Liquids

Propellant slosh loads, NASA SPACE VEHICLE DESIGN CRITERIA (Structures)

Fracture Control of Metallic Pressure Vessels, NASA SPACE VEHICLE DESIGN CRITERIA (Structures)

Prevention of Coupled Structure-Propulsion Instability (POGO), NASA SPACE VEHICLE DESIGN CRITERIA (S

Slosh Suppression NASA Space Vehicle Design Criteria, NASA SPACE VEHICLE DESIGN CRITERIA (Structures

Liquid rocket engine turbopump shafts and couplings, NASA SPACE VEHICLE DESIGN CRITERIA (Chemical)

Liquid rocket engine turbines, NASA SPACE VEHICLE DESIGN CRITERIA (Chemical)

Liquid Rocket Engine Turbopump Inducers, NASA SPACE VEHICLE DESIGN CRITERIA (Chemical Propulsion)

Liquid rocket metal tanks and tank components, NASA SPACE VEHICLE DESIGN CRITERIA (Chemical)

Liquid rocket valve components, NASA SPACE VEHICLE DESIGN CRITERIA (Chemical)

Liquid rocket engine centrifugal flow turbopumps, NASA SPACE VEHICLE DESIGN CRITERIA (Chemical)

Liguid rocket valve assemblies, NASA SPACE VEHICLE DESIGN CRITERIA (Chemical)

Liquid rocket pressure regulators, relief valves, hurst disks, and explosive valves, NASA SPACE VEHI

Liquid rocket disconnects, couplings, fittings, fixed joints, and seals, NASA SPACE VEHICLE DESIGN C

Liquid rocket engine turbopump gears, NASA SPACE VEHICLE DESIGN CRITERIA (Chemical)

Liquid rocket lines, bellows, flexible hoses, and filters, NASA SPACE VEHICLE DESIGN CRITERIA (Chemi

Turbopump systems for liquid rocket engines, NASA SPACE VEHICLE DESIGN CRITERIA (Chemical)

Turbopump systems for liquid rocket engines, NASA SPACE VEHICLE DESIGN CRITERIA (Chemical)

Liquid rocket engine fluid-cooled combustion chambers, NASA SPACE VEHICLE DESIGN CRITERIA (Chemical)

Liquid Rocket Engine Turbopump Bearings , NASA SPACE VEHICLE DESIGN CRITERIA (Chemical Propulsion)

Liquid rocket engine combustion stabilization devices, NASA SPACE VEHICLE DESIGN CRITERIA (Chemical)

Liquid rocket engine turbopump rotating-shaft seals, NASA SPACE VEHICLE DESIGN CRITERIA (Chemical)

Pressurization systems for liquid rockets, NASA SPACE VEHICLE DESIGN CRITERIA (Chemical)

Liquid propellant gas generators, NASA SPACE VEHICLE DESIGN CRITERIA (Chemical)

Liquid rocket engine axial-flow turbopumps, NASA SPACE VEHICLE DESIGN CRITERIA (Chemical)

Liquid rocket actuators and operators, NASA SPACE VEHICLE DESIGN CRITERIA (Chemical)

Liquid rocket engine nozzles, NASA SPACE VEHICLE DESIGN CRITERIA (Chemical)

Liquid rocket engine injectors, NASA SPACE VEHICLE DESIGN CRITERIA (Chemical)

Liquid rocket engine self-cooled combustion chambers, NASA SPACE VEHICLE DESIGN CRITERIA (Chemical)

Design Verification Test Matrix Development for the STME Thrust Chamber Assembly</TITLE> <LINK REV=

High Pressure Oxidizer Turbopump Inducer Dynamic Design Environment

Effect of Crystal Orientation on Analysis of Single-Crystal, Nickel-Based Turbine Blade Superalloys

Reusable Rocket Engine Operability Modeling and Analysis

Design-Development Testing, NASA SPACE VEHICLE DESIGN CRITERIA (Structures)

Captive-fired testing of solid rocket motors , NASA SPACE VEHICLE DESIGN CRITERIA (Chemical Propulsi

Solid propellant grain design and internal ballistics, NASA SPACE VEHICLE DESIGN CRITERIA (Chemical)

Solid rocket motor metal cases, NASA SPACE VEHICLE DESIGN CRITERIA (Chemical Propulsion)

Solid propellant grain structural integrity analysis, NASA SPACE VEHICLE DESIGN CRITERIA (Chemical)

Solid Rocket Motor Performance Analysis and Prediction, NASA SPACE VEHICLE DESIGN CRITERIA (Chemical

Solid Rocket Motor Igniters, NASA SPACE VEHICLE DESIGN CRITERIA (Chemical Propulsion)

Solid propellant processing factor in rocket motor design, NASA SPACE VEHICLE DESIGN CRITERIA (Chemi

Solid propellant selection and characterization, NASA SPACE VEHICLE DESIGN CRITERIA (Chemical)

Solid rocket thrust vector control, NASA SPACE VEHICLE DESIGN CRITERIA (Chemical)

Solid rocket motor internal insulation, NASA SPACE VEHICLE DESIGN CRITERIA (Chemical)

Solid rocket motor nozzles, NASA SPACE VEHICLE DESIGN CRITERIA (Chemical)

Spacecraft solar cell arrays, NASA SPACE VEHICLE DESIGN CRITERIA (Chemical)

The 1997 NASA Aerospace Battery Workshop

The 1999 NASA Aerospace Batery Workshop, NASA/CP-2000-209959

The 2000 NASA Aerospace Battery Workshop, NASA/CP-2001-210883

The 1998 NASA Aerospace Battery Workshop, NASA/CP-1999-209144

Spacecraft Sun Sensors, NASA SPACE VEHICLE DESIGN CRITERIA (Structures)

Spacecraft star trackers, NASA SPACE VEHICLE DESIGN CRITERIA (Guidance and Control)

Spacecraft Earth Horizon Sensors, NASA SPACE VEHICLE DESIGN CRITERIA (Guidance and Control)

Space vechicle qyroscope sensor applications, NASA SPACE VEHICLE DESIGN CRITERIA (Guidance)

Spaceborne digital computer systems, NASA SPACE VEHICLE DESIGN CRITERIA (Guidance)

Space vehicle displays design criteria, NASA SPACE VEHICLE DESIGN CRITERIA (Chemical)

Spaceborne electronic imaging systems, NASA SPACE VEHICLE DESIGN CRITERIA (Guidance)

Spaceborne electronic imaging systems, NASA SPACE VEHICLE DESIGN CRITERIA (Structures)

Integrated Circuit Electromagnetic Immunity Handbook, NASA/CR-2000-210017

Passive gravity-gradient libration dampers, NASA SPACE VEHICLE DESIGN CRITERIA (Guidance)

Space vehicle accelerometer applications, NASA SPACE VEHICLE DESIGN CRITERIA (Guidance)

Space vehicle accelerometer applications, NASA SPACE VEHICLE DESIGN CRITERIA (Guidance)

Spacecraft thermal control, NASA SPACE VEHICLE DESIGN CRITERIA (Environment)

Spacecraft gravitational torques, NASA SPACE VEHICLE DESIGN CRITERIA (Guidance and Control)

Spacecraft attitude control during thrusting maneuvers, NASA SPACE VEHICLE DESIGN CRITERIA (Guidance

Staging loads - Space vehicle design criteria, NASA SPACE VEHICLE DESIGN CRITERIA (Structures)

Flight-loads measurements during launch and exit, NASA SPACE VEHICLE DESIGN CRITERIA, Volume 3: Stru

Acoustic loads generated by the propulsion system, NASA SPACE VEHICLE DESIGN CRITERIA (Structures)

Deployable aerodynamic deceleration systems, NASA SPACE VEHICLE DESIGN CRITERIA (Structures)

Structural Design Criteria Applicable to a Space Shuttle, NASA SPACE VEHICLE DESIGN CRITERIA (Struct

Natural vibration modal analysis, NASA SPACE VEHICLE DESIGN CRITERIA (Structures)

Buckling strength of structural plates, NASA SPACE VEHICLE DESIGN CRITERIA (Structures)

Buckling Of Thin-Walled Doubly Curved Shells, NASA SPACE VEHICLE DESIGN CRITERIA (Structures)

Tubular spacecraft booms (extendible, reel stored), NASA SPACE VEHICLE DESIGN CRITERIA (Guidance)

Effects Of Structural Flexibility On Launch Vehicle Control Systems, NASA SPACE VEHICLE DESIGN CRITE

Preliminary criteria for the fracture control of space shuttle structures, NASA SPACE VEHICLE DESIGN

Panel flutter, NASA SPACE VEHICLE DESIGN CRITERIA (STRUCTURES)

Structural Vibration Prediction, NASA SPACE VEHICLE DESIGN CRITERIA (Structures)

Structural Design/Margin Assessment

Buckling of thin-walled truncated cones, NASA SPACE VEHICLE DESIGN CRITERIA (Structures)

Discontinuity stresses in metallic pressure vessels, NASA SPACE VEHICLE DESIGN CRITERIA (Structures)

Quasi-Static Probabilistic Structural Analyses Process and Criteria

Stress-corrosion cracking in metals, NASA SPACE VEHICLE DESIGN CRITERIA (Structures)

Effects of structural flexibility on entry vehicle control systems, NASA SPACE VEHICLE DESIGN CRITER

Nuclear and Space Radiation Effects on Materials, NASA SPACE VEHICLE DESIGN CRITERIA (Structures)

Transient Loads From Thrust Excitation, NASA SPACE VEHICLE DESIGN CRITERIA (Structures)

Effects of structural flexibility on spacecraft control systems, NASA SPACE VEHICLE DESIGN CRITERIA

Advanced composite structures, NASA SPACE VEHICLE DESIGN CRITERIA (Structures)

Advanced composite structures, NASA SPACE VEHICLE DESIGN CRITERIA (Structures)

Buckling of thin-walled circular cylinders, NASA SPACE VEHICLE DESIGN CRITERIA (Structures)

Wind Loads During Ascent, NASA SPACE VEHICLE DESIGN CRITERIA (Structures)

Buffeting during atmospheric ascent, NASA SPACE VEHICLE DESIGN CRITERIA (Structures)

Combining ascent loads, NASA SPACE VEHICLE DESIGN CRITERIA (Structures)

Aerodynamic And Rocket-Exhaust Heating During Launch And Ascent, NASA SPACE VEHICLE DESIGN CRITERIA

Local Steady Aerodynamic Loads During Launch and Exit, NASA SPACE VEHICLE DESIGN CRITERIA Volume 3:

Guidance and navigation for entry vehicles, NASA SPACE VEHICLE DESIGN CRITERIA (Guidance and Control

Entry thermal protection, NASA SPACE VEHICLE DESIGN CRITERIA (Structures)

Entry Vehicle Control, NASA SPACE VEHICLE DESIGN CRITERIA (Guidance and Control)

Entry gasdynamic heating, NASA SPACE VEHICLE DESIGN CRITERIA (Structures)

The Earth's Ionosphere, NASA SPACE VEHICLE DESIGN CRITERIA (Environment)

Assessment and Control of Spacecraft Magnetic Fields, NASA SPACE VEHICLE DESIGN CRITERIA (Environmen

Meteoroid Damage Assessment, NASA SPACE VEHICLE DESIGN CRITERIA (Structures)

Space Radiation Protection, NASA SPACE VEHICLE DESIGN CRITERIA (Structures)

The earth's trapped radiation belts, NASA SPACE VEHICLE DESIGN CRITERIA (Environment)

Lunar surface models NASA space vehicle design criteria /Environment/, NASA SPACE VEHICLE DESIGN CRI

Solar electromagnetic radiation, NASA SPACE VEHICLE DESIGN CRITERIA (Environment)

Earth albedo and emitted radiation, NASA SPACE VEHICLE DESIGN CRITERIA (Environment)

Prelaunch ground wind loads, NASA SPACE VEHICLE DESIGN CRITERIA

Surface models of Mars, 1975, NASA SPACE VEHICLE DESIGN CRITERIA (Environment)

Meteoroid Environment Model, 1970 - Interplanetary and Planetary, NASA SPACE VEHICLE DESIGN CRITERIA

The planets Uranus, Neptune, and Pluto (1971), NASA SPACE VEHICLE DESIGN CRITERIA (Environment)

The planet Saturn (1970), NASA SPACE VEHICLE DESIGN CRITERIA (Environment)

Magnetic fields - Earth and terrestrial, NASA SPACE VEHICLE DESIGN CRITERIA (Environment)

Gravity fields of the solar system, NASA SPACE VEHICLE DESIGN CRITERIA (Environment)

Interplanetary charged particle models (1974), NASA SPACE VEHICLE DESIGN CRITERIA (Environment)

Terrestrial Environment (Climatic) Criteria Guidelines for Use in Aerospace Vehicle Development, 199

Transportation and handling loads, NASA SPACE VEHICLE DESIGN CRITERIA (Structures)

Models of Mars' atmosphere (1974), NASA SPACE VEHICLE DESIGN CRITERIA (Environment)

Models of Venus atmosphere (1972), NASA SPACE VEHICLE DESIGN CRITERIA (ENVIRONMENT)

The planet Jupiter (1970), NASA SPACE VEHICLE DESIGN CRITERIA (Environment)

The environment of Titan, 1975, NASA SPACE VEHICLE DESIGN CRITERIA (Environment)

Meteorid environment model - 1969 [near earth to lunar surface], NASA SPACE VEHICLE DESIGN CRITERIA

the planet Mercury (1971), NASA SPACE VEHICLE DESIGN CRITERIA (Environment)

Models of earth's atmosphere (90 to 2500 km), NASA SPACE VEHICLE DESIGN CRITERIA (Environment)

Surface atmospheric extremes (launch and transportation areas), NASA SPACE VEHICLE DESIGN CRITERIA (

Assessment and control of electrostatic charges, NASA SPACE VEHICLE DESIGN CRITERIA (Environment)

Structural interaction with transportation and handling systems, NASA SPACE VEHICLE DESIGN CRITERIA

Meteoroids and Orbital Debris: Effects on Spacecraft

Lightning Protection Guidelines for Aerospace Vehicles, NASA/TM-1999-209734

A Compendium of Wind Statistics and Models for the NASA Space Shuttle and Other Aerospace Vehicle Programs, NASA/CR-1998-208859

 Space Elevators An Advanced Earth-Space Infrastructure for the New Millennium, NASA/CP-2000-210429

Thermodynamic Cycle Analysis of Magnetohydrodynamic-Bypass Hypersonic Airbreathing Engines, NASA/TP-2000-210387

General Public Space Travel and Tourism- Volume 2 Workshop Proceedings , NASA/CP-1999-209146

Affordable In-Space Transportation, NASA TM-108521

• 391 26 Flutter, buzz, and divergence, NASA SPACE VEHICLE DESIGN CRITERIA Volume 3: Structures. Part B: Load
• 397 29 Lubrication friction and wear, NASA SPACE VEHICLE DESIGN CRITERIA (Structures)
• 364 29 Flight separation mechanisms , NASA SPACE VEHICLE DESIGN CRITERIA (Structures)
• 356 28 Acceptance Testing, NASA SPACE VEHICLE DESIGN CRITERIA (Structures)
• 346 29 Interactions with umbilicals and launch stand, NASA SPACE VEHICLE DESIGN CRITERIA (Structures)
• 346 28 Spacecraft Mass Expulsion Torques, NASA SPACE VEHICLE DESIGN CRITERIA (Guidance and Control)
• 345 28 Compartment venting, NASA SPACE VEHICLE DESIGN CRITERIA (Structures)
• 335 31 Assessment and control of spacecraft electromagnetic interference, NASA SPACE VEHICLE DESIGN CRITERI
• 332 28 Spacecraft Radiation Torques, NASA SPACE VEHICLE DESIGN CRITERIA (Guidance and Control)
• 324 28 Qualification Testing, NASA SPACE VEHICLE DESIGN CRITERIA (Structures)
• 317 35 Space Tethers: Design Criteria
• 311 28 Spacecraft Aerodynamic Torques, NASA SPACE VEHICLE DESIGN CRITERIA (Guidance And Control)
• 309 29 Landing Impact Attenuation For Non-Surface-Planing Landers, NASA SPACE VEHICLE DESIGN CRITERIA (Stru
• 309 28 Spacecraft magnetic torques, NASA SPACE VEHICLE DESIGN CRITERIA (Environment)
• 298 32 Glossary of terms and table of conversion factors used in design of chemical propulsion systems, NAS
• 294 31 Working on the Boundaries: Philosophies and Practices of the Design Process

 A Conceptual Design for the Attitude Control and Determination System for the Magnetosphere Imager S

• 218 28 Illustrated Structural Application of Universal First-Order Reliability Method.
• 210 29 A History of Aerospace Problems, Their Solutions, Their Lessons
• 153 27 On the Design of Structural Components Using Materials With Time-Dependent Properties
• 150 33 Information Flow in the Launch Design/Analysis Process
• 147 26 Analysis and Assessment of Peak Lightning Current Probabilities at the NASA Kennedy Space Center
• 131 34 Static Strength Characteristics of Mechanically Fastened Composite Joints (MSFC Center Director's Di
• 130 46 Design of Multiple-Ply Laminated Composite Tapered Beams
• 127 31 Marshall Space Flight Center Electromagnetic Compatibility Design and Interference Control (MEDIC) H
• 125 32 Design and Test of Low-Profile Composite Aerospace Tank Dome (MSFC Center Director's Discretionary
• 116 31 CORSSTOL: Cylinder Optimization of Rings, Skin, and Stringers With Tolerance Sensitivity
• 106 29 Investigation of the Springback Associated With Composite Material Component Fabrication (MSFC Cente
• 103 31 Multilayer Insulation Material Guidelines
• 101 29 System Guidelines for EMC Safety--Critical Circuits: Design, Selection, and Margin Demonstration
• 100 41 Preliminary Analysis Techniques for Ring and Stringer Stiffened Cylindrical Shells</TITLE> <LINK RE
• 99 36 Spacecraft Environments Interactions: Space Radiation and its Effects on Electronic Systems
• 98 33 The Natural Space Environment: Effects on Spacecraft
• 98 45 The Effects of Compressive Preloads on the Compression-After-Impact Strength of Carbon/Epoxy</TITL
• 98 29 A Recommended Procedure for Estimating the Cosmic-Ray Spectral Parameter of a Simple Power Law With
• 98 29 Estimating Cosmic-Ray Spectral Parameters From Simulated Detector Responses With Detector Design Imp
• 96 30 System Engineering "Toolbox" for Design-Oriented Engineers
• 94 37 Designing for Human Presence in Space: An Introduction to Environmental Control and Life Support Sys
• 94 35 User's Guide for Monthly Vector Wind Profile Model
• 94 32 Preliminary Control System Design and Analysis for the Space Station Furnace Facility Thermal Contro
• 92 31 Thruster Injector Faceplate Testing in Support of the Aerojet Rocket-Based Combined Cycle (RBCC) Con
• 92 32 Importance of the Natural Terrestrial Environment with Regard to Advanced Launch Vehicle Design and
• 92 36 Lightning Protection Guidelines for Aerospace Vehicles
• 91 28 The Spacelab Accomplishments Forum
• 91 28 Tether Technology Interchange Meeting
• 90 43 An Overview of Reliability Growth Models and Their Potential Use for NASA Applications. </TITLE> <L
• 89 45 Shear Joint Capability Versus Bolt Clearance
• 89 36 High Performance, Robust Control of Flexible Space Structures (MSFC Center Director's Discretionary
• 89 42 A Case Study for Probabilistic Methods Validation (MSFC Center Director's Discretionary Fund Final
• 89 40 <I>International Space Station</I> ECLSS Technical Task Agreement Summary Report
• 88 30 An Assessment on Finite-Element Modeling Techniques for Thick-Solid/Thin-Shell Joints Analysis</TITL
• 88 33 Loads Combination Research at Marshall Space Flight Center
• 88 30 Spacecraft Environments Interactions: Protecting Against the Effects of Spacecraft Charging
• 88 28 The On-Orbit Radio Frequency Environment
• 87 30 United States Control Module Guidance, Navigation, and Control Subsystem Design Concept
• 87 32 Advanced Liquid Oxygen (LO2) Propellant Conditioning Concept Testing
• 86 57 Computerized Atmospheric Trace Contaminant Control Simulation for Manned Spacecraft</TITLE> <LINK R
• 86 28 Inner Magnetosphere Imager (IMI) Solar Terrestrial Probe Class Mission Preliminary Design Study Repo
• 85 30 Operations Summary for the Convection and Moisture Experiment (CAMEX)
• 83 27 Simulation Model for Probabilistic Analysis of Space Shuttle Abort Modes
• 83 31 Deflections of a Uniformly Loaded Circular Plate With Multiple Support Points
• 82 31 Interplanetary Mission Design Handbook: Earth-to-Mars Mission Opportunities and Mars-to-Earth Return
• 82 39 Double-Plate Penetration Equations
• 82 34
• 82 30
• 81 28 Enhancement of High-Speed Infrared Array Electronics (Center Director's Discretionary Fund Final Rep
• 80 36 Evaluation of Trapped Radiation Model Uncertainties for Spacecraft Design
• 79 44 Preliminary In-Flight Loads Analysis of In-Line Launch Vehicles Using the VLOADS 1.4 Program
• 79 38 On the Analytical Determination of Relaxation Modulus of Viscoelastic Materials by Prony's Interpola
• 79 31 A 20k Payload Launch Vehicle Fast Track Development Concept Using an RD-180 Engine and a Centaur Upp
• 78 30 A Guidance and Control Assessment of Three Vertical Landing Options for RLV
• 77 47 An Indepth Probabilistic Study of External Tank Attach Ring
• 77 32 NDE Process Development Specification for SRB Composite Nose Cap </TITLE> <LINK REV="made" HREF="mai
• 76 33 Contamination Control Engineering Design Guidelines for the Aerospace Community
• 76 27 Root-Sum-Square Structural Strength Verification Approach
• 75 32 Design Guidelines for Shielding Effectiveness, Current Carrying Capability, and the Enhancement of C
• 75 36 Trapped Radiation Model Uncertainties: Model--Data and Model--Model Comparisons
• 75 32 Application of Rapid Prototyping and Wire Arc Spray to the Fabrication of Injection Mold Tools (MSFC
• 75 29 Natural Orbital Environment Definition Guidelines for Use in Aerospace Vehicle Development
• 74 30 Contamination Effects on EUV Optics
• 74 37 Characterizing Secondary Debris Impact Ejecta
• 74 29 Launch Vehicle Flight Control Augmentation Using Smart Materials and Advanced Composites (CDDF 93-05
• 74 31 Development of Tailorable Electrically Conductive Thermal Control Material Systems
• 73 30 Review of Our National Heritage of Launch Vehicles Using Aerodynamic Surfaces and Current Use of The
• 73 32 Tether-Based Investigation of the Ionosphere and Lower Thermosphere Concept Definition Study Report
• 73 41 A TREETOPS Simulation of the STABLE Microgravity Vibration Isolation System
• 73 32 Spacecraft Environments Interactions: Solar Activity and Effects on Spacecraft
• 72 29 Test Load Verification Through Strain Data Analysis
• 72 32 Spacecraft System Failures and Anomalies Attributed to the Natural Space Environment
• 72 31 Affordable In-Space Transportation
• 72 31 Development of an Open Architecture Flight Qualified Computer (CDDF Final Report, Project Number 92-
• 71 46 Comprehensive Structural Dynamic Analysis of the SSME/AT Fuel Pump First-Stage Turbine Blade</TITLE
• 71 32 The Solar Array-Induced Disturbance of the Hubble Space Telescope Pointing System
• 70 29 Application of Rapid Prototyping Methods to High-Speed Wind Tunnel Testing (MSFC Center Directors Di
• 70 45 A Compendium of Wind Statistics and Models for the NASA Space Shuttle and Other Aerospace Vehicle Pr
• 70 29 Catastrophic Failure Modes Assessment of the International Space Station Alpha
• 70 32 Research Reports - 1995 NASA/ASEE Summer Faculty Fellowship Program
• 70 33
• 69 55 Simplified Liquid Oxygen Propellant Conditioning Concepts
• 68 33 The Magnetosphere Imager Mission Concept Definition Study Final Report
• 68 31 Research Report--1997 NASA/ASEE Summer Faculty Fellowship Program
• 68 30 A New Aging Treatment for Improving Cryogenic Toughness of the Main Structural Alloy of the Super Li
• 68 47 Research Reports - 1996 NASA/ASEE Summer Faculty Fellowship Program
• 67 30 Design of Launch Vehicle Flight Control Augmentors and Resulting Flight Stability and Control (Cente
• 67 33 Final Report on Life Testing of the Vapor Compression Distillation/ Urine Processing Assembly (VCD/U
• 67 30 High Frequency Flow/Structural Interaction in Dense Subsonic Fluids
• 66 29 System Report for the Optical Properties Monitor (OPM) Experiment
• 65 31 Development of a Probabilistic Dynamic Synthesis Method for the Analysis of Nondeterministic Structu
• 65 31 Developmental Problems and Their Solution for the Space Shuttle Main Engine Alternate Liquid Oxygen
• 65 33 Rationale and Methods for Archival Sampling and Analysis of Atmospheric Trace Chemical Contaminants
• 63 31 The Microgravity Research Experiments (MICREX) Data Base
• 63 31 The Microgravity Research Experiments (MICREX) Data Base

Aerodynamics

Review of X-33 Hypersonic Aerodynamic and Aerothermodynamic Development, , Augus

X-33 Aerodynamic and Aeroheating Computations for Wind Tunnel and Flight Conditi

X-33 Hypersonic Aerodynamic Characteristics, AIAA 99-4162, August 9-11, 1999,

An Inviscid Computational Study of an X-33 Configuration at Hypersonic Speeds, N

Inviscid Flow Computations of the Orbital Sciences X-34 Over a Mach Number Range

X-34 Vehicle Aerodynamic Characteristics, AIAA 98-2531, June 15-18, 1998,

Summary Report of the Orbital X-34 Wing Static Aeroelastic Study, NASA/CR-2001-2

Aerodynamic Characteristics of Two Waverider-Derived Hypersonic Cruise, NASA TP-

Propulsion System Airframe Integration Issues and Aerodynamic Database Developme

Aerodynamic Database Development for the Hyper-X Airframe Integrated Scramjet Pr

Aerodynamic Performance and Flow-Field Characteristics of Two Waverider-Based Hy

Integrated Aero-Propulsive CFD Methodology for the Hyper-X Flight Experiment, AI

Prediction of Hyper-X Stage Separation Aerodynamics Using CFD, AIAA 2000-4009, A

Evaluation of the Low-Speed Stability and Control Characteristics of a Mach 5.5

Hypersonic Aerodynamic Characteristics of a Proposed Single-Stage-to-Orbit Vehic

Supersonic Aerodynamic Characteristics of a Circular Body Earth-to-Orbit Vehicle

Subsonic Aerodynamic Characteristics of a Proposed Advanced Manned Launch System

Subsonic Aerodynamic Characteristics of a Circular Body Earth-to-Orbit Vehicle,

Experimental and Theoretical Study of Aerodynamic Characteristics of Some Liftin

Longitudinal and Lateral-Directional Aerodynamic Characteristics of a Wing-Cone

Aerodynamic Characteristics and Control Effectiveness of the HL-20 Lifting Body

Overview of X-38 Hypersonic Wind Tunnel Data and Comparison With Numerical Resul

Overview of X-38 Hypersonic Aerothermodynamic Wind Tunnel Data and Comparison Wi

Preliminary Subsonic Aerodynamic Model for Simulation Studies of the HL-20 Lifti

Aeroheating and Aerodynamic CFD Validation and Prediction for the X-38 Program,

Aerodynamic Characteristics and Pressure Distributions for an Executive-Jet Base

Supersonic Aerodynamic Characteristics of an Advanced F-16 Derivative Aircraft C

Aerodynamic Characteristics, Database Development and Flight Simulation of the X

Aerodynamic Characteristics and Development of the Aerodynamic Database of the X

Modeling of Aircraft Unsteady Aerodynamic Characteristics, Part 1 - Postulated M

Inviscid Flow Computations of Two '07 Mars Lander Aeroshell Configurations Over

Inviscid Flow Computations of Several Aeroshell Configurations for a '07 Mars La

Measurements and Predictions for a Distributed Exhaust Nozzle, AIAA 2001-2236, M

4 Aerodynamic Measurements on a Large Splitter Plate for the NASA Langley Transoni

2 Low-Speed Longitudinal and Lateral-Directional Aerodynamic Characteristics of th

2 Separation Characteristics of Generic Stores From Lee Side of an Inclined Flat P

9 Hypersonic Lateral and Directional Stability Characteristics of Aeroassist Fligh

37 Two-Dimensional Aerodynamic Characteristics of Several Polygon-Shaped Cross-Sect

32 Aerodynamic Characteristics of an Aerospace Vehicle During a Subsonic Pitch-Over

44 Low-Speed Longitudinal Aerodynamic Characteristics Through Poststall for Twenty-

38 An Experimental Investigation of a Mach 3.0 High-Speed Civil Transport at Supers

35 Low-Speed Wind-Tunnel Investigation of the Stability and Control Characteristics of a Series of Flying Wings With Sweep Angles of 50 Degrees

3 41 Low-Speed Wind-Tunnel Investigation of the Stability and Control Characteristicsof a Series of Flying Wings With Sweep Angles of 60 Degrees

24 Effect of Full-Chord Porosity on Aerodynamic Characteristics of the NACA 0012 Ai

26 Unsteady Slat-Wake Characteristics of a High-Lift Configuration, AIAA 2000-0139,

23 An Approach to the Constrained Design of Natural Laminar Flow Airfoils, NASA CR-

42 Low-Speed Wind-Tunnel Investigation of the Stability and Control Characteristics

25 Reynolds Number Effects on a Supersonic Transport at Transonic Conditions, AIAA

35 Effect of Afterbody Geometry on Aerodynamic Characteristics of Isolated Nonaxisy

53 Calculation of AGARD Wing 445.6 Flutter Using Navier-Stokes Aerodynamics, AIAA P

38 Wind Tunnel Aerodynamic Characteristics of a Transport-Type Airfoil in a Simulat

23 Data Mining of NASA Boeing 737 Flight Data---Frequency Analysis of In-Flight Rec

37 An Approach to Constrained Aerodynamic Design With Application to Airfoils , NAS 438

26 Characterization of Pressure Sensitive Paint Intrusiveness Effects on Aerodynami 43

5 48 Experimental Aerodynamic Characteristics of a Generic Hypersonic , NASA TM-4413

47 Aerodynamic Performance and Flow-Field Characteristics of Two Waverider-Based Hy

24 A Parametric Study of Accelerations of an Airplane Due to a Wake Vortex System, 425

32 Experimental Study at Low Supersonic Speeds of a Missile Concept Having Opposing 424

24 Analysis of Wind Tunnel Oscillatory Data of the X-31A Aircraft, NASA/CR-1999-208 424

37 Experimental and Analytical Investigation of Dynamic Characteristics of Extensio 42

37 Effects of Forebody Strakes and Mach Number on Overall Aerodynamic Characteristi 419

26 The Benchmark Active Controls Technology Model Aerodynamic Data, AIAA 97-0829, J 413

25 Reynolds Number Effects on a Supersonic Transport at Subsonic High-Lift Conditio 412

0 50 Navier-Stokes, Flight, and Wind Tunnel Flow Analysis for the F/A-18 Aircraft, NA 408

40 Multiaxis Thrust-Vectoring Characteristics of a Model Representative of the F-18 40

4 21 Spatial Characteristics of the Unsteady Differential Pressures on 16 Percent F/A 403

47 The NASA Langley 16-Foot Transonic Tunnel---Historical Overview, Facility Descri 40

0 40 Effect of Leading and Trailing-Edge Flaps on Clipped Delta Wings With and Withou 398

395 24 Computational Analysis of Semi-Span Model Test Techniques, CR-4709, March 1996,

43 The Natural Flow Wing-Design Concept , NASA TP-3193 , April 1992 , 392 35 Dynamic Stall Effects and Applications To High Performance Aircraft, AGARD-R-776 23 22 Hypersonic Pitching-Moment Shift for Stardust Reentry Capsule Forebody, NASA/TM- 28 Multidisciplinary Approach to Aerospike Nozzle Design, NASA TM-110326, February 299

21 Advanced Aerodynamic Control Effectors, , October 19-21, 1999, 285 28 Multidisciplinary Approach to Linear Aerospike Nozzle Optimization, AIAA 97-3374 285 35 Low-Speed Wind Tunnel Tests of Two Waverider Configuration Models., AIAA 95-6093 284 33 Wind-Tunnel Free-Flight Investigation of a Supersonic Persistence Fighter, NASA 284 24

272 23 Aerodynamic Parameters of High Performance Aircraft Estimated From Wind Tunnel a 272 26 270 32 Characteristics of the Shuttle Orbiter Leeside Flow During a Reentry Condition, 268 7 Mars Ascent Vehicle Flight Analysis, AIAA 98-2850, June 15-18, 1998, 25

2 252 28 Prediction and Validation of Mars Pathfinder Hypersonic Aerodynamic Data Base, A 244 21 Development of X-33/X-34 Aerothermodynamic Data Bases: Lessons Learned and Futur 23 Experimental Verification of the Osculating Cones Method for Two Waverider Foreb 239 36 DSMC Grid Methodologies for Computing Low-Density, Hypersonic Flows About Reusab 239 26 Multidisciplinary High-Fidelity Analysis and Optimization of Aerospace Vehicles, 235 23 Effective Thermal Conductivity of High Temperature Insulations for Reusable Laun 234 36 An Engineering Aerodynamic Heating Method For Hypersonic Flow, AIAA 92-0499, Jan 231 29 Aerodynamics of the Mars Microprobe Entry Vehicles, AIAA Paper 97-3658, August 1 28 227 25 Sample Returns Missions in the Coming Decade, , October 2-6, 2000, 8 Analysis of the Staging Maneuver and Booster Glideback Guidance for a Two-Stage, 28 Mars Microprobe Entry Analysis, , February 2-6, 1997, 221 24 Rarefied Transitional Bridging of Blunt Body Aerodynamics, , July 26-31, 1998,

http://techreports.larc.nasa.gov/ntrs/hget.cgi?larc?2200/1=techreports.larc.nasa.gov%3A210;2=/usr/local/web/waissrc/ltrs_index;3=0%202200%20/usr/local/web/htdocs/ltrs/refer/1997/cr/NASA-97-cr201730.refer.html;4=techreports.larc.nasa.gov%3A210;5=/usr/local/web/waissrc/ltrs_index;6=0%202200%20/usr/local/web/htdocs/ltrs/refer/1997/cr/NASA-97-cr201730.refer.html;7=%00;