2006-2007 - Kennedy Space Center Technology Transfer Office

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Contents (continued)Range Technologies............................................................................................................ 51Hail Size Distribution Mapping............................................................................................................................................... 52Launch Pad 39 Hail Monitor Array System............................................................................................................................. 54Autonomous Flight Safety System – Phase III.......................................................................................................................... 56The Photogrammetry Cube...................................................................................................................................................... 58Bird Vision System.................................................................................................................................................................. 60Automating Range Surveillance Through Radio Interferometry and Field Strength Mapping Techniques................................ 62Next-Generation Telemetry Workstation................................................................................................................................. 64GPS Metric Tracking Unit....................................................................................................................................................... 66Space-Based Range................................................................................................................................................................... 68Fluid System Technologies................................................................................................. 71Calibrating the Helium Pressurization System for the Space Shuttle Liquid-Hydrogen Tank.................................................... 72Composite Materials for Low-Temperature Applications * 2006 .................................................................................................. 74Mitigating Problems in Measuring Hypergolic Fuels................................................................................................................ 76Cryogenic Moisture Analysis of Spray-On Foam Insulation (SOFI)......................................................................................... 78Thermal Performance of Aged and Weathered Spray-On Foam Insulation (SOFI)Materials Under Cryogenic Vacuum Conditions (Cryostat-4).................................................................................................. 80Automated Method for Estimating Nutation Time Constant Model Parameters for Spacecraft Spinning on Axis.................... 82Parameter Estimation of Lateral Spacecraft Fuel Slosh.............................................................................................................. 84Modeling of Slosh Dynamics in Cryogenic Propellant Tanks in Microgravity Environments................................................... 86Biological Sciences............................................................................................................. 89Countermeasure for Radiation Protection and Repair.............................................................................................................. 90Focused Metabolite Profiling for Dissecting Cellular and Molecular Processesof Living Organisms in Space Environments * 2006 .................................................................................................................... 92* 2006, 2007 Center Director’s Discretionary Fund Projectiv KSC Technology Development and Application 2006-2007
Contents (continued)Process and Human Factors Engineering Technologies................................................. 95Distributed Observer Network................................................................................................................................................. 96Influence Map Methodology for Evaluating Systemic Safety Issues.......................................................................................... 98Simulation and Analysis of Launch Teams (SALT)................................................................................................................. 100Solid-State Lighting Module (SSLM)..................................................................................................................................... 102Systems Maintenance Automated Repair Tasks (SMART)..................................................................................................... 104Launch and Landing Effects Ground Operations (LLEGO) Model....................................................................................... 106Exploration Supply Chain Simulation.................................................................................................................................... 107Command, Control, and Monitoring Technologies......................................................... 109Nanosensors for Evaluating Hazardous Environments........................................................................................................... 110Sixty-four–Channel Inline Cable Tester................................................................................................................................. 112Wireless Inclinometer Calibration System.............................................................................................................................. 114Generating Safety-Critical PLC Code From a High-Level Application Software Specification................................................ 116Spacecraft Electrostatic Radiation Shielding........................................................................................................................... 118Ion Beam Propulsion Study................................................................................................................................................... 120RT-MATRIX: Measuring Total Organic Carbon by Photocatalytic Oxidation of Volatile Organic Compounds.................... 122Appendix A: KSC High-Priority Technology Needs........................................................ 125Appendix B: Innovative Partnership Program................................................................ 129Appendix C: Export Control and Interagency Liaison Division..................................... 135KSC Technology Development and Application 2006-2007v/vi
Page 5 and 6: ForewordSuccessful technology devel
Page 7: ContentsSpaceport Structures and Ma
Page 11 and 12: IntroductionJohn F. Kennedy Space C
Page 13 and 14: Constellation SystemsSurfaceSystems
Page 15 and 16: Spaceport Structures and MaterialsK
Page 17 and 18: 20181614∆ E1210Modified Sensor Be
Page 19 and 20: Initial results of the EDEM model o
Page 21 and 22: Contacts: Dr. Carlos I. Calle ,NASA
Page 23 and 24: Close examination of the corrosions
Page 25 and 26: Adhesion at Failure (psi)2500200015
Page 27 and 28: Figure 1. After 500 hours of salt f
Page 29 and 30: Contacts: Dr. Paul E. Hintze , NASA
Page 31 and 32: Figure 2. Repairs to various types
Page 33 and 34: on top of the cuvette contains the
Page 35 and 36: Figure 2. A corrugated NiTi sheet e
Page 37 and 38: The PLTD can be used to (1) calibra
Page 39 and 40: SEM images of neat MWNT fibers: (a)
Page 41 and 42: Contacts: Trent M. Smith
Page 43 and 44: Figure 1. An isometric cutaway view
Page 45 and 46: Figure 2. Quartz sand flowing in th
Page 47 and 48: Figure 2. Top images show how the e
Page 49 and 50: Sand volume fraction contour at t =
Page 51 and 52: Integrated LWRD/RVC engineering bre
Page 53 and 54: Mean relative percentage change in
Page 55 and 56: We compared the model’s predictio
Page 57 and 58: Figure 2. Three-dimensional simulat
Page 59 and 60:
Figure 3. Camera calibration model.
Page 61 and 62:
The sketch in Figure 2 shows alaunc
Page 63:
Figure 2. Signal generator (right)
Page 66 and 67:
Hail Size Distribution MappingA 3-D
Page 68 and 69:
Launch Pad 39 Hail Monitor Array Sy
Page 70 and 71:
Autonomous Flight Safety System - P
Page 72 and 73:
The Photogrammetry CubeSpaceport/Ra
Page 74 and 75:
Bird Vision SystemThe Bird Vision s
Page 76 and 77:
Automating Range Surveillance Throu
Page 78 and 79:
Next-Generation Telemetry Workstati
Page 80 and 81:
GPS Metric Tracking UnitAs Global P
Page 82 and 83:
Space-Based RangeSpace-Based Range
Page 85 and 86:
Fluid System TechnologiesKSC Techno
Page 87 and 88:
0.900.850.80Discharge Coefficient,
Page 89 and 90:
Composite seals for performance eva
Page 91 and 92:
140000120000100000Signal80000600004
Page 93 and 94:
Contacts: Dr. Barry J. Meneghelli ,
Page 95 and 96:
60555045Comparative k-value (mW/m-K
Page 97 and 98:
a compatible spacecraft model where
Page 99 and 100:
In an ongoing effort for improvemen
Page 101:
Low-gravity probe prototype test.th
Page 104 and 105:
Countermeasure for Radiation Protec
Page 106 and 107:
Focused Metabolite Profiling for Di
Page 109 and 110:
Process and Human FactorsEngineerin
Page 111 and 112:
DON uses game technology to enable
Page 113 and 114:
Type of mobile crane that impacted
Page 115 and 116:
SALT proof-of-concept communication
Page 117 and 118:
SSLM CAD model.Our design offers th
Page 119 and 120:
Variables that can be integrated by
Page 121:
Exploration Supply Chain Simulation
Page 124 and 125:
Nanosensors for Evaluating Hazardou
Page 126 and 127:
Sixty-four-Channel Inline Cable Tes
Page 128 and 129:
Wireless Inclinometer Calibration S
Page 130 and 131:
Generating Safety-Critical PLC Code
Page 132 and 133:
Spacecraft Electrostatic Radiation
Page 134 and 135:
Ion Beam Propulsion StudySpacecraft
Page 136 and 137:
RT-MATRIX: Measuring Total Organic
Page 139 and 140:
Appendix AKSC High-Priority Technol
Page 141 and 142:
Risk Assessment ToolMission Data Fe
Page 143 and 144:
Appendix BInnovative Partnership Pr
Page 145 and 146:
system for the Government, using th
Page 147:
tracking objects after launch, and
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2006-2007 - Kennedy Space Center Technology Transfer Office

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