rocksat-c 2011 codr harding flying bison rocksat-c team conceptual design review harding university...
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RockSat-C 2011
CoDR
Harding Flying Bison ROCKSAT-C Team
Conceptual Design Review
Harding UniversityEd Wilson, Mentor, Will Waldron, Student 2,
Student 33 Oct 2011
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RockSat-C 2011
CoDR
1. Mission Overview – Mission Statement
Design, build, test and fly a spectrometer that will measure transmission spectra of gases in Earth’s atmosphere at lower altitudes and the Sun’s irradiance at higher altitudes
Interpret these spectra and compare them with previously published spectra
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RockSat-C 2011
CoDR
1. Mission Statement – Science Questions
1. Can we determine the temperature, pressure and number density of the gases measured as a function of altitude?
2. What gases can be identified in the atmosphere in the region of the flight trajectory?
3. What molecules can be identified in the Solar Spectrum at higher altitudes?
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RockSat-C 2011
CoDR
1. Mission Overview – Theory
Sunlight can be used as the optical light source in obtaining transmission spectra of Earth’s atmosphere
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SunAtmospheric GasesSpectrometerComputer withData Storage
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RockSat-C 2011
CoDR
1. Mission Overview -- Theory
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is the intensity of radiation of frequency,
is the intensity of radiation incident on the sample
, after
passing through the sample
is the absorption cross section at frequency,
N is the number of absorbing molecules per unit volume
L is the path length of the sample
The transmittance of light through a sample obeys the Beer-Lambert Law
RockSat-C 2011
CoDR
1. Mission Overview – Mission Requirements
Optical port on rocket through which spectra can be obtained
Sensitive spectrometer with computer interfacing capabilities equipped with light gathering fiber optic cable and lens
Embedded computer to operate the instrument and store the data
Software to control the measurement and data storage Adequate electrical power to operate instrumentation and
computer
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RockSat-C 2011
CoDR
1. Mission Overview – Operations
Design payload using SolidWorks
Choose embedded computer
Design and build electronicsg-switch with circuitpower distribution systemsignal conditioning circuitphotodetector feedback circuit
Interface computer with spectrometer
Carry out machining to construct payload chassis
Integrate payload with ROCKSAT-C canister
Carry out exhaustive testing
Integrate ROCKSAT-C canister with NASA rocket vehicle
Launch rocket and recover payload
Interpret data and report results
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RockSat-C 2011
CoDR
ConOps
t ≈ 1.3 min
Altitude: 75 km
t ≈ 15 min
Splash Down
t ≈ 1.7 min
Altitude: 95 km
-G switch triggered
-All systems on
-Begin data collection
t = 0 min
t ≈ 4.0 min
Altitude: 95 km
Apogee
t ≈ 2.8 min
Altitude: ≈115 km
End of Orion Burn
t ≈ 0.6 min
Altitude: 52 km
t ≈ 4.5 min
Altitude: 75 km
Altitude
t ≈ 5.5 min
Chute Deploys
We will take data beginning at launch and lasting for 15 minutes
RockSat-C 2011
CoDR
1. Mission Overview – Expected Results
1. Recover payload, dry and intact, after splashdown2. Download meaningful data from the instrument3. Identify several gases by their spectra and plot their
altitude versus abundance profileoxygenwater vaporozone
4. Fit the lineshapes of the spectra to mathematical models to determine Doppler and pressure broadening
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RockSat-C 2011
CoDR
2. Design Overview – RockSat-C 2011 User’s Guide Compliance
Careful attention will be paid to the center of gravity, weight
requirements and electrical regulations as detailed in the RockSat 2012 Payload Canister User’s Guide
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RockSat-C 2011
CoDR
2. Design Overview – Shared Can Logistics
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We are looking for a partner – we prefer the top 4.5 inches ofthe canister but can locate in the bottom half of the canister as well.
We will need clear access to the optical port on the rocket shell
RockSat-C 2011
CoDR
3. Management – Team Organization
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Team Organization
Harding Flying Bison Rocket Team will consist of one faculty mentor,three undergraduate science or engineering students and one technician
The students will participate in all aspects of the project in order for them to gain valuable experience working through a complete engineering project.
RockSat-C 2011
CoDR
3. Management – Schedule
Schedule
9/9/11 Deadline to submit Intent to Fly Form9/14/11 Initial Down Selections Made10/3/11 Conceptual Design Review (CoDR) Due10/4/11 Conceptual Design Review (CoDR) Teleconference10/17/11 Earnest Payment of $1,000 Due10/17/11 Online Progress Report 1 Due10/26/11 Preliminary Design Review (PDR) Due10/27/11 Preliminary Design Review (PDR) Teleconference11/14/11 Online Progress Report 2 Due11/30/11 Critical Design Review (CDR) Due12/1/11 Critical Design Review (CDR) Teleconference1/9/12 Final Down Select - Flights Awarded
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RockSat-C 2011
CoDR
3. Management – Budget
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Item Amount Total
Canister & FeeS 7000 7000
Travel & lodging for launch week 1800/person 7200
Student Fellowship 8 weeks at 40 hr/wk
4000/student 12000
Materials & Components 1500 1500
Total $27,700
RockSat-C 2011
CoDR
3. Mentors – Faculty and Industry
Dr. Edmond Wilson, Professor of Chemistry at Harding University will be the team mentor. He has had one year of previous experience with ROCKSAT-C in addition to attending an earlier RockOn workshop.
Aerospace companies in Camden, AR will be solicited for mentoring and for financial support of this project.
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RockSat-C 2011
CoDR
4. Conclusions
The mission goal is to measure the transmission spectra of gases in Earth’s atmosphere at lower altitudes and the Sun’s irradiance at higher altitudes.
The results will aid in moving forward another project whose goal is to place a spectrometer onboard a robotic rover on the surface of Mars. The Earth’s atmosphere at higher altitudes has the same densities, pressures and temperatures as that on Mars.
The main challenges are to design a robust, sensitive feedback circuit to adjust the light entering the spectrometer to the optimum level so that no data is lost due to too much or too little light.
The toughest challenge is to find funding to be able to carry out this project to a successful conclusion.
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