Vol. 50, No. 7, 2016
A simultaneous English language translation of this journal is available from Pleiades Publishing, Ltd.
Distributed worldwide by Springer. Solar System Research ISSN 0038-0946.
From the Vega Mission To Comet Halley to the Rosetta Mission to Comet 67/P Churyumov–Gerasimenko
p. 451 abstract
Methods and Means of Information-Analytical Assessment of Asteroid and Comet Hazard
p. 464 abstract
Proposals for the Construction of Space Systems Based on Small Spacecraft and a Transport and Power Module with a Nuclear Power Plant
p. 471 abstract
Requirements for the Appearance and Basic Design Parameters of a Micro-Rocket System Meant for Launching Nano-, Pico, and Femtoscale Spacecraft
p. 477 abstract
Solving the Problem of Shock Wave Attenuation in an Obstacle during a Contact Explosion of a High-Energy Material Charge
p. 484 abstract
Transformable Descent Vehicles
p. 489 abstract
Computational and Theoretical Investigation of Mars’s Atmospheric Impact on the Descent Module “Exomars-2018” under Aerodynamic Deceleration
p. 498 abstract
Laws of Attenuation of Axially Symmetrical Shock Waves in Shells of Detonating Extended Charges
p. 508 abstract
Problems of Design and Development of Advanced Superheavy Launch Vehicles
p. 515 abstract
Preliminary Design of Pseudo Satellites: Basic Methods and Feasibility Criteria
p. 523 abstract
On the Problem of Designing Small Spacecraft with Electric Propulsion Power Plants for Studying Minor Bodies of the Solar System
p. 533 abstract
The Onboard Control System of “Navigator” Platform
p. 540 abstract
A New Generation of Spacecraft Pyroautomatic Systems as a Result of a Successful Cooperation
p. 546 abstract
Optimization of the Interplanetary Trajectories of Spacecraft with a Solar Electric Propulsion Power Plant of Minimal Power
p. 552 abstract
The Analysis of Ballistic Capabilities for Countering Disturbances Associated with Temporary Emergency Electric Propulsion Shutdown
p. 560 abstract
Positioning and Control of the Orbital Structure of the Arktika-M Innovative Space System (Marking the 50 years of Lavochkin Association’s Space Activities)
p. 568 abstract
Advanced Space System for Geostationary Orbit Surveillance
p. 575 abstract
Choosing an Efficient Option of the Combined Propulsion System and Flight Profile of the INTERHELIO-PROBE Spacecraft
p. 581 abstract
Linearization Methods for Optimizing the Low Thrust Spacecraft Trajectory: Theoretical Aspects
p. 587 abstract
Celestial-Mechanical Interpretation of the Two-Way Radio Measurements of Radial Velocity of Spacecraft for Scientific Applications
p. 593 abstract
Main Methods of Trajectory Synthesis for Scenarios of Space Missions with Gravity Assist Maneuvers in the System of Jupiter and with Landing on One of Its Satellites
p. 597 abstract
Method of Predictive Studies of the Effectiveness of Spacecraft Modifications with Integrated Subsystem Replacement
p. 604 abstract