Vol. 61, No. 5, 2023
Optimization of the Maneuver to Ensure a High Velocity of the Spacecraft Entry into the Atmosphere
p. 353 abstract
Statistical Characteristics of Emission from Stationary Plasma Thrusters Operating with Various Propellants
p. 357 abstract
Study of Cosmic Ray Intensity (CRI) along with Solar Wind Parameters and Geomagnetic Indices from Different Stations
p. 364 abstract
Designing Low-Energy Low-Thrust Flight to the Moon on a Temporary Capture Trajectory
p. 380 abstract
A Method for Calculating the Trajectory of a Single-Impulse Flight to a Halo Orbit around the L2 Libration Point of the Earth–Moon System
p. 394 abstract
Propellant Influence on Electromagnetic Environment Generated by Stationary Plasma Thrusters
p. 405 abstract
The Problem of Optimal Discharge Energy in an Ablative Pulsed Plasma Thruster
p. 412 abstract
Optimization of a Low-Thrust Heliocentric Trajectory between the Collinear Libration Points of Different Planets
p. 418 abstract
Optimization of the Spacecraft Transfer Maneuver from a Point of the Elliptical Orbit to Another Point of the Same Orbit
p. 431 abstract
An Experimental Study of an Ion Thruster with Electrodes of an Ion-Extraction System Made of a Fine-Structure Carbon–Carbon Composite
p. 449 abstract
Erratum to: Stability of a Magnetically Actuated Satellite towards the Sun on a Sun-Synchronous Orbit
p. 454 abstract
Erratum to: Space–Time Structures in the Auroral Oval: Approaches to Modeling
p. 455 abstract
Erratum to: High-Cadence Observations of Magnetic Field Dynamics and Photospheric Emission Sources in the Eruptive Near-the-Limb X4.9 Solar Flare on 25 February, 2014: Evidences for Two-Stage Magnetic Reconnection during the Impulsive Phase
p. 456 abstract