Vol. 54, No. 7, 2020
“Bumerang” Must Return to Earth
p. 567 abstract
On the Dynamics of Atmospheric Gas Filling the Interior of a Prospective Descent Module During Descent in the Atmosphere of Mars
p. 574 abstract
Mathematical Model of the Motion of Gaseous Thermal Decomposition Products of Composites in a Porous Frame under Strong Heat Flows
p. 582 abstract
Meteor Hazard for Interplanetary Flights in the Ecliptic Plane
p. 587 abstract
On the Use of Inflatable Decelerators in the Design of Spacecraft Intended for the Study of Venus
p. 595 abstract
System Problems in the Development of Ultralight-Class Launch Vehicles
p. 603 abstract
Analysis of Key Technologies for a Space Geophysics Mission: Required Accuracies and Engineering Solutions
p. 610 abstract
Equivalent Flux Function Smoothing in the Problem of Solar Cells Radiation Degradation Minimization During a Low-Thrust Geostationary Orbit Insertion
p. 621 abstract
Determination of the Thermophysical Characteristics of the Lunar Soil Using Solar Heat
p. 630 abstract
A Concept for Designing a System for a Double-Launch Spacecraft System as Part of the Upper Stages of the Fregat
p. 637 abstract
Features of Lunar Rover Design Considering Radiation Effects from Outer Space and Onboard Radioisotope Heat Sources
p. 646 abstract
Optimization of the Return Trajectories from the Moon for Delivering Soil to a Specified Region on the Earth’s Surface
p. 654 abstract
A New Way of Automated Dust Control of the External Atmosphere of a Spacecraft During Thermal-Vacuum Testing
p. 662 abstract
A Model for Initiating Impulse Development and Transition in Small Detonation Devices
p. 668 abstract
Reduction of Hydraulic Losses in a Pebble-Bed Reactor for Nuclear Power Propulsion Systems for Advanced Spacecraft
p. 673 abstract
Atmospheric Modeling for Controlling the Motion of a Return Vehicle
p. 679 abstract
Conceptual Design of the Chinese-Russian On-Orbit-Assembling Space Telescope (OAST)
p. 685 abstract
Implementation of the Concept for Creating a Spacecraft Double-Launch System as a Part of the Upper Stages of the Fregat Family
p. 690 abstract
Linearization Method for Optimizing Noncoplanar Flights with Low Thrust
p. 699 abstract
On the Development of Transformable Structures of Space Telescopes
p. 707 abstract
The Numerical Simulation of Aerodynamics of the Frontal Aerodynamic Screen of ExoMars Project Descent Vehicle and the Analysis of Flow Pattern in the Base Area and Near Wake
p. 712 abstract
On the Calculation of the Geometric Resolution and Energy Potential of a Bistatic Synthetic Aperture Radar in Geosynchronous Orbit
p. 719 abstract
Development of Technology for Soldering Small-Diameter Pipelines from Aluminum Alloys and Dissimilar Materials
p. 730 abstract