| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
Aleksandr Arkad'evich Krasovskii
|
|
|
2003
|
41 |
5 |
p. 425-426
2 p.
|
artikel
|
| 2 |
Aleksandr Arkad'evich Krasovskii
|
|
|
2003
|
41 |
5 |
p. 425-426
|
artikel
|
| 3 |
Application of the Method of Integral Manifolds for Construction of Resonant Curves for the Problem of Spacecraft Entry into the Atmosphere
|
Yu. M. Zabolotnov
|
|
2003
|
41 |
5 |
p. 453-459
7 p.
|
artikel
|
| 4 |
Application of the Method of Integral Manifolds for Construction of Resonant Curves for the Problem of Spacecraft Entry into the Atmosphere
|
Zabolotnov, Yu. M.
|
|
2003
|
41 |
5 |
p. 453-459
|
artikel
|
| 5 |
Determination of Parameters of the Model of Inherent Drifts for a Gyro-Stabilized Platform Using Information Criteria
|
V. A. Pogorelov
|
|
2003
|
41 |
5 |
p. 477-484
8 p.
|
artikel
|
| 6 |
Determination of Parameters of the Model of Inherent Drifts for a Gyro-Stabilized Platform Using Information Criteria
|
Pogorelov, V. A.
|
|
2003
|
41 |
5 |
p. 477-484
|
artikel
|
| 7 |
Determination of Typical Dimensions of the IMF Solar Wind Tube Structures on September 8, 1973, Using the Data of the Mars-7 Automatic Interplanetary Station
|
G. P. Lyubimov
|
|
2003
|
41 |
5 |
p. 517-520
4 p.
|
artikel
|
| 8 |
Determination of Typical Dimensions of the IMF Solar Wind Tube Structures on September 8, 1973, Using the Data of the Mars-7 Automatic Interplanetary Station
|
Lyubimov, G. P.
|
|
2003
|
41 |
5 |
p. 517-520
|
artikel
|
| 9 |
Dimensions of Microparticles Trapped by the Earth's Magnetic Field at Various Geomagnetic Activity Levels
|
E. K. Kolesnikov
|
|
2003
|
41 |
5 |
p. 526-527
2 p.
|
artikel
|
| 10 |
Dimensions of Microparticles Trapped by the Earth's Magnetic Field at Various Geomagnetic Activity Levels
|
Kolesnikov, E. K.
|
|
2003
|
41 |
5 |
p. 526-527
|
artikel
|
| 11 |
Effect of Microaccelerations on the Distribution of a Dopant in a Semiconductor Melt during Space Flight
|
S. A. Nikitin
|
|
2003
|
41 |
5 |
p. 502-516
15 p.
|
artikel
|
| 12 |
Effect of Microaccelerations on the Distribution of a Dopant in a Semiconductor Melt during Space Flight
|
Nikitin, S. A.
|
|
2003
|
41 |
5 |
p. 502-516
|
artikel
|
| 13 |
Experiment NORT onboard the International Space Station (ISS)
|
G. A. Avanesov
|
|
2003
|
41 |
5 |
p. 521-525
5 p.
|
artikel
|
| 14 |
Experiment NORT onboard the International Space Station (ISS)
|
Avanesov, G. A.
|
|
2003
|
41 |
5 |
p. 521-525
|
artikel
|
| 15 |
Information Support for a Low-Orbit Spacecraft Using Magnetometer and Solar Sensor Readings
|
A. I. Tkachenko
|
|
2003
|
41 |
5 |
p. 485-493
9 p.
|
artikel
|
| 16 |
Information Support for a Low-Orbit Spacecraft Using Magnetometer and Solar Sensor Readings
|
Tkachenko, A. I.
|
|
2003
|
41 |
5 |
p. 485-493
|
artikel
|
| 17 |
Qualitative Properties of Orbits for Minimum-Fuel Impulsive Transfers between Circular Coplanar Orbits with a Given Launch Time
|
S. N. Kirpichnikov
|
|
2003
|
41 |
5 |
p. 443-452
10 p.
|
artikel
|
| 18 |
Qualitative Properties of Orbits for Minimum-Fuel Impulsive Transfers between Circular Coplanar Orbits with a Given Launch Time
|
Kirpichnikov, S. N.
|
|
2003
|
41 |
5 |
p. 443-452
|
artikel
|
| 19 |
Risk Factors of Negative Impact on Objects of the Environment upon Accidents during Launches of Rocket-Space Hardware
|
V. I. Romanov
|
|
2003
|
41 |
5 |
p. 494-501
8 p.
|
artikel
|
| 20 |
Risk Factors of Negative Impact on Objects of the Environment upon Accidents during Launches of Rocket-Space Hardware
|
Romanov, V. I.
|
|
2003
|
41 |
5 |
p. 494-501
|
artikel
|
| 21 |
Solar Probe Mission with Multiple Gravity-Assist Maneuvers Realized with Conversion Launchers
|
V. V. Malyshev
|
|
2003
|
41 |
5 |
p. 431-442
12 p.
|
artikel
|
| 22 |
Solar Probe Mission with Multiple Gravity-Assist Maneuvers Realized with Conversion Launchers
|
Malyshev, V. V.
|
|
2003
|
41 |
5 |
p. 431-442
|
artikel
|
| 23 |
Spacecraft Injection into a Heliocentric Terrestrial Orbit
|
V. G. Kurt
|
|
2003
|
41 |
5 |
p. 427-431
5 p.
|
artikel
|
| 24 |
Spacecraft Injection into a Heliocentric Terrestrial Orbit
|
Kurt, V. G.
|
|
2003
|
41 |
5 |
p. 427-431
|
artikel
|
| 25 |
The Use of Quaternions in the Optimal Control Problems of Motion of the Center of Mass of a Spacecraft in a Newtonian Gravitational Field: III
|
Yu. N. Chelnokov
|
|
2003
|
41 |
5 |
p. 460-477
18 p.
|
artikel
|
| 26 |
The Use of Quaternions in the Optimal Control Problems of Motion of the Center of Mass of a Spacecraft in a Newtonian Gravitational Field: III
|
Chelnokov, Yu. N.
|
|
2003
|
41 |
5 |
p. 460-477
|
artikel
|
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