Loads and Sizing for Launch Vehicle Conceptual and Preliminary Design
Low-Thrust Optimal Control of Spacecraft Hovering for Proximity Operations
Autonomous Vision-Based Algorithm for Interplanetary Navigation
Dynamics Simulation of a Small Satellite with a Robotic Manipulator for Additive Manufacturing
Slew Maneuver Constraints for Agile Flexible Spacecraft
Bistable Deployable Composite Booms with Parabolic Cross Sections
Modeling Fiber Microbuckling in the Bending of Soft Composites Using Nonlinear Homogenization
One-Winged Momentum-Biased Solar Sail: A New Methodology for Propellantless Attitude Control
Rigid-Body Attitude Control, Synchronization, and Bipartite Consensus Using Feedback Reshaping
Anomaly Detection Using Deep Learning Respecting the Resources on Board a CubeSat
Dynamic Analysis of Bidirectional Solar Arrays with Flexible Panels and Clearance Joints
Polynomial Guidance for Impact-Time Control Against Maneuvering Targets
Electrostatic Discharge Tests of Carbon Composite Materials with Conductive Resin
3D-printed, electrically conductive structures for magnetic attitude control
Design Considerations for an Earth–Mars Cycler Spacecraft Using the S1L1 Cycler
Deployment Dynamics Analysis of an Origami-Folded Spacecraft Structure with Elastic Hinges
Space Environment Exposure Effects on Ceramic Coating for Thermal Protection Systems
Overview of the NASA Advanced Composite Solar Sail (ACS3) Technology Demonstration Project
Design of a Microgravity Hybrid Inflatable Airlock
Stability of Potential Systems to General Positional Perturbations
Precise Orbit Determination Technique to Refine Spacecraft Mechanical Modeling
Gateway Lunar Habitat Modules as the Basis for a Modular Mars Transit Habitat
Upper-Bound Vibration Spectrum Computation for Membrane Response from a Few Point Measurements
Space Launch System Mobile Launcher Modal Pretest Analysis
Space Launch System Mobile Launcher Modal Pretest Analysis
Aeroelastic Stability of Conventional and Tow-Steered Composite Plates Under Stochastic Fiber Volume
Postmission Disposal Options in the 2019 USG Orbital Debris Mitigation Standard Practices (ODMSP)
Small Satellites and Structural Design
Overview of Small Satellite Technology and Systems Design
Inflatable Technology: Using Flexible Materials to Make Large Structures
From Apollo to Future Missions to Moon, Mars and Beyond - on Entry and Thermal Protection Systems
Corrosion on Mars: Effect of the Mars Environment on Spacecraft Materials
Attitude determination sensor for low Earth orbit satellite based on Lorentz force
Adaptive Pose Tracking Control for Spacecraft Proximity Operations Under Motion Constraints
Constructing a Large Antenna Reflector via Spacecraft Formation Flying and Reconfiguration Control
HEEET: Innovative New TPS for Extreme Entry
Dynamic Response of Aluminum Honeycomb Panels to High-Frequency Laser Shock Excitations
Spacecraft Structure Model Validation and Test Philosophy
Folding Approaches for Tensioned Precision Planar Shell Structures
Analytical Optimization Method for Space Logistics
Optimization of a Multifunctional Hot Structure Aeroshell for Mars Entry
Advanced Dual-Pull Mechanism for Deployable Spacecraft Booms
High-Fidelity Semianalytical Theory for a Low Lunar Orbit