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Proposal Team 8: Grant Fritz, Jessica Brown, Stephanie Jalovec, Jennifer McGraw, Brian Roth, Evan Townsend
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Mission Overview The purpose of this mission is to capture stabilized video of the sky at ~80,000ft To provide an inexpensive and effective method of astronomical imaging using a CCD video camera and look for images of stars as they immerge in higher altitudes.
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Mission Overview The plan is to prove that images of the stars can be captured at high altitudes to further develop the idea that a telescope can be used on a balloon satellite platform. A high altitude platform would be less expensive than an Smaller telescopes can be used to get good images with an affordable method of observation, more people will be able to have access to space imaging. Don’t have to worry about clouds, which can often prevent astronomers on earth from observing. Can be serviced between each launch
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Design Structure is a dodecahedron
Mounted CCD camera, angled towards the stars Mounted digital camera angled downwards toward the earth HOBO data logger to measure ambient temperature of the craft and the exterior of the craft Heater to keep all electronics warm and running
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Dodecahedron Our structure is a dodecahedron instead of the basic six sided cube, making it less susceptible to impacts and allowing for a greater volume on the interior. However, the primary reason we decided on a dodecahedron is because of its faceted sides which would allow for our CCD Camera to be angled towards the stars.
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Hardware 1500 cm2 Foam Core 1 Digital HP Photosmart E427 camera
1 GB Memory chip 1 Timing circuit kit 1 HOBO data logger 1 Heater kits 3 Switches 12 9Volt Batteries 12 12V Batteries 1 Roll of aluminum tape 1 Roll of Electrical tape 1 CCD camera 1 CCD camera lens 1 Data storage unit 1 Battery pack 1 PVC tube 1 Hot glue and glue gun
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Model
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Functional Diagram
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Management Monday Tuesday Wednesday Thursday Friday Saturday Sunday
Week 1: Sept Group Meeting: Finish RFP RFP and CoDR slides DUE Week 2: Sept Design Doc. Rev A (prototyping design) Design Doc Rev A Order all hardware Week 3: Oct. 1-7 Design Doc Rev A DUE Design Doc Rev B & CDR slides Build prototype & start building final satellite Week 4: Oct. 8-14 CDR slides & Design Doc. Rev B DUE Drop, Whip & Tests Subsystem Functional and Mission Sim Tests Week 5: 15-21 Cold Test Week 6: 22-28 Alter designs if problems in the tests Acquire all hardware Additional Testing if there is problems Design Doc. Rev C Week 7: Oct. 29- Nov. 4 Alter design Design Doc. Rev C & Testing Final Design Complete design, build satellite & functional test Week 8: Nov. 5-11 Fix any problems with satellite, Rev C LRR Meeting & Design Doc. Rev C DUE LAUNCH Be there at 5:00AM! Week 9: Nov Design Doc. Rev D Week 10 Nov Design Doc. Rev D DUE Week 11 Nov.26- Dec. 2 Final Presentation Week 12 Dec. 3-9 Final Presentation due
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Management Grant Jessica Stephanie Jennifer Brian Evan Week 1:
Sept RFP- (Research) RFP RFP- (budget) RFP- (schedule) RFP- (systems) RFP- (design) Week 2: Sept Design Doc. Rev A (Require-ments) Design Doc. Rev A (Budget) & Start Ordering hardware Design Doc. Rev A (Mission Overview) Design Doc. Rev A (Schedule & Org Chart) (Design & Budget) Design Doc. Rev A (Design) Week 3: Oct. 1-7 Design Doc Rev B (Test plan) Start building Design Doc Rev B & CDR slides Design Doc Rev B (require-ments) (require-ments) (expected results) Design Doc Rev B & CDR slides Week 4: Oct 8-14 Build & Drop and Mission Sim tests & alter design if problems Whip and Subsystem tests Whip and Subsystem Tests Whip and Functional Tests Whip and Functional Test Week 5: Oct Cold Test & alter design & alter design & acquire all hardware Week 6: Oct Additional testing & Design Doc. Rev C (Launch Plan) Additional testing & Design Doc. Rev C (Expected Results) Additional testing & Design Doc. Rev C (Recovery plan) Additional testing & Design Doc. Rev C (Test Results) Additional testing & Design Doc. Rev C (Final Parts List) Week 7: Oct. 29- Nov. 4 Test and Complete Final Design & build satellite Week 8: Nov. 5-11 Prepare for Launch! Prepare for Launch! Week 9: Nov Design Doc. Rev D (Ready for Flight) Design Doc. Rev D (Lessons Learned) Design Doc. Rev D (Message to Next Semester) Design Doc. Rev D (Results and Analysis) Design Doc. Rev D (Launch and Recovery) Week 10: Nov & Final Presenta-tion Week 11: Nov. 26- Dec. 2 Final Presenta-tion (RFP Compliance) & movie? (Design Overview) (Expected Results) (Test results) Final Presenta-tion (Design Overview) Week 12: Dec. 3-9 Present Final
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$Budget$ 1500 cm2 Foam Core $5 (provided)
1 Digital HP Photosmart E427 camera $99.99 (provided) 1 GB Memory chip $27.99 (provided) 1 Timing circuit kit $12.50 (provided) 1 HOBO data logger $49.99 (provided) 1 Heater kits $5 (provided) 5 Switches $1 each (2 provided) 12 9Volt Batteries $2 each 12 12V Batteries $2.99 each 1 Roll of aluminum tape $25 (provided) 1 Roll of Electrical tape $4 (provided) 1 CCD camera $ (provided) 1 Data storage unit $378.93(provided) 1 PVC tube $0.50 1 Hot glue and glue gun $8 (provided) Total: $63.5
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Mass Budget Heater- 172.4 grams HP Photosmart Camera- 224.8 grams
Foam Core grams HOBO Data Logger grams Extra supplies (duct tape, hot glue, etc.) grams PVC tube grams Recorder grams 12 V batteries for camera grams Total: grams
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