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Engineering Directorate Materials and Processes Laboratory Capabilities
A Multi-Disciplinary Analysis Framework for the Design of Small Launch Vehicles
Integrated Design Results for the MSR DAC-0.0 Mars Ascent Vehicle
Test Capabilities of the NASA Langley Direct Connect Supersonic Combustion Test Facility
Apollo Lunar Landing GN&C Lessons Learned
Astrobee Working Group (AWG) Facility slides
Attitude Control Approach For Descent and Transfer Elements During Long-Term Ballistic Coast
NASA’s Space Launch System: Status Report on the World’s Most Capable Launch Vehicle
SLS Evolution: Comparing Configurations Using System Exergy
Joining and Mechanical Systems at Langley Research Center
Manual Crew Override of Vehicle Landings Following G-Transitions
NASA ARC Mission Design Center Overview
High Performance Rotating Detonation Rocket Engine for Mars Interplanetary Transport
NASA SMALL SPACECRAFT TECHNOLOGY (SST) PROGRAM and RECENT TECHNOLOGY DEMONSTRATIONS
SpaceX Dragon 1 Post Flight MMOD Inspection Campaign
The Flight Dynamics Risk Assessment of Artemis I
Gas-Particle Interaction Model Development in Plume Surface Interaction Erosion and Cratering
Goes-16 On-Station Custom Maneuver Generation with Focussuite
TECHEDSAT-7 and 10: The Little Spacecraft That Could
Automated Software for Crewed Spacecraft - Bridging the Gap from Sci Fi to Reality
Post-flight Reconstruction for a Mars Ascent Vehicle
NASA Centers and Universities Collaborate in Annual Smallsat Technology Partnerships
SLS Evolution: Comparing Configurations Using System Exergy
Overview of the Acoustic Testing of the European Service Module Structural Test Article (E-STA)
X-57 Maxwell Airworthiness Validation Plan
Space Shuttle Cargo Integration Coupled Loads Analysis Lessons Learned
Total Technology Readiness Level: Accelerating Technology Readiness for Aircraft Design
X-57 Structural Analysis, Wing Design, & Testing (Statics)
Integrated Modal Test of the Artmis I Launch Vehicle
X-57 Whirl Flutter & Propeller Stability Assessments
NASA Common Research Model (CRM) – Past, Present and Future
Goniometric and Polarized Imaging Spectroscopic Lab Measurements of Spacecraft Materials
Space Technology Mission Directorate Small Spacecraft Technology
Small Satellite-sized Hypersonic Inflatable Decelerators (HIAD) for Interplanetary Science Missions
Flight Envelope Assessment of SmallSat Aerocapture Trajectories at Venus and Mars
NASA's Human Landing System: Enabling the next generation of lunar science
Challenges, Lessons Learned, and Methodologies from the LCRD Optical Communication System AI&T