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Spanwise Adaptive Wing - PTERA Flight Test
Low-Thrust Transfers from Distant Retrograde Orbits to L2 Halo Orbits in the Earth-Moon System
Low-Thrust Transfers from Distant Retrograde Orbits to L2 Halo Orbits in the Earth-Moon System
MDO Problem Suite V3: We have the technology, we can rebuilt it!
Design Guide for Aerodynamics Testing of Earth and Planetary Entry Vehicles in a Ballistic Range
Development of an Inertia Relief Method for Aircraft with Dissimilar Engines in LEAPS
VSP-CAD-CFD Interaction and Advanced Modeling Techniques
Development of an Inertia Relief Method for Aircraft with Dissimilar Engines in LEAPS
Analysis of High-Speed Aerodynamics of a Swept Wing with Seamless Flaps
History and Status of the CDISC Aerodynamic Design Method
Design Considerations for a Mars Highland Helicopter
History and Status of the CDISC Aerodynamic Design Method
Multidisciplinary Design Optimization of Low-Boom Supersonic Aircraft with Mission Constraints
Interplanetary Terminal Procedure Design Applied to Lunar Landing
NDARC: NASA Design and Analysis of Rotorcraft
NDARC NASA Design and Analysis of Rotorcraft
NDARC NASA Design and Analysis of Rotorcraft
NDARC - NASA Design and Analysis of Rotorcraft
NDARC NASA Design and Analysis of Rotorcraft
Buckling of Thin-Walled Circular Cylinders
General Mission Analysis Tool (GMAT)
Design Limit Loads and Verification Approach for the TESS Observatory
InSight Entry, Descent and Landing Post-Flight Performance Assessment
An Overview of NASA’s Learn-to-Fly Technology Development
Computational Investigation of Powered Descent for Human-Scale Mars Landers
A Simulation Framework for Precision Landing and Hazard Avoidance Technology Assessments
Overview and Performance of the LOFTID Instrumentation Suite
Topology Optimization of Low-Speed Aeroelastic Wind Tunnel Models
Entry, Descent, and Landing technological barriers and crewed MARS vehicle performance analysis
Topology Optimization of Low-Speed Aeroelastic Wind Tunnel Models
InSight Entry, Descent and Landing Pre-Flight Performance Predictions
Trajectory Design to Mitigate Risk on the Transiting Exoplanet Survey Satellite (TESS) Mission
What is a Tiltrotor? A Fundamental Reexamination of the Tiltrotor Aircraft Design Space
Techniques for Conducting Effective Concept Design and Design-to-Cost Trade Studies
A Modular Multiphysics Simulation Framework
Topology Optimization of Low-Speed Aeroelastic Wind Tunnel Models
MMS Extended Mission Design: Evaluation of a Lunar Gravity Assist Option
Operational Analysis of Vertiport Surface Topology
NDARC NASA Design and Analysis of Rotorcraft - Input, Appendix 4
Handling Qualities Optimization for Rotorcraft Conceptual Design
NDARC NASA Design and Analysis of Rotorcraft Theory Appendix 1
Structural Design and Aeromechanical Analysis of Unconventional Blades for Future Mars Rotorcraft