| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
Advanced space system for geostationary orbit surveillance
|
Klimenko, N. N.
|
|
2016
|
50 |
7 |
p. 575-580
|
artikel
|
| 2 |
A new generation of spacecraft pyroautomatic systems as a result of a successful cooperation
|
Kotomin, A. A.
|
|
2016
|
50 |
7 |
p. 546-551
|
artikel
|
| 3 |
Celestial-mechanical interpretation of the two-way radio measurements of radial velocity of spacecraft for scientific applications
|
Komovkin, S. V.
|
|
2016
|
50 |
7 |
p. 593-596
|
artikel
|
| 4 |
Choosing an efficient option of the combined propulsion system and flight profile of the INTERHELIO-PROBE spacecraft
|
Platov, I. V.
|
|
2016
|
50 |
7 |
p. 581-586
|
artikel
|
| 5 |
Computational and theoretical investigation of Mars’s atmospheric impact on the descent module “Exomars-2018” under aerodynamic deceleration
|
Golomazov, M. M.
|
|
2016
|
50 |
7 |
p. 498-507
|
artikel
|
| 6 |
From the Vega mission to comet Halley to the Rosetta mission to comet 67/P Churyumov–Gerasimenko
|
Zelenyi, L. M.
|
|
2016
|
50 |
7 |
p. 451-463
|
artikel
|
| 7 |
Laws of attenuation of axially symmetrical shock waves in shells of detonating extended charges
|
Kuzin, E. N.
|
|
2016
|
50 |
7 |
p. 508-514
|
artikel
|
| 8 |
Linearization methods for optimizing the low thrust spacecraft trajectory: Theoretical aspects
|
Kazmerchuk, P. V.
|
|
2016
|
50 |
7 |
p. 587-592
|
artikel
|
| 9 |
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
|
Golubev, Yu. F.
|
|
2016
|
50 |
7 |
p. 597-603
|
artikel
|
| 10 |
Method of predictive studies of the effectiveness of spacecraft modifications with integrated subsystem replacement
|
Matveev, Yu. A.
|
|
2016
|
50 |
7 |
p. 604-610
|
artikel
|
| 11 |
Methods and means of information-analytical assessment of asteroid and comet hazard
|
Kulagin, V. P.
|
|
2016
|
50 |
7 |
p. 464-470
|
artikel
|
| 12 |
On the problem of designing small spacecraft with electric propulsion power plants for studying minor bodies of the Solar System
|
Kulkov, V. M.
|
|
2016
|
50 |
7 |
p. 533-539
|
artikel
|
| 13 |
Optimization of the interplanetary trajectories of spacecraft with a solar electric propulsion power plant of minimal power
|
Ivanyukhin, A. V.
|
|
2016
|
50 |
7 |
p. 552-559
|
artikel
|
| 14 |
Positioning and control of the orbital structure of the Arktika-M innovative space system (marking the 50 years of Lavochkin Association’s space activities)
|
Nazarov, A. E.
|
|
2016
|
50 |
7 |
p. 568-574
|
artikel
|
| 15 |
Preliminary design of pseudo satellites: Basic methods and feasibility criteria
|
Klimenko, N. N.
|
|
2016
|
50 |
7 |
p. 523-532
|
artikel
|
| 16 |
Problems of design and development of advanced superheavy launch vehicles
|
Daniluk, A. Yu.
|
|
2016
|
50 |
7 |
p. 515-522
|
artikel
|
| 17 |
Proposals for the construction of space systems based on small spacecraft and a transport and power module with a nuclear power plant
|
Barabanov, A. A.
|
|
2016
|
50 |
7 |
p. 471-476
|
artikel
|
| 18 |
Requirements for the appearance and basic design parameters of a micro-rocket system meant for launching nano-, pico, and femtoscale spacecraft
|
Daniluk, A. Yu.
|
|
2016
|
50 |
7 |
p. 477-483
|
artikel
|
| 19 |
Solving the problem of shock wave attenuation in an obstacle during a contact explosion of a high-energy material charge
|
Kuzin, E. N.
|
|
2016
|
50 |
7 |
p. 484-488
|
artikel
|
| 20 |
The analysis of ballistic capabilities for countering disturbances associated with temporary emergency electric propulsion shutdown
|
Konstantinov, M. S.
|
|
2016
|
50 |
7 |
p. 560-567
|
artikel
|
| 21 |
The onboard control system of “Navigator” platform
|
Syrov, A. S.
|
|
2016
|
50 |
7 |
p. 540-545
|
artikel
|
| 22 |
Transformable descent vehicles
|
Pichkhadze, K. M.
|
|
2016
|
50 |
7 |
p. 489-497
|
artikel
|
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