nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
1 |
Ablation characteristics and reaction mechanism of insulation materials under slag deposition condition
|
Guan, Yiwen |
|
2017 |
136 |
C |
p. 80-89 |
artikel |
2 |
Ablation spot area and impulse characteristics of polymers induced by burst irradiation of 1µm laser pulses
|
Tsuruta, Hisashi |
|
2017 |
136 |
C |
p. 46-54 |
artikel |
3 |
Aluminum agglomeration involving the second mergence of agglomerates on the solid propellants burning surface: Experiments and modeling
|
Ao, Wen |
|
2017 |
136 |
C |
p. 219-229 |
artikel |
4 |
Analysis of orbit determination from Earth-based tracking for relay satellites in a perturbed areostationary orbit
|
Romero, P. |
|
2017 |
136 |
C |
p. 434-442 |
artikel |
5 |
A new concept of space solar power satellite
|
Li, Xun |
|
2017 |
136 |
C |
p. 182-189 |
artikel |
6 |
Asteroid deflection using a spacecraft in restricted keplerian motion
|
Ketema, Yohannes |
|
2017 |
136 |
C |
p. 64-79 |
artikel |
7 |
A wall grid scale criterion for hypersonic aerodynamic heating calculation
|
Yang, Jianlong |
|
2017 |
136 |
C |
p. 137-143 |
artikel |
8 |
Cruise status of Hayabusa2: Round trip mission to asteroid 162173 Ryugu
|
Tsuda, Yuichi |
|
2017 |
136 |
C |
p. 176-181 |
artikel |
9 |
Design for CubeSat-based dust and radiation studies at Europa
|
Goel, Ashish |
|
2017 |
136 |
C |
p. 204-218 |
artikel |
10 |
Diamagnetic antimatter storage
|
Semyonov, Oleg G. |
|
2017 |
136 |
C |
p. 190-203 |
artikel |
11 |
Dynamics and mixing mechanism of transverse jet injection into a supersonic combustor with cavity flameholder
|
Liu, Chaoyang |
|
2017 |
136 |
C |
p. 90-100 |
artikel |
12 |
Effect of static shape deformation on aerodynamics and aerothermodynamics of hypersonic inflatable aerodynamic decelerator
|
Guo, Jinghui |
|
2017 |
136 |
C |
p. 421-433 |
artikel |
13 |
Finite time attitude takeover control for combination via tethered space robot
|
Lu, Yingbo |
|
2017 |
136 |
C |
p. 9-21 |
artikel |
14 |
Finite time coordinated formation control for spacecraft formation flying under directed communication topology
|
Ran, Dechao |
|
2017 |
136 |
C |
p. 125-136 |
artikel |
15 |
High accuracy GNSS based navigation in GEO
|
Capuano, Vincenzo |
|
2017 |
136 |
C |
p. 332-341 |
artikel |
16 |
IFC - Publication Information
|
|
|
2017 |
136 |
C |
p. IFC |
artikel |
17 |
Ignition kinetics of boron in primary combustion products of propellant based on its unique characteristics
|
Ao, Wen |
|
2017 |
136 |
C |
p. 450-458 |
artikel |
18 |
In-situ grown MgO-ZnO ceramic coating with high thermal emittance on Mg alloy by plasma electrolytic oxidation
|
Li, Hang |
|
2017 |
136 |
C |
p. 230-235 |
artikel |
19 |
Kinematic accuracy and dynamic performance of a simple planar space deployable mechanism with joint clearance considering parameter uncertainty
|
Li, Junlan |
|
2017 |
136 |
C |
p. 34-45 |
artikel |
20 |
Long-range AIS message analysis based on the TianTuo-3 micro satellite
|
Li, Shiyou |
|
2017 |
136 |
C |
p. 159-165 |
artikel |
21 |
Method of interplanetary trajectory optimization for the spacecraft with low thrust and swing-bys
|
Konstantinov, M.S. |
|
2017 |
136 |
C |
p. 297-311 |
artikel |
22 |
Modeling of aerodynamic heat flux and thermoelastic behavior of nose caps of hypersonic vehicles
|
Persova, Marina G. |
|
2017 |
136 |
C |
p. 312-331 |
artikel |
23 |
Multi-objective trajectory optimization of Space Manoeuvre Vehicle using adaptive differential evolution and modified game theory
|
Chai, Runqi |
|
2017 |
136 |
C |
p. 273-280 |
artikel |
24 |
Nonablative lightweight thermal protection system for Mars Aeroflyby Sample collection mission
|
Suzuki, Toshiyuki |
|
2017 |
136 |
C |
p. 407-420 |
artikel |
25 |
Nose-to-tail analysis of an airbreathing hypersonic vehicle using an in-house simplified tool
|
Piscitelli, Filomena |
|
2017 |
136 |
C |
p. 148-158 |
artikel |
26 |
Numerical investigation of switching mechanism for the supersonic jet element
|
Xu, Y. |
|
2017 |
136 |
C |
p. 342-353 |
artikel |
27 |
Numerical simulations on unsteady operation processes of N2O/HTPB hybrid rocket motor with/without diaphragm
|
Zhang, Shuai |
|
2017 |
136 |
C |
p. 115-124 |
artikel |
28 |
On the advantages of exploiting the hierarchical structure of astrodynamical models
|
Dei Tos, Diogene Alessandro |
|
2017 |
136 |
C |
p. 236-247 |
artikel |
29 |
Optimal capture occasion determination and trajectory generation for space robots grasping tumbling objects
|
Luo, Jianjun |
|
2017 |
136 |
C |
p. 380-386 |
artikel |
30 |
Optimal thrust level for orbit insertion
|
Cerf, Max |
|
2017 |
136 |
C |
p. 55-63 |
artikel |
31 |
Protection of surface assets on Mars from wind blown jettisoned spacecraft components
|
Paton, Mark |
|
2017 |
136 |
C |
p. 395-406 |
artikel |
32 |
Research into topology optimization and the FDM method for a space cracked membrane
|
Hu, Qingxi |
|
2017 |
136 |
C |
p. 443-449 |
artikel |
33 |
Robust distributed control of spacecraft formation flying with adaptive network topology
|
Shasti, Behrouz |
|
2017 |
136 |
C |
p. 281-296 |
artikel |
34 |
Robust, fast and accurate vision-based localization of a cooperative target used for space robotic arm
|
Wen, Zhuoman |
|
2017 |
136 |
C |
p. 101-114 |
artikel |
35 |
Robust high-precision attitude control for flexible spacecraft with improved mixed H 2/H ∞ control strategy under poles assignment constraint
|
Liu, Chuang |
|
2017 |
136 |
C |
p. 166-175 |
artikel |
36 |
Robust spacecraft attitude tracking control using hybrid actuators with uncertainties
|
Cao, Xibin |
|
2017 |
136 |
C |
p. 1-8 |
artikel |
37 |
Self-calibration rank filter for unknown dynamic inputs mitigation during the Mars powered descent phase
|
Xiao, Qiang |
|
2017 |
136 |
C |
p. 360-368 |
artikel |
38 |
Strategies to utilize advanced heat shield technology for high-payload mars atmospheric entry missions
|
Braun, Max |
|
2017 |
136 |
C |
p. 22-33 |
artikel |
39 |
Study of the unsteady mode transition process for an over-under TBCC exhaust system
|
Lv, Zheng |
|
2017 |
136 |
C |
p. 259-272 |
artikel |
40 |
Study on atomization and combustion characteristics of LOX/methane pintle injectors
|
Fang, Xin-xin |
|
2017 |
136 |
C |
p. 369-379 |
artikel |
41 |
The final year of the Rosetta mission
|
Accomazzo, Andrea |
|
2017 |
136 |
C |
p. 354-359 |
artikel |
42 |
Thermal design and validation of radiation detector for the ChubuSat-2 micro-satellite with high-thermal-conductive graphite sheets
|
Park, Daeil |
|
2017 |
136 |
C |
p. 387-394 |
artikel |
43 |
Thermal protection performance of magnetohydrodynamic heat shield system based on multipolar magnetic field
|
Kai, Li |
|
2017 |
136 |
C |
p. 248-258 |
artikel |
44 |
The ultimate limits of the relativistic rocket equation. The Planck photon rocket
|
Haug, Espen Gaarder |
|
2017 |
136 |
C |
p. 144-147 |
artikel |