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Astronautik
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Adaptive-Mesh Sequential Convex Programming for Space Trajectory Optimization
Space Flight Demonstration of Rotating Detonation Engine Using Sounding Rocket S-520-31
Automated Design of Optimal Finite Thrust Orbit Insertion with Ballistic Flyby Constraints
Trajectory Analysis of a Zero-Pitch-Angle E-Sail with Homotopy Perturbation Technique
Reply by the Authors to G. Rapakoulias and P. Tsiotras
Spaceflight Logistics Approach to Modeling Aggregated Vehicle Concepts
Existence of Probability Density Function for Norm of Finite-Dimensional Random Vector
Nitrous Oxide/Ethanol Cylindrical Rotating Detonation Engine for Sounding Rocket Space Flight
Ethical Standards for Publication of Aeronautics and Astronautics Research
Ethical Standards for Publication of Aeronautics and Astronautics Research
Ethical Standards for Publication of Aeronautics and Astronautics Research
Optimization of the Ballistic Deployment to the Secondary of a Binary Asteroid
Ethical Standards for Publication of Aeronautics and Astronautics Research
Improvement to the Implementation of the QUEST Algorithm
Three-Dimensional Particle Tracing Analysis of a Rotational Magnetic Sail
Additive Manufacturing of Lightweight, Optimized, Metallic Components Suitable for Space Flight
Ethical Standards for Publication of Aeronautics and Astronautics Research
Ethical Standards for Publication of Aeronautics and Astronautics Research