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Technology Readiness Level (TRL) as the foundation of Human Readiness Level (HRL)
Environmental Test Effectiveness
A High-Heritage Blunt-Body Entry, Descent, and Landing Concept for Human Mars Exploration
Interoperable Solution for Test Execution in Various I&T Environments
High-Energy Atmospheric Reentry Test Aerothermodynamic Analysis
Spacecraft Dynamics Should be Considered in Kalman Filter Attitude Estimation
As-Flown Shuttle Micro-Meteoroid Orbital Debris (MMOD) Assessment History
The ISS as a Testbed for Future Large Astronomical Observatories: The OpTIIX Demonstration Program
Solar Dynamics Observatory Launch and Commissioning
Lessons Learned from Shuttle Payload Verification Loads Analysis
Human Operations Beyond LEO by the End of the Decade: An Affordable Near-Term "Stepping Stone"
NASA Handbook for Spacecraft Structural Dynamics Testing
Magnetospheric Multiscale Mission (MMS) Phase 2B Navigation Performance
Handling Qualities Evaluation of Pilot Tools for Spacecraft Docking in Earth Orbit
Simplified Model for iLIDS IDD
Cluster Development Test 2: An Assessment of a Failed Test
Current LISA Spacecraft Design
Low Impact Docking System (LIDS)
Inflight Characterization of the Cassini Spacecraft Propellant Slosh and Structural Frequencies
Post-Landing Orion Crew Survival in Warm Ocean Areas: A Case Study in Iterative Environmental Design
International Space Station USOS Crew Quarters Development
Vertical Drop Testing and Analysis of the WASP Helicopter Skid Gear
A High Performance Command and Data Handling System for NASA's Lunar Reconnaissance Orbiter
Response of Damaged and Undamaged Tailored Extension-Shear-Coupled Composite Panels
Trim Flight Conditions for a Low-Boom Aircraft Design Under Uncertainty
Control of the ST7 Disturbance Reduction System Flight Experiment
Sensor Selection and Optimization for Health Assessment of Aerospace Systems
Orion Orbit Control Design and Analysis
New Air-Launched Small Missile (ALSM) Flight Testbed for Hypersonic Systems
An Overview of Space Power Systems for NASA Missions
NASA Dryden's UAS Service Capabilities
Apollo Seals: A Basis for the Crew Exploration Vehicle Seals
Orion Entry, Descent, and Landing Performance and Mission Design
Automated Rendezvous and Docking Sensor Testing at the Flight Robotics Laboratory
Spacecraft Design Considerations for Piloted Reentry and Landing
Flight Testing of Hybrid Powered Vehicles
Orbiter Gap Filler Bending Model for Re-entry
Aerospace Applications of Optimization under Uncertainty
Aerospace Applications of Optimization under Uncertainty
The Business Case for Spiral Development in Heavy Lift Launch Vehicle Systems
Design and Development of a Real-Time Model Attitude Measurement System for Hypersonic Facilities
A Design Comparison of Atmospheric Flight Vehicles for the Exploration of Titan
The New Millennium Program Space Technology 5 (ST-5) Mission
A Comparative Study of Aerocapture Missions with a Mars Destination
Exploring the Feasibility of Electrostatic Shielding for Spacecrafts
TESTING OF A 20-METER SOLAR SAIL SYSTEM