Cosmic Sat University of Northern Colorado April 2
- Slides: 25
Cosmic. Sat University of Northern Colorado April 2, 2004
Cosmic. Sat Goals n Objective: Determine charged particle count with altitude using a coincidence count detector n NASA Benefits: Measure cosmic radiation in a Mars-like atmosphere using a small detector
Cosmic. Sat n System Requirements: n Detectors , coincidence counts circuit, housing, heating circuit and data storage. n Payload mass - ~ 2 kg n Atmospheric temperatures of ~ - 60 degrees F n Large atmospheric pressure differential n Coronal Discharge n Magnetic shielding n Crash survival
Cosmic. Sat: System Overview Scintillator PMT Coincidence Circuit Data Logger Batteries Scintillator Heater Circuit Batteries Switches
Subsystem: PMTs and Scintillator n Purpose: n Scintillator: n n n Interacts with charged particles Excites electrons between molecular bound states Electron de-exitation produces photons Photon travels along scintillator undergoing many total internal reflections Photomultiplier Tubes: n n Collect photons Converts photons to an electronic signal
PMTs and Scintillator n Photomultiplier Tube Module Interfaces: n n n Base encased with PMT High voltage source in base Requires an external 5 V power source Base interfaced with coincidence count circuit Optical grease between PMT face and scintillator Base PMT Head
Charged Particles PMTs and Scintillator Optical Grease PMT Scintillator Vacuum Epoxy n The PMTs bonded to scintillator n Organic Scintillator wrapped in Mylar foil and electrical tape n PMTs wired to coincidence circuit via BNCs
PMTs and Scintillator PVC n BNC Housing: n n n PMTs encased in PVC pipe – maintain atmospheric pressure PMT – scintillator joined with vacuum epoxy and then JB Weld. PVC capped and interfaced with BNCs for wires JB Weld Vacuum Epoxy Scintillator
Housing Prototype
System Stabilization Wood Frame n The two PVC pipes bonded with ABS “glue” n Adds support for all system components n Tether passes through brass tube in center n Each PMT - Scintillator combination slides into frame. Brass Tube
The Exterior Box Materials n Reflective Mylar n Insulation n Foam Core n Thermo. Sheild Paint n Aluminum tape n Epoxy
Coincidence Counting Circuit n Purpose: n To supply each PMT with 5 V n To time impulses from each PMT determine coincidences and n Send count impulses to data logger
Coincidence Timing Circuit Courtesy of Lawrence Berkeley National Laboratory
Circuit System Schematic n Interfaces: n Two PMT Modules n Two nine volt batteries in series n Madge. Tech Data Logger Circuit
Circuit: Start to Finish Courtesy of Lawrence Berkeley National Laboratory
Heater Circuit n Six Resistors – n n Resistors 3. 9 ohm each 5 Watts each n Three 9 Volt batteries in parallel n Keep payload interior > 5 C Batteries in parallel
Power Budget n 18 Volts to the Coincidence Count Circuit n n Power out – heater – 18 watts n n PMT modules High voltage source is housed within the PMT base 9 Volts to the heater circuit (three 9 V batteries in parallel) Current requirments: 1934 m. A n n n Heater - 1450 m. A Circuit – 224 m. A PMT modules – 80 m. A each
Data Collection § Purpose: § Collect electronic pulses from the circuit § Put a time stamp to each pulse
Data Collection Schematic Computer Post-Recovery Data Logger Circuit During Flight
Mass Budget : 3000 gm 2 Scintillator Panels Brass rod Box Frame 2 PMTs Pulse recorder Hobos Batteries Heater Circuit Cables, switches 415 grams 34 grams 600 grams 460 grams 26 grams 61 grams 191 grams 37 grams 145 grams 100 grams Total 2469 grams
Budget PMT Modules ~ 2300. 00 Madge. Tech Data Logger ~ 195. 00 Batteries ~ 100. 00 Box Materials ~ 100. 00 LX 200 ~ 250. 00 Geiger tube ~ 270. 00 Cables ~ 50. 00 Buffing Compound ~ 125. 00 Optical Grease ~ 75. 00 Electronic components ~ 50. 00 Total _____________________ ~3515. 00
Project Organization n Project Advisors: n Electronics: n n n Dr. Robert Walch Dr. Dick Dietz Dr. Cynthia Galovich Dr. Kendall Mallory n n Project Manager: n Data Collection & Heater: n n n Ryan Marshall PMT Module & Scintillator: n Pat Mills Julie Smith Anna Samsel System Housing & Stabilization: n Levi Ellis
Schedule n April 5 – 10: n n n April 11 – 16: n n n Individual component testing Construct the housing and frame Construct the detector Construct the Geiger tube – Palmtop detector Test the whole system Make any final adjustments April 17 : n Launch
Alternate Payload Geiger Tube – Palmtop Computer
Acknowledgements Dr. M. A. Duvernois Dr. James Connell Dr. Howard Matis Andrew Loomis Ken Cochran Kodak University of Minnisota University of New Hampshire Lawrence Berkeley National Laboratory UNC PMTs purchased with Electroptics Grant funds Many Thanks to: The Colorado Space Grant Consortium, NASA and JPL for giving us this wonderful opportunity The UNC Dept. of Physics faculty; without whom, none of this would be possible
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