nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
1 |
Access to space: A new approach by the united nations office for outer space affairs
|
Kojima, Ayami |
|
2018 |
152 |
C |
p. 201-207 |
artikel |
2 |
Active use of solar radiation pressure for angular momentum control of the PROCYON micro-spacecraft
|
Ito, T. |
|
2018 |
152 |
C |
p. 299-309 |
artikel |
3 |
Adaptive higher order super-twisting control algorithm for a flexible air-breathing hypersonic vehicle
|
Ding, Yibo |
|
2018 |
152 |
C |
p. 275-288 |
artikel |
4 |
Adaptive prediction backstepping attitude control for liquid-filled micro-satellite with flexible appendages
|
Huo, Jun-hai |
|
2018 |
152 |
C |
p. 557-566 |
artikel |
5 |
Aerodynamic heating of inflatable aeroshell in orbital reentry
|
Takahashi, Yusuke |
|
2018 |
152 |
C |
p. 437-448 |
artikel |
6 |
A fast trajectory planning framework with task-priority for space robot
|
Luo, Jianjun |
|
2018 |
152 |
C |
p. 823-835 |
artikel |
7 |
A gradual approach towards space traffic management: The contribution of UNISAPCE+50
|
Stubbe, Peter |
|
2018 |
152 |
C |
p. 179-184 |
artikel |
8 |
A model for understanding and managing cost growth on joint programs
|
Dwyer, Morgan |
|
2018 |
152 |
C |
p. 59-70 |
artikel |
9 |
An accelerated life test model for solid lubricated bearings used in space based on time-varying dependence analysis of different failure modes
|
Zhang, Chao |
|
2018 |
152 |
C |
p. 352-359 |
artikel |
10 |
Analysis of artificial gravity paradigms using a mathematical model of spatial orientation
|
Vincent, Grant R. |
|
2018 |
152 |
C |
p. 602-610 |
artikel |
11 |
Analysis of the gas exchange and water balance in a closed experimental model of the artificial ecosystem intended for an estimated portion of a human
|
Ushakova, Sofya |
|
2018 |
152 |
C |
p. 105-111 |
artikel |
12 |
An analytical model for characterizing the thrust performance of a Low-Pressure Micro-Resistojet
|
Guerrieri, Daduí C. |
|
2018 |
152 |
C |
p. 719-726 |
artikel |
13 |
An improved energy management strategy of hybrid photovoltaic/battery/fuel cell system for stratospheric airship
|
Liao, Jun |
|
2018 |
152 |
C |
p. 727-739 |
artikel |
14 |
A novel inertial-aided feature detection model for autonomous navigation in planetary landing
|
Yu, Meng |
|
2018 |
152 |
C |
p. 667-681 |
artikel |
15 |
An overview of waverider design concept in airframe/inlet integration methodology for air-breathing hypersonic vehicles
|
Ding, Feng |
|
2018 |
152 |
C |
p. 639-656 |
artikel |
16 |
A review on enhanced mixing methods in supersonic mixing layer flows
|
Tan, Jianguo |
|
2018 |
152 |
C |
p. 310-324 |
artikel |
17 |
A review on exergy analysis of aerospace power systems
|
Dong, Zeyu |
|
2018 |
152 |
C |
p. 486-495 |
artikel |
18 |
Astroengineering, Dysonian SETI, and naturalism: A new Catch-22
|
Ćirković, Milan M. |
|
2018 |
152 |
C |
p. 289-298 |
artikel |
19 |
Attitude and vibration control with double-gimbal variable-speed control moment gyros
|
Sasaki, Takahiro |
|
2018 |
152 |
C |
p. 740-751 |
artikel |
20 |
Bounded trajectory design and self-adaptive maintenance control near non-synchronized binary systems comprised of small irregular bodies
|
Li, Xiangyu |
|
2018 |
152 |
C |
p. 768-781 |
artikel |
21 |
Capture of small near-Earth asteroids to Earth orbit using aerobraking
|
Tan, Minghu |
|
2018 |
152 |
C |
p. 185-195 |
artikel |
22 |
Combustion stabilization modes in a hydrogen-fueled scramjet combustor at high stagnation temperature
|
Wang, Yanan |
|
2018 |
152 |
C |
p. 112-122 |
artikel |
23 |
Conceptual design analysis for a two-stage-to-orbit semi-reusable launch system for small satellites
|
Maddock, Christie Alisa |
|
2018 |
152 |
C |
p. 782-792 |
artikel |
24 |
Contribution of bone micromechanical behavior beyond lamellar length scale to the macroscopic bone quality of hind limb unloading rats
|
Sun, Lian-wen |
|
2018 |
152 |
C |
p. 468-473 |
artikel |
25 |
CUTIE: A cubesats tether-inserted mission for moon exploration
|
Bettanini, C. |
|
2018 |
152 |
C |
p. 580-587 |
artikel |
26 |
Development and testing of a pyro-driven launcher for harpoon-based comet sample acquisition
|
Völk, Stefan |
|
2018 |
152 |
C |
p. 218-228 |
artikel |
27 |
Development of EVA-SEBS based wax fuel for hybrid rocket applications
|
Mengu, Dinesh |
|
2018 |
152 |
C |
p. 325-334 |
artikel |
28 |
Dynamic and static controller placement in Software-Defined Satellite Networking
|
Wu, Shuai |
|
2018 |
152 |
C |
p. 49-58 |
artikel |
29 |
Earth analogue testing and analysis of Martian duricrust properties
|
Lewinger, William |
|
2018 |
152 |
C |
p. 567-579 |
artikel |
30 |
Electrostatic-magnetic-hybrid thrust generation in central–cathode electrostatic thruster (CC–EST)
|
Sasoh, Akihiro |
|
2018 |
152 |
C |
p. 137-145 |
artikel |
31 |
Evaluation criteria for a flameless combustor based on recirculation and mixing - A CFD approach
|
Khalil, Hesham M. |
|
2018 |
152 |
C |
p. 127-136 |
artikel |
32 |
ExMASS: A viable model for authentic student-scientist research partnerships
|
Shaner, Andrew |
|
2018 |
152 |
C |
p. 1-9 |
artikel |
33 |
Flame stabilization with a rear-wall-expansion cavity in a supersonic combustor
|
Yang, Yixin |
|
2018 |
152 |
C |
p. 752-756 |
artikel |
34 |
Flatness-based trajectory planning for electromagnetic spacecraft proximity operations in elliptical orbits
|
Zhu, Yan-wei |
|
2018 |
152 |
C |
p. 342-351 |
artikel |
35 |
Flexible heat shields deployed by centrifugal force
|
Wu, Rui |
|
2018 |
152 |
C |
p. 78-87 |
artikel |
36 |
Form-finding design of electrostatically controlled deployable membrane antenna based on an extended force density method
|
Gu, Yongzhen |
|
2018 |
152 |
C |
p. 757-767 |
artikel |
37 |
Ground-based experiment of capturing space debris based on artificial potential field
|
Huang, Zheng |
|
2018 |
152 |
C |
p. 235-241 |
artikel |
38 |
Heliogyro solar sail with self-regulated centrifugal deployment enabled by an origami-inspired morphing reflector
|
Wu, Rui |
|
2018 |
152 |
C |
p. 242-253 |
artikel |
39 |
Humor as a coping strategy in spaceflight
|
Brcic, Jelena |
|
2018 |
152 |
C |
p. 175-178 |
artikel |
40 |
Hybrid tension control method for tethered satellite systems during large tumbling space debris removal
|
Chu, Zhongyi |
|
2018 |
152 |
C |
p. 611-623 |
artikel |
41 |
Hydraulic characteristics of high temperature hydrocarbon liquid jets with various orifice geometries
|
Lee, Hyung Ju |
|
2018 |
152 |
C |
p. 657-666 |
artikel |
42 |
IFC - Publication Information
|
|
|
2018 |
152 |
C |
p. IFC |
artikel |
43 |
Impact of dynamic coupling between relative orbit and attitude on the estimation of relative dynamics of spacecraft
|
Chaves-Jiménez, A. |
|
2018 |
152 |
C |
p. 850-858 |
artikel |
44 |
Investigation on gaseous jet in forebody/inlet for shock-induced combustion ramjet (shcramjet) engines
|
Du, Zhao-bo |
|
2018 |
152 |
C |
p. 262-274 |
artikel |
45 |
Investigations of injection parameters on combustion oscillation in a supersonic crossflow
|
Zhao, Guo-Yan |
|
2018 |
152 |
C |
p. 426-436 |
artikel |
46 |
Investigations on flowfield behavior and resistance backpressure characteristics of supersonic cascade with boundary layer suction
|
Wang, Ziao |
|
2018 |
152 |
C |
p. 588-601 |
artikel |
47 |
Low-energy transfers to long-term capture in the Earth-Moon system
|
Qi, Yi |
|
2018 |
152 |
C |
p. 836-849 |
artikel |
48 |
LOX/methane reusable rocket propulsion at reach with large scale demonstrators tested
|
Boué, Yoan |
|
2018 |
152 |
C |
p. 542-556 |
artikel |
49 |
Manned lunar landing mission scale analysis and flight scheme selection based on mission architecture matrix
|
Wang, Xiaohui |
|
2018 |
152 |
C |
p. 385-395 |
artikel |
50 |
Mixing enhancement mechanism induced by the cascaded fuel injectors in supersonic flows: A numerical study
|
Huang, Wei |
|
2018 |
152 |
C |
p. 18-26 |
artikel |
51 |
Modal analysis and identification of deployable membrane structures
|
Wei, Jianzheng |
|
2018 |
152 |
C |
p. 811-822 |
artikel |
52 |
MPC-based anti-sway control of tethered space robots
|
Meng, Zhongjie |
|
2018 |
152 |
C |
p. 146-162 |
artikel |
53 |
Non-sphere perturbation on dynamic behaviors of spatial flexible damping beam
|
Hu, Weipeng |
|
2018 |
152 |
C |
p. 196-200 |
artikel |
54 |
Numerical investigation of a rotating detonation engine under premixed/non-premixed conditions
|
Sun, Jian |
|
2018 |
152 |
C |
p. 630-638 |
artikel |
55 |
Numerical investigation of effect of hydrogen injection frequency on supersonic reactive flow
|
Liu, Xin |
|
2018 |
152 |
C |
p. 880-890 |
artikel |
56 |
Numerical investigation on behaviors of shock train in a hypersonic inlet with translating cowl
|
Shi, Wen |
|
2018 |
152 |
C |
p. 682-691 |
artikel |
57 |
Numerical investigation on the film cooling performance in a multi-elements splash platelet injector
|
Yin, Liang |
|
2018 |
152 |
C |
p. 458-467 |
artikel |
58 |
On-orbit assembly mission planning considering topological constraint and attitude disturbance
|
She, Yuchen |
|
2018 |
152 |
C |
p. 692-704 |
artikel |
59 |
Optical changes of molecular contamination thin-film outgassed from epoxy-based resin during deposition and desorption process
|
Shimazaki, Kazunori |
|
2018 |
152 |
C |
p. 10-17 |
artikel |
60 |
Optimization design for shape-transition curved isolator with controllable cross-sectional area
|
Meng, Zewei |
|
2018 |
152 |
C |
p. 335-341 |
artikel |
61 |
Optimization of scramjet performance with different fuel injection techniques and flame holder cavities
|
Kummitha, Obula Reddy |
|
2018 |
152 |
C |
p. 908-919 |
artikel |
62 |
Passive nonlinear actuators for deploying mesh antennas
|
Li, Meng |
|
2018 |
152 |
C |
p. 254-261 |
artikel |
63 |
Performance analysis of fixed wing space drones in different solar system bodies
|
Hassanalian, M. |
|
2018 |
152 |
C |
p. 27-48 |
artikel |
64 |
Photometric limits on the high resolution imaging of exoplanets using the solar gravity lens
|
Willems, Phil A. |
|
2018 |
152 |
C |
p. 408-414 |
artikel |
65 |
Precise time estimation of on-orbit satellite fragmentations
|
Itaya, Yuki |
|
2018 |
152 |
C |
p. 415-425 |
artikel |
66 |
Psychological and biological challenges of the Mars mission viewed through the construct of the evolution of fundamental human needs
|
Szocik, Konrad |
|
2018 |
152 |
C |
p. 793-799 |
artikel |
67 |
Relative equilibria and stability of a dumbbell spacecraft about an asteroid
|
Shi, Yu |
|
2018 |
152 |
C |
p. 208-217 |
artikel |
68 |
Resilience evaluation of the environmental control and life support system of a spacecraft for deep space travel
|
Matelli, José Alexandre |
|
2018 |
152 |
C |
p. 360-369 |
artikel |
69 |
Semi-autonomous attitude guidance using relative navigation based on line of sight measurements – Aim scenario
|
Pellacani, Andrea |
|
2018 |
152 |
C |
p. 496-508 |
artikel |
70 |
Serum microRNA as noninvasive indicator for space radiation
|
Wei, Wenjun |
|
2018 |
152 |
C |
p. 101-104 |
artikel |
71 |
Simulation of pressure oscillations in a combustion chamber under periodic inlet disturbances
|
Wang, Dapeng |
|
2018 |
152 |
C |
p. 859-871 |
artikel |
72 |
Simulation of supersonic Ethylene–Hydrogen and air auto-ignition flame using skeletal mechanism
|
Liu, Bing |
|
2018 |
152 |
C |
p. 521-533 |
artikel |
73 |
Solar 3D printing of lunar regolith
|
Meurisse, A. |
|
2018 |
152 |
C |
p. 800-810 |
artikel |
74 |
Space elevator maturing into a Galactic Harbour
|
Swan, Peter |
|
2018 |
152 |
C |
p. 123-126 |
artikel |
75 |
Spaceport and Ground Segment assessment for enabling operations of suborbital transportation systems in the Italian territory
|
Santoro, Francesco |
|
2018 |
152 |
C |
p. 396-407 |
artikel |
76 |
Stable orbital transfer of partial space elevator by tether deployment and retrieval
|
Shi, Gefei |
|
2018 |
152 |
C |
p. 624-629 |
artikel |
77 |
Stochastic optimization of asteroid three-dimensional trajectory transfer
|
Bazzocchi, Michael C.F. |
|
2018 |
152 |
C |
p. 705-718 |
artikel |
78 |
Study of satellite formation flying control using differential lift and drag
|
Ivanov, D. |
|
2018 |
152 |
C |
p. 88-100 |
artikel |
79 |
Study on the dynamic response of a pressure swirl injector to ramp variation of mass flow rate
|
Cheng, Peng |
|
2018 |
152 |
C |
p. 449-457 |
artikel |
80 |
Surrogate modeling for liquid-gas interface determination under microgravity
|
Wu, Zongyu |
|
2018 |
152 |
C |
p. 71-77 |
artikel |
81 |
The Breakthrough Starshot system model
|
Parkin, Kevin L.G. |
|
2018 |
152 |
C |
p. 370-384 |
artikel |
82 |
The Rosetta science operations and planning implementation
|
Pérez-Ayúcar, Miguel |
|
2018 |
152 |
C |
p. 163-174 |
artikel |
83 |
The Space Rider Programme: End user's needs and payload applications survey as driver for mission and system definition
|
Fedele, Alberto |
|
2018 |
152 |
C |
p. 534-541 |
artikel |
84 |
Time-optimal solar sail heteroclinic-like connections for an Earth-Mars cycler
|
Vergaaij, Merel |
|
2018 |
152 |
C |
p. 474-485 |
artikel |
85 |
Topology optimization of pretensioned reflector antennas with unified cable-bar model
|
Feng, Shufei |
|
2018 |
152 |
C |
p. 872-879 |
artikel |
86 |
Type synthesis of non-holonomic spherical constraint underactuated parallel robotics
|
Gao, Zenggui |
|
2018 |
152 |
C |
p. 509-520 |
artikel |
87 |
Verbal reports of neurovestibular symptoms in astronauts after short-duration space flight
|
Reschke, Millard F. |
|
2018 |
152 |
C |
p. 229-234 |
artikel |
88 |
Volumetric assessment of satellite encounter rates
|
Alfano, Salvatore |
|
2018 |
152 |
C |
p. 891-907 |
artikel |