| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
A deep neural network framework with Analytic Continuation for predicting hypervelocity fragment flyout from satellite explosions
|
Larsen, Katharine E.
|
|
|
226 |
P2 |
p. 87-101
|
artikel
|
| 2 |
Analysis and control of the equilibrium position in bare electrodynamic tether systems
|
Xie, Mingze
|
|
|
226 |
P2 |
p. 60-70
|
artikel
|
| 3 |
Analytic solution for combined in-plane and out-of-plane spacecraft formation reconfiguration with passive collision avoidance
|
Xu, Chenglong
|
|
|
226 |
P2 |
p. 48-59
|
artikel
|
| 4 |
Comprehensive parametric model and decoupling design of a Stewart platform for a large spaceborne optical load
|
Du, Longfei
|
|
|
226 |
P2 |
p. 119-134
|
artikel
|
| 5 |
Editorial Board
|
|
|
|
226 |
P2 |
p. ii
|
artikel
|
| 6 |
Effect of aluminum nanoparticles size and concentration on the combustion characteristics of nanofluid fuel: Experiments and modeling
|
Zhou, Shuai
|
|
|
226 |
P2 |
p. 149-161
|
artikel
|
| 7 |
Effects of particle size on the magnetic cleaning system for manned lunar explorations
|
Adachi, Masato
|
|
|
226 |
P2 |
p. 23-30
|
artikel
|
| 8 |
Habitat site selection on Mars: Suitability analysis and mapping
|
Zhu, Sijie
|
|
|
226 |
P2 |
p. 1-22
|
artikel
|
| 9 |
In-orbit system identification of a flexible satellite with variable mass using dual Unscented Kalman filters
|
Elliott, Alex J.
|
|
|
226 |
P2 |
p. 71-86
|
artikel
|
| 10 |
MaiaSpace: Sustainability applied to the development of a semi-reusable solution for space mobility
|
Vila, Jérôme
|
|
|
226 |
P2 |
p. 31-38
|
artikel
|
| 11 |
On periodic modes of motion of a vibrating robot in a horizontal plane with anisotropic friction
|
Shamin, A.Y.
|
|
|
226 |
P2 |
p. 113-118
|
artikel
|
| 12 |
Publisher's note
|
|
|
|
226 |
P2 |
p. iii
|
artikel
|
| 13 |
Scheme and trajectory design of in-situ atmospheric sampling with multi-pass aeroassisted maneuvers
|
Feng, Xiangdong
|
|
|
226 |
P2 |
p. 135-148
|
artikel
|
| 14 |
Simulation of rarefied gas flow inside the satellite air intake in ultra-low Earth orbit
|
Yakunchikov, Artem
|
|
|
226 |
P2 |
p. 102-112
|
artikel
|
| 15 |
The Deployment Mechanism of the E.T.PACK Deorbit System: Functional and Qualification tests
|
Brunello, A.
|
|
|
226 |
P2 |
p. 39-47
|
artikel
|
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