| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
Active subspace approach to reliability and safety assessments of small satellite separation
|
Hu, Xingzhi
|
|
2017
|
131 |
C |
p. 159-165
7 p.
|
artikel
|
| 2 |
Antarctic station life: The first 15 years of mixed expeditions to the Antarctic
|
Sarris, Aspa
|
|
2017
|
131 |
C |
p. 50-54
5 p.
|
artikel
|
| 3 |
A study of performance parameters on drag and heat flux reduction efficiency of combinational novel cavity and opposing jet concept in hypersonic flows
|
Sun, Xi-wan
|
|
2017
|
131 |
C |
p. 204-225
22 p.
|
artikel
|
| 4 |
Autonomous shooting at middle size space debris objects from space-based APT laser systems
|
Gambi, J.M.
|
|
2017
|
131 |
C |
p. 83-91
9 p.
|
artikel
|
| 5 |
Considering the collision probability of Active Debris Removal missions
|
Lidtke, Aleksander A.
|
|
2017
|
131 |
C |
p. 10-17
8 p.
|
artikel
|
| 6 |
Corrigendum to “Dynamic modeling and optimization for space logistics using time-expanded networks” [Acta Astronaut. 105 (2014) 428–443]
|
Ho, Koki
|
|
2017
|
131 |
C |
p. 226-
1 p.
|
artikel
|
| 7 |
Cosmic radiation measurements on the Foton-M4 satellite by passive detectors
|
Strádi, Andrea
|
|
2017
|
131 |
C |
p. 110-112
3 p.
|
artikel
|
| 8 |
Development of a low-cost, low micro-vibration CMG for small agile satellite applications
|
Kawak, B.J.
|
|
2017
|
131 |
C |
p. 113-122
10 p.
|
artikel
|
| 9 |
Development of a Martian regolith simulant for in-situ resource utilization testing
|
Scott, A.N.
|
|
2017
|
131 |
C |
p. 45-49
5 p.
|
artikel
|
| 10 |
Drilling forces model for lunar regolith exploration and experimental validation
|
Zhang, Tao
|
|
2017
|
131 |
C |
p. 190-203
14 p.
|
artikel
|
| 11 |
Dynamic analysis and control of novel moving mass flight vehicle
|
Li, Jianqing
|
|
2017
|
131 |
C |
p. 36-44
9 p.
|
artikel
|
| 12 |
Dynamic analysis of the deployment for mesh reflector deployable antennas with the cable-net structure
|
Zhang, Yiqun
|
|
2017
|
131 |
C |
p. 182-189
8 p.
|
artikel
|
| 13 |
High-accuracy optimal finite-thrust trajectories for Moon escape
|
Shen, Hong-Xin
|
|
2017
|
131 |
C |
p. 102-109
8 p.
|
artikel
|
| 14 |
IFC - Publication Information
|
|
|
2017
|
131 |
C |
p. IFC-
1 p.
|
artikel
|
| 15 |
Inertial parameter identification using contact force information for an unknown object captured by a space manipulator
|
Chu, Zhongyi
|
|
2017
|
131 |
C |
p. 69-82
14 p.
|
artikel
|
| 16 |
Innovative viscoelastic material selection strategy based on dma and mini-shaker tests for spacecraft applications
|
Kawak, B.J.
|
|
2017
|
131 |
C |
p. 18-27
10 p.
|
artikel
|
| 17 |
Interactions of the space debris environment with mega constellations—Using the example of the OneWeb constellation
|
Radtke, Jonas
|
|
2017
|
131 |
C |
p. 55-68
14 p.
|
artikel
|
| 18 |
Nanosatellites in LEO and beyond: Advanced Radiation protection techniques for COTS-based spacecraft
|
Selčan, David
|
|
2017
|
131 |
C |
p. 131-144
14 p.
|
artikel
|
| 19 |
Ocean worlds exploration
|
Lunine, Jonathan I.
|
|
2017
|
131 |
C |
p. 123-130
8 p.
|
artikel
|
| 20 |
Passivity control with practically finite-time convergence for large space structures
|
Hu, Quan
|
|
2017
|
131 |
C |
p. 152-158
7 p.
|
artikel
|
| 21 |
Performance of a green propellant thruster with discharge plasma
|
Shindo, Takahiro
|
|
2017
|
131 |
C |
p. 92-95
4 p.
|
artikel
|
| 22 |
Real-time star identification using synthetic radial pattern and its hardware implementation
|
Zhao, Yang
|
|
2017
|
131 |
C |
p. 1-9
9 p.
|
artikel
|
| 23 |
The designing of launch vehicles with liquid propulsion engines ensuring fire, explosion and environmental safety requirements of worked-off stages
|
Trushlyakov, V.
|
|
2017
|
131 |
C |
p. 96-101
6 p.
|
artikel
|
| 24 |
Thrust vectoring of an electric solar wind sail with a realistic sail shape
|
Toivanen, P.
|
|
2017
|
131 |
C |
p. 145-151
7 p.
|
artikel
|
| 25 |
Underactuated spacecraft formation reconfiguration with collision avoidance
|
Huang, Xu
|
|
2017
|
131 |
C |
p. 166-181
16 p.
|
artikel
|
| 26 |
Verification of MEMS fabrication process for the application of MEMS solid propellant thruster arrays in space through launch and on-orbit environment tests
|
Oh, Hyun-Ung
|
|
2017
|
131 |
C |
p. 28-35
8 p.
|
artikel
|
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