Shape Sensing for Wings with Spars and Ribs Using Simulated Strain
Orion Exploration Flight Test 1 (EFT-1) Best Estimated Trajectory Development
Orion Launch Abort System Nominal Jettison Performance on Exploration Flight Test 1
Orion Launch Abort System Performance on Exploration Flight Test 1
Orion Launch Abort System Jettison Motor Performance During Exploration Flight Test 1
Experimental and Computational Sonic Boom Assessment of Lockheed-Martin N+2 Low Boom Models
Concept designs for NASA's Solar Electric Propulsion Technology Demonstration Mission
Cart3D Simulations for the First AIAA Sonic Boom Prediction Workshop
Summary and Statistical Analysis of the First AIAA Sonic Boom Prediction Workshop
LAVA Simulations for the AIAA Sonic Boom Prediction Workshop
Overview of the Launch Vehicle Blast Environments Development Efforts
Structural Dynamics and Data Analysis
OCO-2 (Orbiting Carbon Observatory-2) on Schedule for a 01 July 2014 Launch
Study of Movement and Seepage Along Levees Using DInSAR and the UAVSAR Instrument
Design of Spacecraft Missions to Remove Multiple Orbital Debris Objects
Command and Data Handling System for the Panchromatic Fourier Transform Spectrometer
Mars as a Destination in a Capability-Driven Framework
Delta-V Budgets for Robotic and Human Exploration of Phobos and Deimos
Delta-V Budgets for Robotic and Human Exploration of Phobos and Deimos
Space Transportation Infrastructure Supported By Propellant Depots
Flow Visualization and Detailed Load Measurements Over a Maneuvering UCAV 1303
Flight Avionics Sequencing Telemetry (FAST) DIV Latching Display
Aerodynamic Studies over a Maneuvering UCAV 1303 Configuration
Establish the Delta Military Operations Area Environmental Assessment
Innovations in Delta Differential One-Way Range: from Viking to Mars Science Laboratory
Propulsive Maneuver Design for the 2007 Mars Phoenix Lander Mission
Assuring Access to Space: The Partnership Continues
Sting Influence on Vortex Breakdown on a 65 Degree Delta Wing in Transonic Flow
Spanwise Wing Loads on the Space Shuttle Orbiter during Roll Maneuver
Ares V: Designing the Heavy Lift Capability to Explore the Moon
Crew Exploration Vehicle Ascent Abort Trajectory Analysis and Optimization