Deorbiting Performance of Bare Electrodynamic Tethers in Inclined Orbits
Algebraic Approach to the Minimum-Cost Multi-Impulse Orbit-Transfer Problem
Mass Ratio of Electrodynamic Tether to Spacecraft on Deorbit Stability and Efficiency
Science Orbits with an Inner Disturbing Body and an Outer Disturbing Body
Precise Analysis of Deorbiting by Electrodynamic Tethers Using Coupled Multiphysics Finite Elements
Analytical Modeling Framework and Applications for Space Communication Networks
Spacecraft Demand Tasking and Skip Entry Responsive Maneuvers
The Operation of Molyniya Communications Satellites
Analysis of the Orbit of Cosmos 268 Rocket (1969-20B)
Optimum Orbit Plane Change Using a Skip Reentry Trajectory for the Space Shuttle Orbiter
Energetic Radiation Environment in a Highly Elliptical (Molniya) Orbit
Use of an Aerodynamic Turn to Maximize the Orbit Inclination Change for the Space Shuttle Orbiter
Aerospace Applications of Navigation Satellites
The Orbital Elements of Cosmos 2 for April-June, 1962
The Variation in the Orbit of Cosmos 97 Rocket Throughout Its Life