| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
Aerodynamics and flight mechanics activities for a suborbital flight test of a deployable heat shield capsule
|
Fedele, Alberto
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|
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151 |
C |
p. 324-333
|
artikel
|
| 2 |
Aging constitutive model of hydroxyl-terminated polybutadiene coating in solid rocket motor
|
Li, Ke
|
|
|
151 |
C |
p. 555-562
|
artikel
|
| 3 |
A high-accuracy constrained SINS/CNS tight integrated navigation for high-orbit automated transfer vehicles
|
Wang, Dingjie
|
|
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151 |
C |
p. 614-625
|
artikel
|
| 4 |
ALCIDES: A novel lunar mission concept study for the demonstration of enabling technologies in deep-space exploration and human-robots interaction
|
Hady, Ghassabian G.
|
|
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151 |
C |
p. 270-283
|
artikel
|
| 5 |
A lunar flyby for a tridimensional Earth-to-Earth mission
|
Gagg Filho, Luiz Arthur
|
|
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151 |
C |
p. 228-242
|
artikel
|
| 6 |
Ambiguous relative orbits in sequential relative orbit estimation with range-only measurements
|
Wang, Jingwei
|
|
|
151 |
C |
p. 626-644
|
artikel
|
| 7 |
Analysis and reduction of skin-friction in a rocket-based combined-cycle engine flow path operating from Mach 1.5 to 6.0
|
Wang, Shuai
|
|
|
151 |
C |
p. 357-367
|
artikel
|
| 8 |
Analysis of lithium-combustion power systems for extreme environment spacecraft
|
Greer, Christopher J.
|
|
|
151 |
C |
p. 68-79
|
artikel
|
| 9 |
An anti-saturation steering law for Three Dimensional Magnetically Suspended Wheel cluster with angle constraint
|
Zhang, Rui
|
|
|
151 |
C |
p. 467-474
|
artikel
|
| 10 |
An early history of the Philippine space development program
|
Verspieren, Q.
|
|
|
151 |
C |
p. 919-927
|
artikel
|
| 11 |
An easy-to-implement thermal test system for large deployable antennas
|
Wu, Hao
|
|
|
151 |
C |
p. 494-503
|
artikel
|
| 12 |
A new explorer mission for soft X-ray timing - Observation of the Crab pulsar
|
Huang, Liangwei
|
|
|
151 |
C |
p. 63-67
|
artikel
|
| 13 |
Angular momentum management strategy of the FengYun-4 meteorological satellite
|
Liu, Yiwu
|
|
|
151 |
C |
p. 22-31
|
artikel
|
| 14 |
An investigation of millimeter wave reflectarrays for small satellite platforms
|
Ahmad, Ghulam
|
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|
151 |
C |
p. 475-486
|
artikel
|
| 15 |
A passive camera based determination of a non-cooperative and unknown satellite's pose and shape
|
Volpe, Renato
|
|
|
151 |
C |
p. 805-817
|
artikel
|
| 16 |
Benchmarking information carriers
|
Hippke, Michael
|
|
|
151 |
C |
p. 53-62
|
artikel
|
| 17 |
Benchmarking inscribed matter probes
|
Hippke, Michael
|
|
|
151 |
C |
p. 32-36
|
artikel
|
| 18 |
CGR-BF: An efficient contact utilization scheme for predictable deep space Delay Tolerant Network
|
Dhara, Sangita
|
|
|
151 |
C |
p. 401-411
|
artikel
|
| 19 |
Comparison of the space bubble detector response to space-like neutron spectra and high energy protons
|
Miller, Alexander
|
|
|
151 |
C |
p. 1-6
|
artikel
|
| 20 |
Contact dynamics and control of a space robot capturing a tumbling object
|
Wu, Shuang
|
|
|
151 |
C |
p. 532-542
|
artikel
|
| 21 |
Control of the drag on a spacecraft in the earth’s ionosphere using the spacecraft’s magnetic field
|
Shuvalov, Valentin A.
|
|
|
151 |
C |
p. 717-725
|
artikel
|
| 22 |
CubeSat constellation management using Ionic Liquid Electrospray Propulsion
|
Gomez Jenkins, Marco
|
|
|
151 |
C |
p. 243-252
|
artikel
|
| 23 |
Curing of large prepreg shell in solar synchronous Low Earth Orbit: Precession flight regimes
|
Pestrenin, V.M.
|
|
|
151 |
C |
p. 342-347
|
artikel
|
| 24 |
Design and analysis of flexure revolute joint based on four-bar mechanism
|
Zhang, Jing
|
|
|
151 |
C |
p. 420-431
|
artikel
|
| 25 |
Design and high speed aerodynamic performance analysis of vortex lift waverider with a wide-speed range
|
Zhao, Zhen-tao
|
|
|
151 |
C |
p. 848-863
|
artikel
|
| 26 |
Design methodology of the waverider with a controllable planar shape
|
Wang, Jifei
|
|
|
151 |
C |
p. 504-510
|
artikel
|
| 27 |
Disturbance rejection dynamic inverse control of air-breathing hypersonic vehicles
|
An, Hao
|
|
|
151 |
C |
p. 348-356
|
artikel
|
| 28 |
Effect of the heat release on the component coordination in the rocket-based combined cycle engine
|
Yan, Dekun
|
|
|
151 |
C |
p. 942-952
|
artikel
|
| 29 |
Effects of a High Fidelity Filter on the attitude stabilization of a flexible spacecraft
|
Sabatini, Marco
|
|
|
151 |
C |
p. 260-269
|
artikel
|
| 30 |
Effects of solar panels on Aerodynamics of a small satellite with deployable aero-brake
|
Mungiguerra, S.
|
|
|
151 |
C |
p. 456-466
|
artikel
|
| 31 |
Experimental investigation of self-excited combustion instabilities with injection coupling in a cryogenic rocket combustor
|
Armbruster, Wolfgang
|
|
|
151 |
C |
p. 655-667
|
artikel
|
| 32 |
Experimental investigations on ethylene-air Continuous Rotating Detonation wave in the hollow chamber with Laval nozzle
|
Peng, Haoyang
|
|
|
151 |
C |
p. 137-145
|
artikel
|
| 33 |
Experimental study of near-blowoff characteristics in a cavity-based supersonic combustor
|
Song, Xiliang
|
|
|
151 |
C |
p. 37-43
|
artikel
|
| 34 |
Experimental study on a rotating detonation combustor with an axial-flow turbine
|
Zhou, Shengbing
|
|
|
151 |
C |
p. 7-14
|
artikel
|
| 35 |
Fault-tolerant attitude control of miniature satellites using reaction wheels
|
Kumar, Krishna Dev
|
|
|
151 |
C |
p. 206-216
|
artikel
|
| 36 |
Fixed-time attitude tracking control for spacecraft without unwinding
|
Huang, Bing
|
|
|
151 |
C |
p. 818-827
|
artikel
|
| 37 |
Form-finding of deployable mesh reflectors using dynamic relaxation method
|
Wang, Xinyu
|
|
|
151 |
C |
p. 380-388
|
artikel
|
| 38 |
Galactic distribution of chirality sources of organic molecules
|
Helman, Daniel S.
|
|
|
151 |
C |
p. 595-602
|
artikel
|
| 39 |
Ground-based experiments of tether deployment subject to an analytical control law
|
Yu, B.S.
|
|
|
151 |
C |
p. 253-259
|
artikel
|
| 40 |
Guaranteeing prescribed performance for air-breathing hypersonic vehicles via an adaptive non-affine tracking controller
|
Bu, Xiangwei
|
|
|
151 |
C |
p. 368-379
|
artikel
|
| 41 |
Hayabusa2-Ryugu proximity operation planning and landing site selection
|
Yamaguchi, Tomohiro
|
|
|
151 |
C |
p. 217-227
|
artikel
|
| 42 |
Historical-orbital-data-based method for monitoring the operational status of satellites in low Earth orbit
|
Li, Tao
|
|
|
151 |
C |
p. 88-94
|
artikel
|
| 43 |
Hypersonic shock wave transitional boundary layer interactions - A review
|
Knight, Doyle
|
|
|
151 |
C |
p. 296-317
|
artikel
|
| 44 |
IFC - Publication Information
|
|
|
|
151 |
C |
p. IFC
|
artikel
|
| 45 |
Ignition mechanism in ablative pulsed plasma thrusters with coaxial semiconductor spark plugs
|
Sun, Guorui
|
|
|
151 |
C |
p. 120-124
|
artikel
|
| 46 |
Improved tracklet association for space objects using short-arc optical measurements
|
Cai, Han
|
|
|
151 |
C |
p. 836-847
|
artikel
|
| 47 |
Integrated vibration isolation and attitude control for spacecraft with uncertain or unknown payload inertia parameters
|
Guo, Zixi
|
|
|
151 |
C |
p. 107-119
|
artikel
|
| 48 |
Investigation of RBCC performance improvements based on a variable geometry ramjet combustor
|
Ye, Jinying
|
|
|
151 |
C |
p. 874-885
|
artikel
|
| 49 |
Investigation of self-pulsation characteristics for a liquid-centered swirl coaxial injector with recess
|
Bai, Xiao
|
|
|
151 |
C |
p. 511-521
|
artikel
|
| 50 |
Investigation on dynamic behaviors of thermal protection system using a two degree-of-freedom nonlinear theoretical method
|
Huang, Jie
|
|
|
151 |
C |
p. 828-835
|
artikel
|
| 51 |
Investigation on plume expansion and ionization in a laser ablation plasma thruster
|
Zhang, Yu
|
|
|
151 |
C |
p. 432-444
|
artikel
|
| 52 |
Lessons learned in 20 years of application of Systems Concurrent Engineering to space products
|
Loureiro, G.
|
|
|
151 |
C |
p. 44-52
|
artikel
|
| 53 |
Libration dynamics of electrodynamic tether system for 13 degrees International Geomagnetic Reference Field
|
Yang, Yu-wei
|
|
|
151 |
C |
p. 182-205
|
artikel
|
| 54 |
Linear time-varying model predictive control of magnetically actuated satellites in elliptic orbits
|
Kim, Jongbum
|
|
|
151 |
C |
p. 791-804
|
artikel
|
| 55 |
Massive scale, long battery life, direct to orbit connectivity for the internet of things
|
Haley, David
|
|
|
151 |
C |
p. 318-323
|
artikel
|
| 56 |
Mastering operational limitations of LEO satellites – The GomX-3 approach
|
Nies, Gilles
|
|
|
151 |
C |
p. 726-735
|
artikel
|
| 57 |
Mission analysis for Earth to Mars-Phobos distant Retrograde Orbits
|
Conte, Davide
|
|
|
151 |
C |
p. 761-771
|
artikel
|
| 58 |
Momentum enhancement factor estimation for asteroid redirect missions
|
Delchambre, Simon
|
|
|
151 |
C |
p. 125-136
|
artikel
|
| 59 |
Multi-objective integrated robust H∞ control for attitude tracking of a flexible spacecraft
|
Wu, Shunan
|
|
|
151 |
C |
p. 80-87
|
artikel
|
| 60 |
NASA's eXploration Systems and Habitation (X-Hab) Academic Innovation Challenge
|
Crusan, Jason
|
|
|
151 |
C |
p. 412-419
|
artikel
|
| 61 |
Non-iterative angles-only initial relative orbit determination with J 2 perturbations
|
Perez, A.C.
|
|
|
151 |
C |
p. 146-159
|
artikel
|
| 62 |
Numerical investigation of bleeding control method on section-controllable wavecatcher intakes
|
Zuo, Fengyuan
|
|
|
151 |
C |
p. 572-584
|
artikel
|
| 63 |
Numerical simulations of radiative heat effects in a plasma wind-tunnel flow under Mars entry conditions
|
García-Garrido, Javier
|
|
|
151 |
C |
p. 334-341
|
artikel
|
| 64 |
Numerical study on separation shock characteristics of pyrotechnic separation nuts
|
Zhao, Hongda
|
|
|
151 |
C |
p. 893-903
|
artikel
|
| 65 |
Optimal injection point for launch trajectories with parametric thrust profile
|
Cerf, Max
|
|
|
151 |
C |
p. 752-760
|
artikel
|
| 66 |
Parameterization and optimization for shape-transition curved isolator
|
Meng, Zewei
|
|
|
151 |
C |
p. 563-571
|
artikel
|
| 67 |
Performance evaluation and comparison of electricity generation systems based on single- and two-stage thermoelectric generator for hypersonic vehicles
|
Cheng, Kunlin
|
|
|
151 |
C |
p. 15-21
|
artikel
|
| 68 |
Performance evaluation methodology for multistage launch vehicles with high-fidelity modeling
|
Pallone, Marco
|
|
|
151 |
C |
p. 522-531
|
artikel
|
| 69 |
Predictive visual servo kinematic control for autonomous robotic capture of non-cooperative space target
|
Dong, Gangqi
|
|
|
151 |
C |
p. 173-181
|
artikel
|
| 70 |
Pros and cons of relativistic interstellar flight
|
Semyonov, Oleg G.
|
|
|
151 |
C |
p. 736-742
|
artikel
|
| 71 |
Re-affirming Europe's ambitions in space: Past, present and future perspectives
|
Antoni, Ntorina
|
|
|
151 |
C |
p. 772-778
|
artikel
|
| 72 |
Relative control of an ion beam shepherd satellite using the impulse compensation thruster
|
Alpatov, A.
|
|
|
151 |
C |
p. 543-554
|
artikel
|
| 73 |
Re-planning strategies for space station on-orbit activities executed in emergencies
|
Mu, Shuai
|
|
|
151 |
C |
p. 779-790
|
artikel
|
| 74 |
Sliding mode control for autonomous spacecraft rendezvous with collision avoidance
|
Li, Qi
|
|
|
151 |
C |
p. 743-751
|
artikel
|
| 75 |
Spacecraft angular velocity trajectory planning for SGCMG singularity avoidance
|
Hou, Zhili
|
|
|
151 |
C |
p. 284-295
|
artikel
|
| 76 |
Space debris collision probability analysis for proposed global broadband constellations
|
Le May, S.
|
|
|
151 |
C |
p. 445-455
|
artikel
|
| 77 |
SpooQySats: CubeSats to demonstrate quantum key distribution technologies
|
Grieve, James A.
|
|
|
151 |
C |
p. 103-106
|
artikel
|
| 78 |
Structural design and optimization of large cable–rib tension deployable antenna structure with dynamic constraint
|
Liu, Ruiwei
|
|
|
151 |
C |
p. 160-172
|
artikel
|
| 79 |
Structures of near-wall wakes subjected to a sonic jet in a supersonic crossflow
|
Liu, Yuan
|
|
|
151 |
C |
p. 886-892
|
artikel
|
| 80 |
The edge of space: Revisiting the Karman Line
|
McDowell, Jonathan C.
|
|
|
151 |
C |
p. 668-677
|
artikel
|
| 81 |
The influence of coolant jet direction on heat reduction on the nose cone with Aerodome at supersonic flow
|
Moradi, R.
|
|
|
151 |
C |
p. 487-493
|
artikel
|
| 82 |
The influences of aramid fibre and its compound with ceramic on shielding performance of stuffed layer
|
Ke, Fa-wei
|
|
|
151 |
C |
p. 928-941
|
artikel
|
| 83 |
The Projecting Surface Method for improvement of surface accuracy of large deployable mesh reflectors
|
Yuan, Sichen
|
|
|
151 |
C |
p. 678-690
|
artikel
|
| 84 |
The structural properties of paraffin wax based hybrid rocket fuels with aluminium particles
|
Veale, Kirsty
|
|
|
151 |
C |
p. 864-873
|
artikel
|
| 85 |
Three-dimensional particle simulation of ion thruster plume impingement
|
Cai, Guobiao
|
|
|
151 |
C |
p. 645-654
|
artikel
|
| 86 |
Trajectory design and guidance for landing on Phobos
|
Joffre, Eric
|
|
|
151 |
C |
p. 389-400
|
artikel
|
| 87 |
Uncertain surface accuracy evaluation based on non-probabilistic approach for large spacecraft
|
Yang, Chen
|
|
|
151 |
C |
p. 95-102
|
artikel
|
| 88 |
Uncertainty and sensitivity analysis of flow parameters on aerodynamics of a hypersonic inlet
|
Liu, Hongkang
|
|
|
151 |
C |
p. 703-716
|
artikel
|
| 89 |
Uncertainty calculation for spacecraft thermal models using a generalized SEA method
|
Gómez-San-Juan, Alejandro
|
|
|
151 |
C |
p. 691-702
|
artikel
|
| 90 |
Utilization of trash for radiation protection during manned space missions
|
Xu, Feng
|
|
|
151 |
C |
p. 585-594
|
artikel
|
| 91 |
Vibration analysis of functionally graded porous shear deformable tubes excited by moving distributed loads
|
Wang, Yuewu
|
|
|
151 |
C |
p. 603-613
|
artikel
|
| 92 |
Vibration suppression control of free-floating space robots with flexible appendages for autonomous target capturing
|
Meng, Deshan
|
|
|
151 |
C |
p. 904-918
|
artikel
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