| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
Ablation characteristics of rocket nozzle using HfC-SiC refractory ceramic composite
|
Kim, Kyu-Seop
|
|
|
173 |
C |
p. 31-44
|
artikel
|
| 2 |
Achieving the required mobility in the solar system through direct fusion drive
|
Genta, Giancarlo
|
|
|
173 |
C |
p. 303-309
|
artikel
|
| 3 |
Adaptive parameter identification based nadir-pointing control of spacecraft with misaligned rotational component
|
Wu, Fan
|
|
|
173 |
C |
p. 202-211
|
artikel
|
| 4 |
A multiple-shooting differential dynamic programming algorithm. Part 2: Applications
|
Pellegrini, Etienne
|
|
|
173 |
C |
p. 460-472
|
artikel
|
| 5 |
A real-time search for interstellar impacts on the moon
|
Siraj, Amir
|
|
|
173 |
C |
p. 53-55
|
artikel
|
| 6 |
Attitude control for spacecraft using pyramid-type variable-speed control moment gyros
|
Higashiyama, Daiki
|
|
|
173 |
C |
p. 252-265
|
artikel
|
| 7 |
Attitude determination & control system design for gravity recovery missions like GRACE
|
Mashtakov, Yaroslav
|
|
|
173 |
C |
p. 172-182
|
artikel
|
| 8 |
Boundary control design for vibration suppression and attitude control of flexible satellites with multi-section appendages
|
Ataei, Mohammad Mahdi
|
|
|
173 |
C |
p. 22-30
|
artikel
|
| 9 |
Calculation of linear conductances for thermal lumped models by means of the CMF method
|
Piqueras, Javier
|
|
|
173 |
C |
p. 76-85
|
artikel
|
| 10 |
Combustion of H2/air supersonic mixing layers with splitter plate: Flame structure and statistical characteristics
|
Xiao, Yao
|
|
|
173 |
C |
p. 279-293
|
artikel
|
| 11 |
Comparison of Beidou autonomous navigation performance using the SRP model and onboard accelerometers
|
Qiao, Jing
|
|
|
173 |
C |
p. 183-194
|
artikel
|
| 12 |
Corrigendum to “Spray characteristics of a pintle injector based on annular orifice area” [Acta Astronautica 167 (2020) 201–211]
|
Lee, Suji
|
|
|
173 |
C |
p. 473-474
|
artikel
|
| 13 |
Environment capacity as an early mission design driver
|
Letizia, Francesca
|
|
|
173 |
C |
p. 320-332
|
artikel
|
| 14 |
Experimental study of flame stabilization in a single-side expansion scramjet combustor with different cavity length-to-depth ratios
|
Li, Fan
|
|
|
173 |
C |
p. 1-8
|
artikel
|
| 15 |
Fast rendezvous profile evolution: From ISS to lunar station
|
Murtazin, R.
|
|
|
173 |
C |
p. 139-144
|
artikel
|
| 16 |
Feasibility assessment of passive stabilisation for a nanosatellite with aeroshell deployed by orbit-attitude-aerodynamics simulation platform
|
Berthet, Maximilien
|
|
|
173 |
C |
p. 266-278
|
artikel
|
| 17 |
Geotechnical characterisation of two new low-fidelity lunar regolith analogues (UoM-B and UoM-W) for use in large-scale engineering experiments
|
Just, G.H.
|
|
|
173 |
C |
p. 414-424
|
artikel
|
| 18 |
Global positioning system interferometric reflectometry for accurate tide gauge measurement: Insights from South Beach, Oregon, United States
|
Ansari, Kutubuddin
|
|
|
173 |
C |
p. 356-362
|
artikel
|
| 19 |
Ground testing of an on-orbit atomic oxygen flux and ionizing radiation dose sensor based on material degradation by the space environment
|
Verker, Ronen
|
|
|
173 |
C |
p. 333-343
|
artikel
|
| 20 |
IFC - Publication Information
|
|
|
|
173 |
C |
p. IFC
|
artikel
|
| 21 |
Imperfection sensitivity of free vibration of symmetrically/anti-symmetrically laminated FRC beams in thermally pre-and post-buckling equilibrium states
|
Jin, Qiduo
|
|
|
173 |
C |
p. 240-251
|
artikel
|
| 22 |
Implementing bioburden reduction and control on the deliquescent hydrogel of the HABIT/ExoMars 2022 instrument
|
Mathanlal, Thasshwin
|
|
|
173 |
C |
p. 232-239
|
artikel
|
| 23 |
Insight into the plasma structure of the Quad Confinement Thruster using electron kinetic modelling
|
Williams, Rhys David
|
|
|
173 |
C |
p. 111-118
|
artikel
|
| 24 |
Instability of an asymmetric supersonic planar wake
|
Yang, Rui
|
|
|
173 |
C |
p. 86-90
|
artikel
|
| 25 |
Integration of Deprit's radial intermediary
|
Abad, Alberto
|
|
|
173 |
C |
p. 19-21
|
artikel
|
| 26 |
LaserCube optical communication terminal for nano and micro satellites
|
Sansone, Francesco
|
|
|
173 |
C |
p. 310-319
|
artikel
|
| 27 |
Lunar critical fragment layer simulant identification using an impact method
|
Ye, T.
|
|
|
173 |
C |
p. 294-302
|
artikel
|
| 28 |
Lunar Flashlight CubeSat GNC system development
|
Lai, Peter C.
|
|
|
173 |
C |
p. 425-441
|
artikel
|
| 29 |
Machine learning algorithm to forecast ionospheric time delays using Global Navigation satellite system observations
|
Mallika I, Lakshmi
|
|
|
173 |
C |
p. 221-231
|
artikel
|
| 30 |
Maneuvers to reduce Ariane 5 upper stage lifetime duration in orbit
|
Renard, Emelyne
|
|
|
173 |
C |
p. 442-448
|
artikel
|
| 31 |
Modelling of satellite constellations for trusted node QKD networks
|
Vergoossen, Tom
|
|
|
173 |
C |
p. 164-171
|
artikel
|
| 32 |
New GEO paradigm: Re-purposing satellite components from the GEO graveyard
|
Barbara, Nicholas H.
|
|
|
173 |
C |
p. 155-163
|
artikel
|
| 33 |
Numerical and experimental investigation of the geometrical scale effect on a confined subsonic-supersonic shear layer
|
Ma, Kai
|
|
|
173 |
C |
p. 212-220
|
artikel
|
| 34 |
Preliminary investigation of paraffin-based fuel combustion in solid fuel scramjet
|
Zhang, Hao
|
|
|
173 |
C |
p. 119-130
|
artikel
|
| 35 |
Reducing Doppler noise with multi-station tracking: The Cassini test case
|
Notaro, Virginia
|
|
|
173 |
C |
p. 45-52
|
artikel
|
| 36 |
Representing and querying space object registration data using graph databases
|
Le May, S.
|
|
|
173 |
C |
p. 392-403
|
artikel
|
| 37 |
Rotating spoke analysis of Hall thruster performance during the extinguishing process
|
Lv, You
|
|
|
173 |
C |
p. 378-382
|
artikel
|
| 38 |
Shock wave/turbulence boundary layer interaction control with the secondary recirculation jet in a supersonic flow
|
Yan, Li
|
|
|
173 |
C |
p. 131-138
|
artikel
|
| 39 |
Significance of 3U CubeSat OrigamiSat-1 for space demonstration of multifunctional deployable membrane
|
Ikeya, Kosuke
|
|
|
173 |
C |
p. 363-377
|
artikel
|
| 40 |
Single axis stabilization of a fast rotating satellite in the orbital frame using magnetorquers and a rotor
|
Ovchinnikov, M. Yu.
|
|
|
173 |
C |
p. 195-201
|
artikel
|
| 41 |
Size matters - The shell lander concept for exploring medium-size airless bodies
|
Grimm, Christian D.
|
|
|
173 |
C |
p. 91-110
|
artikel
|
| 42 |
Solar sailing near the Sun: A comparison study between point-like and spherical-like Sun models
|
Markhoos, Ahmed M.
|
|
|
173 |
C |
p. 9-18
|
artikel
|
| 43 |
Space debris ontology for ADR capture methods selection
|
Jankovic, Marko
|
|
|
173 |
C |
p. 56-68
|
artikel
|
| 44 |
StELIUM: A student experiment to investigate the sloshing of magnetic liquids in microgravity
|
Romero-Calvo, Á.
|
|
|
173 |
C |
p. 344-355
|
artikel
|
| 45 |
Study and modeling of propellant ablation in coaxial ablative pulsed plasma thrusters
|
Huang, Tiankun
|
|
|
173 |
C |
p. 69-75
|
artikel
|
| 46 |
The EcAMSat fluidic system to study antibiotic resistance in low earth orbit: Development and lessons learned from space flight
|
Padgen, Michael R.
|
|
|
173 |
C |
p. 449-459
|
artikel
|
| 47 |
The MaMBA-concept for an extraterrestrial base and its first module mock-up
|
Heinicke, C.
|
|
|
173 |
C |
p. 404-413
|
artikel
|
| 48 |
Utilizing the Analytical Hierarchy Process to determine the optimal lunar habitat configuration
|
Higgins, Michael
|
|
|
173 |
C |
p. 145-154
|
artikel
|
| 49 |
Visual navigation algorithm based on line geomorphic feature matching for Mars landing
|
Shao, Wei
|
|
|
173 |
C |
p. 383-391
|
artikel
|
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