NSBE - Winter 2009/2010 - 68

nSBE AEroSpAcE SyStEmS confErEncE prEviEw • LoS AngELES, cALif. • fEB. 5–10, 2010 nEw horizonS…nEw DEStinAtionS…nEw DiScovEriES ConferenCe SpeaKerS, continued hILdRETh wALKER Former Apollo Scientist • Panelist: Aerospace Pioneers Plenary Session • Developed laser range-finding experiment to measure distance from the Earth to the Moon JOSEph FuLLER JR. Founder, President and CEO, Futron Corporation • Panelist: Space/Astronautics Plenary Session • Design background includes Apollo, Space Shuttle and TIROS/NOAA teCHniCal paper abstraCts* * Submitted as of Sept. 21, 2009 1. ATHLETE Vehicle Tool Manipulation and Usage 2. Launching the Future Constellation Program at KSC 3. Aeroelastic Studies of a Rectangular Wing with a Hole: Correlation of Theory and Experiment 4. Human Factors Evaluations of Two-Dimensional Spacecraft Conceptual Layouts 5. Thermal Vacuum Testing: Test Preparation 6. Amateur Rockets: The Little Giants in the Aerospace 7. 8. 9. 10. 11. 12. 13. 14. 15. 16. 17. 18. 19. 20. 21. 22. 23. 24. 25. 26. Industry Overview of the FAA’s Space Traffic Management Program Vehicle Systems Management (VSM) Human Research Implications for Exploration on the Lunar and Martian Surfaces An Examination of the Design and Development of Environmental Systems in Spacecraft: The Space Shuttle Ground Station Selection Investigation for the HyspIRI Satellite Mission SPS-Eprime Abstract for 2010 NSBE Aerospace Systems Conference February 5-10, 2010 NSBESAT 1: System Engineering Overview Project Arusha Pressurized Rover Cabin Layout Arusha Pressurized Rover Displays, Controls, and Workstations Arusha Pressurized Rover Waste, Water, Hygiene, and Crew Accommodations Subsystems Arusha Pressurized Rover Lighting Low Fidelity Mockup of NSBE Arusha Pressurized Rover 3D Visualization for Phoenix Mars Lander Science Operations Rover Prototype for Mobile Surveying Technology Development Safety & Mission Assurance (S&MA) Verification of Flight Products Haptic Mobility Control for Teleoperated Rovers Concept for Constellation Program Certification of Flight Readiness (COFR) Using XML to Integrate VLJ Mechanical 3D CAD data into a visual repository of tessellated, articulated 3D geometry Transitioning for a Sustainable Future: A World View of Renewable Energy A Hybrid Neural Network Finite Element Scheme for Prediction of Crack Length and Orientation on Curved Plates Computational Approach for Design and Analysis of different Bullets under the Influence of Aerodynamic Coefficients An Entropy-Based Measure of Spacecraft Planned 29. 30. 31. Activity Complexity: Applied To Mars Exploration Rovers Surface Activities Enterprise Content Management At JSC Analysis of Spacecraft Macro Memory Usage on the New Horizons and the MESSENGER Space Programs Development of Automated Sample extraction and preparation system for geomicrobiology and Astrobiology in situ research applications Area and edge effects in radiometric forces 27. 32. 33. A Three Dimensional Computational Fluid Dynamics Navier Stokes study for an isolated high bypass ratio turbofan engine nacelle using tetrahedral, polyhedral hexahedral and hybrid mesh. 34. Statistical Modeling of Interactions between Gas Molecules and Pulsed Optical Lattices 35. The Gravity & Extreme Magnetism SMEX (GEMS) X-ray Polarimeter Instrument 36. Modular Open Systems Assessment of the B-52 Program: A Case Study 37. Results from the NASA Instrument Capability Study 38. Information Exchange in Multi-rover SLAM 39. An Introduction to Commercial Aerospace Public Safety: From the Inside Looking Out 40. Important Fundamentals and Astrophysical Observations found to be misapplied to Gravitational Lensing 41. Radiation Hardened SiGe-based Reconfigurable Current Sensor for Lunar Applications 42. A Holistic Approach to Managing Risk Factors Contributing to Falls in an Aerospace Environment 43. Functional Standardization of Avionics Interfaces 44. Line-shape Analysis of Spectral Distributions 45. Concept for an intelligent fault detection using Multiresolution Analysis 46. Lunar Regolith Control and Resource Utilization 47. Nano-Structured Propellants and Launch Systems 48. Aerodynamic Characterization of Scale Model Aircraft using 5 DOF Dynamic Test Rig 49. Too Much of a Good Thing: A Discussion of the excessive Advisories, Cautions, and Warnings in the E-2D Advanced Hawkeye 50. Use of NASA University Competitions as Augments to Curriculum 51. The Role of Aircraft Simulation in Improving Flight Safety in General Aviation 52. A Presentation of An Intelligent Integrated Vehicle Health Management Concept for Spacecraft Systems 53. Open-Source Simulation for Planetary Surface Robotics 54. IR LED Calibration Sources for Space Applications 28. 68 • career engineer • winter 2009 • www.nsbe.org

NSBE - Winter 2009/2010

Table of Contents for the Digital Edition of NSBE - Winter 2009/2010