_viewer.php?mid=107
3. Sad Dr Rodrigue – Introduction to physical Geaography. http://www.csulb.edu/~rodrigue/geog140/lectures/thermalstructure.html
4. BASIC Stamp 2p 24-Pin Module. http://www.parallax.com/Store/Microcontrollers/BASICStampModules/tabid/134/ProductID/7/List/1/Default.aspx?SortField=UnitCost,ProductName. November 25, 2009
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Questions?