| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
A comprehensive assessment of collision likelihood in Geosynchronous Earth Orbit
|
Oltrogge, D.L.
|
|
|
147 |
C |
p. 316-345
|
artikel
|
| 2 |
An integrated control scheme for space robot after capturing non-cooperative target
|
Wang, Mingming
|
|
|
147 |
C |
p. 350-363
|
artikel
|
| 3 |
An open-loop system design for deep space signal processing applications
|
Tang, Jifei
|
|
|
147 |
C |
p. 259-272
|
artikel
|
| 4 |
A study of upwind schemes on the laminar hypersonic heating predictions for the reusable space vehicle
|
Qu, Feng
|
|
|
147 |
C |
p. 412-420
|
artikel
|
| 5 |
Autonomous assembly with collision avoidance of a fleet of flexible spacecraft based on disturbance observer
|
Chen, Ti
|
|
|
147 |
C |
p. 86-96
|
artikel
|
| 6 |
Boundary control of anti-symmetric vibration of satellite with flexible appendages in planar motion with exponential stability
|
Rad, Hossein Kaviani
|
|
|
147 |
C |
p. 219-230
|
artikel
|
| 7 |
Calibration and performance measurements for the nasa deep space network aperture enhancement project (daep)
|
LaBelle, Remi C.
|
|
|
147 |
C |
p. 37-47
|
artikel
|
| 8 |
Can the implementation of aerospace science in elementary school help girls maintain their confidence and engagement in science as they transition to middle school?
|
Solberg, Margot
|
|
|
147 |
C |
p. 462-472
|
artikel
|
| 9 |
Characterization of commercial off-the shelf regenerable sorbent to scrub carbon dioxide in a portable life support system
|
Arai, Tatsuya
|
|
|
147 |
C |
p. 273-280
|
artikel
|
| 10 |
Combustion dynamics in cryogenic rocket engines: Research programme at DLR Lampoldshausen
|
Hardi, Justin S.
|
|
|
147 |
C |
p. 251-258
|
artikel
|
| 11 |
Concept and performance study of turbocharged solid propellant ramjet
|
Li, Jiang
|
|
|
147 |
C |
p. 431-444
|
artikel
|
| 12 |
Design and landing dynamic analysis of reusable landing leg for a near-space manned capsule
|
Yue, Shuai
|
|
|
147 |
C |
p. 9-26
|
artikel
|
| 13 |
Development of a hardware-in-the-loop testbed to demonstrate multiple spacecraft operations in proximity
|
Eun, Youngho
|
|
|
147 |
C |
p. 48-58
|
artikel
|
| 14 |
Elements of ESA’s policy on space and security
|
Giannopapa, Christina
|
|
|
147 |
C |
p. 346-349
|
artikel
|
| 15 |
Energy-driven scheduling algorithm for nanosatellite energy harvesting maximization
|
Slongo, L.K.
|
|
|
147 |
C |
p. 141-151
|
artikel
|
| 16 |
Experimental analysis of a Flat Plate Pulsating Heat Pipe with Self-ReWetting Fluids during a parabolic flight campaign
|
Cecere, Anselmo
|
|
|
147 |
C |
p. 454-461
|
artikel
|
| 17 |
Experimental study on the thrust modulation performance of powdered magnesium and CO2 bipropellant engine
|
Li, Chao
|
|
|
147 |
C |
p. 403-411
|
artikel
|
| 18 |
Experiments study on attitude coupling control method for flexible spacecraft
|
Wang, Jie
|
|
|
147 |
C |
p. 393-402
|
artikel
|
| 19 |
Exploring opportunities and challenges for establishing a South American Space Agency
|
Silva-Martinez, Jackelynne P.
|
|
|
147 |
C |
p. 473-488
|
artikel
|
| 20 |
Flame structure of methane/oxygen shear coaxial jet with velocity ratio using high-speed imaging and OH*, CH* chemiluminescence
|
Shim, Myungbo
|
|
|
147 |
C |
p. 127-132
|
artikel
|
| 21 |
Hong-Ou-Mandel Gravitational Wave Space spectrometER – HOMER mission
|
Jacinto de Matos, Clovis
|
|
|
147 |
C |
p. 364-373
|
artikel
|
| 22 |
Hybrid Smith predictor and phase lead based divergence compensation for hardware-in-the-loop contact simulation with measurement delay
|
Qi, Chenkun
|
|
|
147 |
C |
p. 175-182
|
artikel
|
| 23 |
IFC - Publication Information
|
|
|
|
147 |
C |
p. IFC
|
artikel
|
| 24 |
Initiation characteristics of wedge-induced oblique detonation waves in turbulence flows
|
Yu, Moyao
|
|
|
147 |
C |
p. 195-204
|
artikel
|
| 25 |
Investigation on thermo-acoustic instability dynamic characteristics of hydrocarbon fuel flowing in scramjet cooling channel based on wavelet entropy method
|
Zan, Hao
|
|
|
147 |
C |
p. 27-36
|
artikel
|
| 26 |
Micromechanical analysis of composites with fibers distributed randomly over the transverse cross-section
|
Weng, Jingmeng
|
|
|
147 |
C |
p. 133-140
|
artikel
|
| 27 |
Nonlinear convective flows in a two-layer system under the action of spatial temperature modulation of heat release/consumption at the interface
|
Simanovskii, Ilya B.
|
|
|
147 |
C |
p. 297-315
|
artikel
|
| 28 |
Numerical analysis and design optimization of supersonic after-burning with strut fuel injectors for scramjet engines
|
Candon, M.J.
|
|
|
147 |
C |
p. 281-296
|
artikel
|
| 29 |
Numerical experiment on the flow field properties of a blunted body with a counterflowing jet in supersonic flows
|
Huang, Wei
|
|
|
147 |
C |
p. 231-240
|
artikel
|
| 30 |
Numerical form-finding method for large mesh reflectors with elastic rim trusses
|
Yang, Dongwu
|
|
|
147 |
C |
p. 241-250
|
artikel
|
| 31 |
Orbital resonances of Taiwan’s FORMOSAT-2 remote sensing satellite
|
Lin, Shin-Fa
|
|
|
147 |
C |
p. 71-85
|
artikel
|
| 32 |
Overload control of artificial gravity facility using spinning tether system for high eccentricity transfer orbits
|
Gou, Xing-wang
|
|
|
147 |
C |
p. 383-392
|
artikel
|
| 33 |
Periodic orbit-attitude solutions along planar orbits in a perturbed circular restricted three-body problem for the Earth-Moon system
|
Bucci, Lorenzo
|
|
|
147 |
C |
p. 152-162
|
artikel
|
| 34 |
Quasi-model free control for the post-capture operation of a non-cooperative target
|
She, Yuchen
|
|
|
147 |
C |
p. 59-70
|
artikel
|
| 35 |
Reliability analysis of multicellular system architectures for low-cost satellites
|
Erlank, A.O.
|
|
|
147 |
C |
p. 183-194
|
artikel
|
| 36 |
Satellite Vibration Testing: Angle optimisation method to Reduce Overtesting
|
Knight, Charly
|
|
|
147 |
C |
p. 205-218
|
artikel
|
| 37 |
Simulations of momentum transfer process between solar wind plasma and bias voltage tethers of electric sail thruster
|
Xia, Guangqing
|
|
|
147 |
C |
p. 107-113
|
artikel
|
| 38 |
Speed-constrained three-axes attitude control using kinematic steering
|
Schaub, Hanspeter
|
|
|
147 |
C |
p. 1-8
|
artikel
|
| 39 |
Star of AOXiang: An innovative 12U CubeSat to demonstrate polarized light navigation and microgravity measurement
|
Yu, Xiaozhou
|
|
|
147 |
C |
p. 97-106
|
artikel
|
| 40 |
Suitable configurations for triangular formation flying about collinear libration points under the circular and elliptic restricted three-body problems
|
Ferrari, Fabio
|
|
|
147 |
C |
p. 374-382
|
artikel
|
| 41 |
Surface thermochemical effects on TPS-coupled aerothermodynamics in hypersonic Martian gas flow
|
Yang, Xiaofeng
|
|
|
147 |
C |
p. 445-453
|
artikel
|
| 42 |
System analysis and test-bed for an atmosphere-breathing electric propulsion system using an inductive plasma thruster
|
Romano, F.
|
|
|
147 |
C |
p. 114-126
|
artikel
|
| 43 |
The paradoxical effect of long instructions on negative affect and performance: When, for whom and why do they backfire?
|
Goemaere, Sophie
|
|
|
147 |
C |
p. 421-430
|
artikel
|
| 44 |
Variable Mach number design approach for a parallel waverider with a wide-speed range based on the osculating cone theory
|
Zhao, Zhen-tao
|
|
|
147 |
C |
p. 163-174
|
artikel
|
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