Use of an Aerodynamic Turn to Maximize the Orbit Inclination Change for the Space Shuttle Orbiter
The Variation in the Orbit of Cosmos 97 Rocket Throughout Its Life
The Orbital Elements of Cosmos 2 for April-June, 1962
The Operation of Molyniya Communications Satellites
Technical Challenges of Integration of Space and Terrestrial Systems
Spacecraft Demand Tasking and Skip Entry Responsive Maneuvers
Science Orbits with an Inner Disturbing Body and an Outer Disturbing Body
Satellite Orbits for Communications Satellites
Precise Analysis of Deorbiting by Electrodynamic Tethers Using Coupled Multiphysics Finite Elements
Optimum Orbit Plane Change Using a Skip Reentry Trajectory for the Space Shuttle Orbiter
Mass Ratio of Electrodynamic Tether to Spacecraft on Deorbit Stability and Efficiency
Lifetime Testing, Redundancy, Reliability, and Mean Time to Failure
Investigation of Atmospheric Reentry for the Space Maneuver Vehicle
Energetic Radiation Environment in a Highly Elliptical (Molniya) Orbit
Deorbiting Performance of Bare Electrodynamic Tethers in Inclined Orbits