nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
1 |
Changes of properties of the materials of spacecraft solar arrays under the action of atomic oxygen
|
Shuvalov, V. A. |
|
|
45 |
4 |
p. 294-304 |
artikel |
2 |
Changes of properties of the materials of spacecraft solar arrays under the action of atomic oxygen
|
Shuvalov, V. A. |
|
2007 |
45 |
4 |
p. 294-304 |
artikel |
3 |
Combined equations of motion for description of dynamics of spacecraft docking using the pin-cone system
|
Yaskevich, A. V. |
|
2007 |
45 |
4 |
p. 305-316 |
artikel |
4 |
Dynamics of ion energy-dispersed structures near the plasma sheet outer boundary
|
Kovrazhkin, R. A. |
|
2007 |
45 |
4 |
p. 287-293 |
artikel |
5 |
Features of rotational motion of a spacecraft descending in the Martian atmosphere
|
Aslanov, V. S. |
|
2007 |
45 |
4 |
p. 331-338 |
artikel |
6 |
First results of investigating the space environment onboard the Universitetskii-Tatyana satellite
|
Sadovnichy, V. A. |
|
2007 |
45 |
4 |
p. 273-286 |
artikel |
7 |
Intensity enhancements of 200–2000 MeV protons in 1997–2005 as measured by the KET/ULYSSES
|
Struminsky, A. B. |
|
2007 |
45 |
4 |
p. 368-372 |
artikel |
8 |
Measurement of the spectrum of relativistic protons from solar flares on October 28 and November 2, 2003 onboard the CORONAS-F satellite
|
Kuznetsov, S. N. |
|
|
45 |
4 |
p. 373-375 |
artikel |
9 |
Measurement of the spectrum of relativistic protons from solar flares on October 28 and November 2, 2003 onboard the CORONAS-F satellite
|
Kuznetsov, S. N. |
|
2007 |
45 |
4 |
p. 373-375 |
artikel |
10 |
Robust algorithm of control for a maneuver in the Martian atmosphere to insert a spacecraft into the planet’s satellite orbit
|
Sikharulidze, Yu. G. |
|
2007 |
45 |
4 |
p. 317-330 |
artikel |
11 |
Some new applications of the generalized problem of two fixed centers
|
Kochetkova, A. Yu. |
|
2007 |
45 |
4 |
p. 354-358 |
artikel |
12 |
Stochastic motion of geosynchronous satellites
|
Kuznetsov, E. D. |
|
2007 |
45 |
4 |
p. 359-367 |
artikel |
13 |
The use of solutions to problems of spacecraft trajectory optimization in impulse formulation when solving the problems of optimal control of trajectories of a spacecraft with limited thrust engine: I
|
Grigoriev, I. S. |
|
2007 |
45 |
4 |
p. 339-347 |
artikel |
14 |
Variational equations in parametric variables and transformation of their solutions
|
Shefer, V. A. |
|
2007 |
45 |
4 |
p. 348-353 |
artikel |