| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
A cutting edge 6U CubeSat ADCS design for Earth observation with sub-meter spatial resolution at 230–380 km altitude
|
Kuiper, Hans
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4 |
p. 613-621
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artikel
|
| 2 |
ADEO: the European commercial passive de-orbit subsystem family enabling space debris mitigation
|
Stelzl, Daniel
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4 |
p. 591-598
|
artikel
|
| 3 |
A design strategy for water-based noise suppression systems in liquid rocket engines firing tests
|
Zolla, Paolo Maria
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4 |
p. 597-611
|
artikel
|
| 4 |
All-fiber versatile laser frequency reference at 2 μm for CO2 space-borne lidar applications
|
Schilt, Stéphane
|
|
2017
|
|
4 |
p. 493-505
|
artikel
|
| 5 |
A method for the experimental characterisation of novel drag-reducing materials for very low Earth orbits using the Satellite for Orbital Aerodynamics Research (SOAR) mission
|
Crisp, Nicholas H.
|
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4 |
p. 655-674
|
artikel
|
| 6 |
An afocal telescope configuration for the ESA ARIEL mission
|
Da Deppo, Vania
|
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2017
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4 |
p. 379-398
|
artikel
|
| 7 |
An investigation into directional characteristics of the rocket plane in a tailless configuration
|
Kwiek, Agnieszka
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4 |
p. 627-640
|
artikel
|
| 8 |
A novel design of a deployable CubeSat for material exposure missions in low earth orbit
|
Xiao, Liping
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4 |
p. 641-653
|
artikel
|
| 9 |
AOCS design for the ATHENA X-ray telescope: challenges and solutions
|
Ott, T.
|
|
2018
|
|
4 |
p. 519-534
|
artikel
|
| 10 |
Applicability of delay tolerant networking to distributed satellite systems
|
Freimann, A.
|
|
2016
|
|
4 |
p. 323-332
|
artikel
|
| 11 |
Are Very Low Earth Orbit (VLEO) satellites a solution for tomorrow’s telecommunication needs?
|
Berthoud, Lucy
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4 |
p. 609-623
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artikel
|
| 12 |
ATLID, ESA atmospheric backscatter LIDAR for the ESA EarthCARE mission
|
Pereira do Carmo, João
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4 |
p. 423-435
|
artikel
|
| 13 |
Automatic mass balancing system for a dynamic CubeSat attitude simulator: development and experimental validation
|
Bahu, Anton
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|
4 |
p. 597-611
|
artikel
|
| 14 |
Autonomous formation flight using solar radiation pressure
|
Thoemel, Jan
|
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4 |
p. 555-566
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artikel
|
| 15 |
Autonomous reconfiguration of a distributed synthetic aperture radar driven by mission requirements
|
Sarno, S.
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4 |
p. 527-537
|
artikel
|
| 16 |
Beyond L∞ reaction wheel commanding: increased on-board autonomy through enhanced wheel failure handling
|
Winkler, Stefan
|
|
2018
|
|
4 |
p. 597-604
|
artikel
|
| 17 |
Broadband antireflection coatings for visible and infrared ranges
|
Lemarquis, Frédéric
|
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|
4 |
p. 567-578
|
artikel
|
| 18 |
Business roadmap for the European Union in the NewSpace ecosystem: a case study for access to space
|
Rodriguez-Donaire, Silvia
|
|
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|
4 |
p. 785-804
|
artikel
|
| 19 |
CASPA-ADM: a mission concept for observing thermospheric mass density
|
Siemes, Christian
|
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|
4 |
p. 637-653
|
artikel
|
| 20 |
Combined method for spacecraft deorbiting with angular stabilization of the sail using magnetorquers
|
Alpatov, Anatoliy
|
|
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|
4 |
p. 613-625
|
artikel
|
| 21 |
Compact S-band and X-band antennas for CubeSats
|
Byrne, Benedikt
|
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|
|
4 |
p. 587-596
|
artikel
|
| 22 |
Complex optical interference filters with stress compensation for space applications
|
Begou, Thomas
|
|
2017
|
|
4 |
p. 441-449
|
artikel
|
| 23 |
Conceptual analysis for a technology demonstration mission of the ion beam shepherds
|
Colpari, Ricardo
|
|
|
|
4 |
p. 567-584
|
artikel
|
| 24 |
Correction and adjusting for the deformation on solar sail
|
Shen, Fan
|
|
2016
|
|
4 |
p. 315-322
|
artikel
|
| 25 |
Correction to: Preliminary aerodynamic design of a reusable booster flight experiment
|
Merrem, C.
|
|
|
|
4 |
p. 665
|
artikel
|
| 26 |
CubeSat measurements of thermospheric plasma: spacecraft charging effects on a plasma analyzer
|
Reddy, Sachin
|
|
|
|
4 |
p. 675-687
|
artikel
|
| 27 |
Damping of piezoelectric space instruments: application to an active optics deformable mirror
|
Alaluf, David
|
|
|
|
4 |
p. 543-551
|
artikel
|
| 28 |
Deployment requirements for deorbiting electrodynamic tether technology
|
Sarego, Giulia
|
|
|
|
4 |
p. 567-581
|
artikel
|
| 29 |
Design and qualification of a recessed satellite cornercube retroreflector for ground-based attitude verification via satellite laser ranging
|
Bartels, Nils
|
|
|
|
4 |
p. 391-403
|
artikel
|
| 30 |
Design and validation of a GNC system for missions to asteroids: the AIM scenario
|
Pellacani, A.
|
|
2017
|
|
4 |
p. 555-566
|
artikel
|
| 31 |
Design of an intake and a thruster for an atmosphere-breathing electric propulsion system
|
Romano, F.
|
|
|
|
4 |
p. 707-715
|
artikel
|
| 32 |
Detection efficiency of microchannel plates to penetrating radiation in space
|
André, N.
|
|
|
|
4 |
p. 607-616
|
artikel
|
| 33 |
Development and analysis of novel mission scenarios based on Atmosphere-Breathing Electric Propulsion (ABEP)
|
Vaidya, S.
|
|
|
|
4 |
p. 689-706
|
artikel
|
| 34 |
Development and qualification of the Feed-Select Mechanism for the Polarimetric and Helioseismic Imager on-board Solar Orbiter
|
Staub, Jan
|
|
|
|
4 |
p. 497-505
|
artikel
|
| 35 |
Development of an innovative validation strategy of gas–surface interaction modelling for re-entry applications
|
Joiner, N.
|
|
2016
|
|
4 |
p. 237-255
|
artikel
|
| 36 |
Development of micro-mirror slicer integral field unit for space-borne solar spectrographs
|
Suematsu, Yoshinori
|
|
2017
|
|
4 |
p. 421-431
|
artikel
|
| 37 |
Developments of high frequency and intensity stabilized lasers for space gravitational wave detector DECIGO/B-DECIGO
|
Suemasa, Aru
|
|
2017
|
|
4 |
p. 485-491
|
artikel
|
| 38 |
Diode-pumped Alexandrite laser for next generation satellite-based earth observation lidar
|
Strotkamp, Michael
|
|
|
|
4 |
p. 413-422
|
artikel
|
| 39 |
Editorial
|
Fix, Andreas
|
|
2017
|
|
4 |
p. 367-369
|
artikel
|
| 40 |
Editorial: International ESA Conference on Guidance, Navigation and Control Systems 2017
|
Bennani, S.
|
|
2018
|
|
4 |
p. 469-470
|
artikel
|
| 41 |
Enabling radiation tolerant heterogeneous GPU-based onboard data processing in space
|
Bruhn, Fredrik C.
|
|
|
|
4 |
p. 551-564
|
artikel
|
| 42 |
End-to-end simulation and verification of GNC and robotic systems considering both space segment and ground segment
|
Benninghoff, Heike
|
|
2017
|
|
4 |
p. 535-553
|
artikel
|
| 43 |
Enhanced AIS receiver design for satellite reception
|
Clazzer, Federico
|
|
2016
|
|
4 |
p. 257-268
|
artikel
|
| 44 |
Enhanced algorithms to ensure the success of rendezvous maneuvers using aerodynamic forces
|
Bühler, S.
|
|
|
|
4 |
p. 637-652
|
artikel
|
| 45 |
Evaluating the stability of NASA’s space launch system with adaptive augmenting control
|
VanZwieten, Tannen S.
|
|
2018
|
|
4 |
p. 583-595
|
artikel
|
| 46 |
Experimental and numerical investigation on thermal fluid–structure interaction on ceramic plates in high enthalpy flow
|
Willems, Sebastian
|
|
2015
|
|
4 |
p. 483-497
|
artikel
|
| 47 |
Experimental validation of heavy rain attenuation in E-band based on climate wind tunnel measurements at 77 GHz
|
Lewark, Ulrich J.
|
|
2015
|
|
4 |
p. 475-481
|
artikel
|
| 48 |
Exploring our solar system with CubeSats and SmallSats: the dawn of a new era
|
Freeman, Anthony
|
|
|
|
4 |
p. 491-502
|
artikel
|
| 49 |
FAINTSTAR: an intelligent single-chip sensor head for star trackers—prototype results
|
Ogiers, W.
|
|
2018
|
|
4 |
p. 605-619
|
artikel
|
| 50 |
Fourier transform spectrometers for remote sensing of planetary atmospheres and surfaces
|
Shakun, Alexey
|
|
2017
|
|
4 |
p. 399-409
|
artikel
|
| 51 |
From lunar regolith to oxygen and structural materials: an integrated conceptual design
|
Radl, Alexandra
|
|
|
|
4 |
p. 585-595
|
artikel
|
| 52 |
From TechnoSat to TUBIN: performance upgrade for the TUBiX20 microsatellite platform based on flight experience
|
Gordon, Karsten
|
|
|
|
4 |
p. 515-525
|
artikel
|
| 53 |
Fused silica GRISMs manufactured by hydrophilic direct bonding at moderate heating
|
Kalkowski, G.
|
|
2017
|
|
4 |
p. 433-440
|
artikel
|
| 54 |
GOES-R active vibration damping controller design, implementation, and on-orbit performance
|
Clapp, Brian R.
|
|
2018
|
|
4 |
p. 501-517
|
artikel
|
| 55 |
Gravity sensing: cold atom trap onboard a 6U CubeSat
|
Devani, Diviya
|
|
|
|
4 |
p. 539-549
|
artikel
|
| 56 |
HgCdTe APDs for time-resolved space applications
|
Rothman, J.
|
|
2017
|
|
4 |
p. 507-516
|
artikel
|
| 57 |
Hybrid controller for global, robust, attitude stabilization of a magnetically actuated spacecraft
|
Bahu, Anton
|
|
|
|
4 |
p. 543-554
|
artikel
|
| 58 |
Hybrid optical navigation by crater detection for lunar pin-point landing: trajectories from helicopter flight tests
|
Trigo, Guilherme F.
|
|
2018
|
|
4 |
p. 567-581
|
artikel
|
| 59 |
In-orbit AIS performance of the Norwegian microsatellites NorSat-1 and NorSat-2
|
Eriksen, Torkild
|
|
|
|
4 |
p. 503-513
|
artikel
|
| 60 |
In-orbit performance of the LISA Pathfinder drag-free and attitude control system
|
Schleicher, A.
|
|
2018
|
|
4 |
p. 471-485
|
artikel
|
| 61 |
Integrated atomic quantum technologies in demanding environments: development and qualification of miniaturized optical setups and integration technologies for UHV and space operation
|
Christ, Marc
|
|
|
|
4 |
p. 561-566
|
artikel
|
| 62 |
Investigation of very low Earth orbits (VLEOs) for global spaceborne lidar
|
McGrath, Ciara
|
|
|
|
4 |
p. 625-636
|
artikel
|
| 63 |
Ka-band to L-band frequency down-conversion based on III–V-on-silicon photonic integrated circuits
|
Gasse, K. Van
|
|
2017
|
|
4 |
p. 531-541
|
artikel
|
| 64 |
Laser-detonation hyperthermal beam source applicable to VLEO environmental simulations
|
Tagawa, Masahito
|
|
|
|
4 |
p. 757-765
|
artikel
|
| 65 |
Launch lock system for reaction wheels
|
Berlin, M.
|
|
|
|
4 |
p. 583-589
|
artikel
|
| 66 |
MERLIN: design of an IPDA LIDAR instrument
|
Nikolov, Susanne
|
|
|
|
4 |
p. 437-457
|
artikel
|
| 67 |
MICROSCOPE mission: drag-free and attitude control system expertise activities toward the scientific team
|
Delavault, Stéphanie
|
|
2018
|
|
4 |
p. 487-500
|
artikel
|
| 68 |
Minimum stiffness criteria for ring frame stiffeners of space launch vehicles
|
Friedrich, Linus
|
|
2016
|
|
4 |
p. 269-290
|
artikel
|
| 69 |
Misalignment estimation for active telescopes
|
Escolle, C.
|
|
|
|
4 |
p. 553-559
|
artikel
|
| 70 |
Modeling and simulation of a GOX/kerosene subscale rocket combustion chamber with film cooling
|
Höglauer, C.
|
|
2015
|
|
4 |
p. 419-432
|
artikel
|
| 71 |
Modified design of the deployable mesh reflector antenna for mini satellites
|
Sushko, O.
|
|
|
|
4 |
p. 533-542
|
artikel
|
| 72 |
NanoCarb hyperspectral sensor: on performance optimization and analysis for greenhouse gas monitoring from a constellation of small satellites
|
Gousset, Silvère
|
|
|
|
4 |
p. 507-524
|
artikel
|
| 73 |
NanoVipa: a miniaturized high-resolution echelle spectrometer, for the monitoring of young stars from a 6U Cubesat
|
Bourdarot, G.
|
|
2017
|
|
4 |
p. 411-419
|
artikel
|
| 74 |
Numerical and experimental analysis of spallation phenomena
|
Martin, Alexandre
|
|
2016
|
|
4 |
p. 229-236
|
artikel
|
| 75 |
On the assembly and calibration of a spatial heterodyne interferometer for limb sounding of the middle atmosphere
|
Kaufmann, Martin
|
|
|
|
4 |
p. 525-531
|
artikel
|
| 76 |
Overview on grating developments at ESA
|
Guldimann, Benedikt
|
|
2015
|
|
4 |
p. 433-451
|
artikel
|
| 77 |
OWLS as platform technology in OPTOS satellite
|
Rivas Abalo, J.
|
|
2017
|
|
4 |
p. 543-554
|
artikel
|
| 78 |
Parasitic light scattered by complex optical coatings: modelization and metrology
|
Zerrad, Myriam
|
|
2017
|
|
4 |
p. 473-484
|
artikel
|
| 79 |
Passive magnetic detumbling to enable Active Debris Removal of non-operational satellites in Low Earth Orbit
|
Benoit, Alain
|
|
|
|
4 |
p. 599-636
|
artikel
|
| 80 |
Performance evaluation of a plasma generator and ion optics for air-breathing ion engine
|
Miya, Yukai
|
|
|
|
4 |
p. 749-755
|
artikel
|
| 81 |
Precise and robust optical beam steering for space optical instrumentation
|
Drougakis, G.
|
|
|
|
4 |
p. 589-595
|
artikel
|
| 82 |
Propulsive jet influence on generic launcher base flow
|
Stephan, S.
|
|
2015
|
|
4 |
p. 453-473
|
artikel
|
| 83 |
Protected silver coatings for reflectors
|
Schwinde, Stefan
|
|
|
|
4 |
p. 579-587
|
artikel
|
| 84 |
Radiometric calibration of the SIMBIO-SYS STereo imaging Channel
|
Slemer, A.
|
|
|
|
4 |
p. 485-496
|
artikel
|
| 85 |
Re-entry predictions of space debris for collision avoidance with air traffic
|
Bernelli-Zazzera, Franco
|
|
|
|
4 |
p. 553-565
|
artikel
|
| 86 |
Remote-sensing satellite ground station evaluation using QPSK emulator with test pattern and PRBS generation
|
Srinivas, R.
|
|
2015
|
|
4 |
p. 399-417
|
artikel
|
| 87 |
Robust approximation of image illumination direction in a segmentation-based crater detection algorithm for spacecraft navigation
|
Maass, Bolko
|
|
2016
|
|
4 |
p. 303-314
|
artikel
|
| 88 |
Satellite laser ranging at 100 kHz pulse repetition rate
|
Hampf, Daniel
|
|
|
|
4 |
p. 363-370
|
artikel
|
| 89 |
Simulation-guided engineering of an air-breathing electric propulsion concept
|
Obrusnik, A.
|
|
|
|
4 |
p. 741-747
|
artikel
|
| 90 |
Small satellites beyond boundaries
|
Tortora, P.
|
|
|
|
4 |
p. 489-490
|
artikel
|
| 91 |
Small satellite TT&C allocations below 1 GHz: outcome of ITU WRC-19
|
von der Ohe, Martin
|
|
|
|
4 |
p. 565-571
|
artikel
|
| 92 |
Space gravitational wave antenna DECIGO and B-DECIGO
|
Musha, Mitsuru
|
|
2017
|
|
4 |
p. 371-377
|
artikel
|
| 93 |
Space Lidar and Space Optics
|
Fix, Andreas
|
|
|
|
4 |
p. 359-362
|
artikel
|
| 94 |
Strategic similarities between earth observation small satellite constellations in very low earth orbit and low-cost carriers by means of strategy canvas
|
Rodriguez-Donaire, Silvia
|
|
|
|
4 |
p. 767-784
|
artikel
|
| 95 |
1st Symposium of Very Low Earth Orbit Missions and Technologies
|
Roberts, Peter C. E.
|
|
|
|
4 |
p. 605-608
|
artikel
|
| 96 |
The absolute frequency reference unit for the spaceborne methane-sensing lidar mission MERLIN
|
Heinecke, D.
|
|
|
|
4 |
p. 459-473
|
artikel
|
| 97 |
The AETHER project: development of air-breathing electric propulsion for VLEO missions
|
Andreussi, T.
|
|
|
|
4 |
p. 717-740
|
artikel
|
| 98 |
The BepiColombo Laser Altimeter (BELA): a post-launch summary
|
Thomas, Nicolas
|
|
|
|
4 |
p. 371-380
|
artikel
|
| 99 |
The challenges of measuring methane from space with a LIDAR
|
Riris, Haris
|
|
|
|
4 |
p. 475-483
|
artikel
|
| 100 |
The design and development of low- and high-voltage ASICs for space-borne CCD cameras
|
Waltham, N.
|
|
2017
|
|
4 |
p. 517-529
|
artikel
|
| 101 |
The Ganymede laser altimeter (GALA): key objectives, instrument design, and performance
|
Hussmann, Hauke
|
|
|
|
4 |
p. 381-390
|
artikel
|
| 102 |
The PILOT optical alignment for its first flight
|
Mot, B.
|
|
2017
|
|
4 |
p. 459-471
|
artikel
|
| 103 |
Thermal characterization of resistance and gain of microchannel plate (MCP) detectors for the JENI experiment
|
Chassela, O. B.
|
|
|
|
4 |
p. 597-605
|
artikel
|
| 104 |
Thin glass shells for active optics for future space telescopes
|
Vecchi, G.
|
|
|
|
4 |
p. 533-541
|
artikel
|
| 105 |
Time analysis for a bistatic radar for asteroid tomography: simulations and test bench
|
Granados, Ricardo
|
|
|
|
4 |
p. 653-664
|
artikel
|
| 106 |
TOMARES
|
Lottes, Laura Malena
|
|
|
|
4 |
p. 521-532
|
artikel
|
| 107 |
Track-to-track association methodology for operational surveillance scenarios with radar observations
|
Pastor, Alejandro
|
|
|
|
4 |
p. 535-551
|
artikel
|
| 108 |
Transformable reflector structure with V-folding rods
|
Tserodze, Sh.
|
|
2016
|
|
4 |
p. 291-301
|
artikel
|
| 109 |
Utility and constraints of PocketQubes
|
Bouwmeester, J.
|
|
|
|
4 |
p. 573-586
|
artikel
|
| 110 |
UV/visible high-sensitivity MCP-PMT single-photon GHz counting detector for long-range lidar instrumentations
|
Orlov, D. A.
|
|
|
|
4 |
p. 405-411
|
artikel
|
| 111 |
Wavefront error measurement of the concave ellipsoidal mirrors of the METIS coronagraph on ESA Solar Orbiter mission
|
Sandri, P.
|
|
2017
|
|
4 |
p. 451-458
|
artikel
|
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