| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
Aerodynamic design of a descent vehicle in the Martian atmosphere under the exomars project
|
Golomazov, M. M.
|
|
2014
|
48 |
7 |
p. 541-548
|
artikel
|
| 2 |
A method for a short-term forecast of the absorbed dose accumulation dynamics on the international space station based on radiation monitoring system data
|
Lishnevskii, A. E.
|
|
2014
|
48 |
7 |
p. 568-573
|
artikel
|
| 3 |
A navigation method for an automated interplanetary probe on a quasi-satellite orbit in a three-body problem based on optical measurements
|
Chulin, A. N.
|
|
2014
|
48 |
7 |
p. 574-581
|
artikel
|
| 4 |
A sensor for the spatial registration and measurement of particles parameters in near and deep space—Experimental investigation of SiO2-aerogel characteristics
|
Ivanov, N. N.
|
|
2014
|
48 |
7 |
p. 549-554
|
artikel
|
| 5 |
A strategy for developing a launch vehicle system for orbit insertion: Methodological aspects
|
Klyushnikov, V. Yu.
|
|
2014
|
48 |
7 |
p. 582-587
|
artikel
|
| 6 |
Baroresistor effect and semiconductor thin-film baroresistors based on samarium sulfide for spacecraft applications
|
Kaminskiy, V. V.
|
|
2014
|
48 |
7 |
p. 561-567
|
artikel
|
| 7 |
Combined system for the compensation of the solar pressure-induced disturbing torque for geostationary satellites
|
Shmatov, S. I.
|
|
2014
|
48 |
7 |
p. 507-514
|
artikel
|
| 8 |
Ensuring dynamic stability of the orbital structure of the Arktika-M space system
|
Nazarov, A. E.
|
|
2014
|
48 |
7 |
p. 523-530
|
artikel
|
| 9 |
Final touchdown phases and a guidance and control methodology for a soft Moon landing
|
Likhachev, V. N.
|
|
2014
|
48 |
7 |
p. 497-506
|
artikel
|
| 10 |
Joint computation of aerodynamic and radiation forces acting on spacecraft
|
Shmatov, S. I.
|
|
2014
|
48 |
7 |
p. 515-522
|
artikel
|
| 11 |
Near-Earth space as an object of global monitoring
|
Barmin, I. V.
|
|
2014
|
48 |
7 |
p. 531-535
|
artikel
|
| 12 |
On the implementation of the program for exploration of Solar System small bodies
|
Lomakin, I. V.
|
|
2014
|
48 |
7 |
p. 485-492
|
artikel
|
| 13 |
On the reduction of dynamic loads during actuation of separation devices of advanced orbital astrophysical observatories
|
Efanov, V. V.
|
|
2014
|
48 |
7 |
p. 475-479
|
artikel
|
| 14 |
Optimization of the transfer trajectory of a low-thrust spacecraft for research of Jupiter using an Earth gravity-assist maneuver
|
Konstantinov, M. S.
|
|
2014
|
48 |
7 |
p. 606-612
|
artikel
|
| 15 |
Perturbing effect of solar radiation on the Spektr-RG spacecraft in operational orbit
|
Shmatov, S. I.
|
|
2014
|
48 |
7 |
p. 601-605
|
artikel
|
| 16 |
Problem “13” for geostationary spacecraft
|
Nazarov, A. E.
|
|
2014
|
48 |
7 |
p. 588-592
|
artikel
|
| 17 |
Quality analysis of image geolocation for a space synthetic aperture radar
|
Zanin, K. A.
|
|
2014
|
48 |
7 |
p. 555-560
|
artikel
|
| 18 |
Remote method of determining the coordinates of points on a planetary surface
|
Barmin, I. V.
|
|
2014
|
48 |
7 |
p. 493-496
|
artikel
|
| 19 |
Rings of debris in near-Earth space
|
Barmin, I. V.
|
|
2014
|
48 |
7 |
p. 593-600
|
artikel
|
| 20 |
Science issues of the “Spektr-UF” project
|
Shustov, B. M.
|
|
2014
|
48 |
7 |
p. 467-474
|
artikel
|
| 21 |
Ultraviolet observatories of the future
|
Sachkov, M. E.
|
|
2014
|
48 |
7 |
p. 480-484
|
artikel
|
| 22 |
Using fracture mechanics principles for calculating the pressurized structure lifetime by example of the propellant tank for the fourth stage of launch vehicle VEGA
|
Birukov, A. S.
|
|
2014
|
48 |
7 |
p. 536-540
|
artikel
|
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