| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
A compact matchbox-sized dust detector for lunar surface applications
|
Wang, Yongjun
|
|
|
223 |
C |
p. 540-549
|
artikel
|
| 2 |
Aerodynamic performance optimization of a UAV's airfoil at low-Reynolds number and transonic flow under the Martian carbon dioxide atmosphere
|
Zhao, Yuanqi
|
|
|
223 |
C |
p. 512-524
|
artikel
|
| 3 |
A holistic approach for efficient greener in-space propulsion
|
Blondel-Canepari, Lily
|
|
|
223 |
C |
p. 435-447
|
artikel
|
| 4 |
Altitude optimality boundary of two variants of large space debris removal to disposal orbits
|
Grishko, D.A.
|
|
|
223 |
C |
p. 328-341
|
artikel
|
| 5 |
A new system design tool for a hybrid rocket engine
|
Quero Granado, Elena
|
|
|
223 |
C |
p. 119-133
|
artikel
|
| 6 |
Architecting CubeSat constellations for messaging service, Part I
|
Osipova, Ksenia
|
|
|
223 |
C |
p. 525-539
|
artikel
|
| 7 |
A review of shielding systems for protecting off-earth structures from micrometeoroid and orbital debris impact
|
Rakib, Md Abdur
|
|
|
223 |
C |
p. 404-425
|
artikel
|
| 8 |
Assessing black soldier fly pupation and survival in lunar regolith simulant: Implications for sustainable controlled habitats on the Moon
|
Romano, Donato
|
|
|
223 |
C |
p. 505-511
|
artikel
|
| 9 |
AstrobeeCD: Change detection in microgravity with free-flying robots
|
Dinkel, Holly
|
|
|
223 |
C |
p. 98-107
|
artikel
|
| 10 |
Combustion behavior of NMP-001, a nitromethane-based green rocket propellant
|
Kurilov, Maxim
|
|
|
223 |
C |
p. 1-14
|
artikel
|
| 11 |
Comparison of transfer trajectory to NRHO and operation plan for logistics resupply mission to gateway
|
Kikuchi, Junji
|
|
|
223 |
C |
p. 577-584
|
artikel
|
| 12 |
Composite structures with embedded fiber optic sensors: A smart propellant tank for future spacecraft applications
|
Nosseir, Ahmed E.S.
|
|
|
223 |
C |
p. 144-158
|
artikel
|
| 13 |
Conceptual design of rocket engines using regolith-derived propellants
|
Hampl, Sebastian K.
|
|
|
223 |
C |
p. 594-605
|
artikel
|
| 14 |
Corrigendum to “A numerical model of dust particle impacts during a cometary encounter with application to ESA’s Comet Interceptor mission” [Acta Astronaut. 195 (2022) 243–250]
|
Haslebacher, Nico
|
|
|
223 |
C |
p. 638-639
|
artikel
|
| 15 |
Decreased human sperm motility and vitality after fast gravity load changes in a parabolic flight
|
Perez-Poch, Antoni
|
|
|
223 |
C |
p. 640-648
|
artikel
|
| 16 |
Deep reinforcement learning-based dynamic multi-beam power allocation for GEO-LEO co-existing satellites
|
Xu, Jing
|
|
|
223 |
C |
p. 197-209
|
artikel
|
| 17 |
Development of a modular half-duplex frequency-agile X-band transceiver for CubeSats and robotic spacecraft
|
Bonny, Robin F.
|
|
|
223 |
C |
p. 630-637
|
artikel
|
| 18 |
Distant retrograde orbit baseline generation considering solar eclipse mitigation
|
Sun, Yang
|
|
|
223 |
C |
p. 221-233
|
artikel
|
| 19 |
Editorial Board
|
|
|
|
223 |
C |
p. ii
|
artikel
|
| 20 |
Effect of non-equilibrium thermochemistry on Pitot pressure measurements in shock tunnels (or: Is 0.92 really the magic number?)
|
Sopek, Tamara
|
|
|
223 |
C |
p. 249-261
|
artikel
|
| 21 |
Effects of liquid-fuel temperature on rotating-detonation-wave propagation
|
Zhou, Shengbing
|
|
|
223 |
C |
p. 134-143
|
artikel
|
| 22 |
Effects of the droplet size and engine size on two-phase kerosene/air rotating detonation engines in flight operation conditions
|
Cao, Wenbo
|
|
|
223 |
C |
p. 108-118
|
artikel
|
| 23 |
Expansion ignition limit of hydrocarbon fuels based on the controllable free radical relay combustion under extreme conditions
|
Sheng, Haoqiang
|
|
|
223 |
C |
p. 373-383
|
artikel
|
| 24 |
Exploring efficiency in next generation high temperature superconducting-enhanced applied field magnetoplasmadynamic thrusters: A combined numerical and experimental study
|
Aftab, Hammad
|
|
|
223 |
C |
p. 448-461
|
artikel
|
| 25 |
Exploring the potential of fractionated spacecraft for enhanced satellite connectivity: Application to the satellite-to-cell case
|
Alandihallaj, M. Amin
|
|
|
223 |
C |
p. 58-76
|
artikel
|
| 26 |
Fast development and validation of a Sensing Suite system for CubeSats
|
Bollattino, Simone
|
|
|
223 |
C |
p. 342-354
|
artikel
|
| 27 |
Flow-thermal coupled investigation on hypersonic spike-jet with channel
|
Wang, Ziyu
|
|
|
223 |
C |
p. 649-665
|
artikel
|
| 28 |
Ignition and combustion characteristics of magnesium-based nanofluid fuel
|
Zhao, Zilong
|
|
|
223 |
C |
p. 234-241
|
artikel
|
| 29 |
Impact of dormancy on ECLSS design and operation: A review
|
Eshima, Samuel P.
|
|
|
223 |
C |
p. 304-315
|
artikel
|
| 30 |
Improved detection of a Near-Earth Asteroid from an interplanetary CubeSat mission
|
Mitchell, Adriana M.
|
|
|
223 |
C |
p. 685-692
|
artikel
|
| 31 |
Improving the knowledge of the orbital population New technical means of space debris monitoring
|
Letizia, Francesca
|
|
|
223 |
C |
p. 734-740
|
artikel
|
| 32 |
Indirect optimal control techniques for multimode propulsion mission design
|
Cline, Bryan C.
|
|
|
223 |
C |
p. 759-776
|
artikel
|
| 33 |
Mass property estimation on TSE(3) via unscented Kalman filter using RCS thrusters
|
McCann, Brennan S.
|
|
|
223 |
C |
p. 462-480
|
artikel
|
| 34 |
Model-based controllers for CubeSat ORU installation: A comparative study
|
Kurnell, Mitchell
|
|
|
223 |
C |
p. 666-684
|
artikel
|
| 35 |
Model-based hybrid control of combined active–passive vertical zero-gravity system
|
Qi, Naiming
|
|
|
223 |
C |
p. 606-620
|
artikel
|
| 36 |
Modeling of turbulence, chemistry, and heat transfer of a rocket nozzle
|
Kumar, Naveen
|
|
|
223 |
C |
p. 495-504
|
artikel
|
| 37 |
Multi-disciplinary optimization of constellation deployment strategies including launcher selection
|
Di Pasquale, Giuseppe
|
|
|
223 |
C |
p. 389-403
|
artikel
|
| 38 |
NASA’s Capture, Containment, and Return System: Bringing Mars samples to Earth
|
Sarli, Bruno
|
|
|
223 |
C |
p. 270-303
|
artikel
|
| 39 |
No reason to colonize the whole galaxy
|
Totschnig, Wolfhart
|
|
|
223 |
C |
p. 693-701
|
artikel
|
| 40 |
Optimal design and current control strategies of an electrodynamic tape for ISS station-keeping
|
Brunello, A.
|
|
|
223 |
C |
p. 621-629
|
artikel
|
| 41 |
Optimizing translucent multilayer membrane for lunar habitats: A design study
|
Razeto, Cosimo
|
|
|
223 |
C |
p. 316-327
|
artikel
|
| 42 |
Performance evaluation of rebound damping of target marker
|
Kusumoto, Tetsuya
|
|
|
223 |
C |
p. 36-48
|
artikel
|
| 43 |
Piezoelectric energy harvesting from the atomic oxygen hypervelocity impact in low Earth orbit
|
Seo, Jae Hyeon
|
|
|
223 |
C |
p. 585-593
|
artikel
|
| 44 |
Predicting muscle function and mass with electrical impedance myography: A study in rat analogs of micro- and partial gravity
|
Rosa-Caldwell, Megan E.
|
|
|
223 |
C |
p. 384-388
|
artikel
|
| 45 |
Proprioceptive swarms for celestial body exploration
|
Cottiga, Simone
|
|
|
223 |
C |
p. 159-174
|
artikel
|
| 46 |
Prospecting in-situ resources for future crewed missions to Mars
|
Gross, Christoph
|
|
|
223 |
C |
p. 15-24
|
artikel
|
| 47 |
Robotic exploration of Martian caves: Evaluating operational concepts through analog experiments in lava tubes
|
Morrell, Benjamin J.
|
|
|
223 |
C |
p. 741-758
|
artikel
|
| 48 |
Slopes along Apollo EVAs: Astronaut experience as input for future mission planning
|
Iqbal, Wajiha
|
|
|
223 |
C |
p. 184-196
|
artikel
|
| 49 |
Space interferometer orbit determination with multi-GNSS
|
Zapevalin, P.R.
|
|
|
223 |
C |
p. 175-183
|
artikel
|
| 50 |
Specific rhizobacterial assembly enhances the physiological adaptation of soil-cultivated wheat to simulated microgravity
|
Zhao, Liting
|
|
|
223 |
C |
p. 723-733
|
artikel
|
| 51 |
SPRISS: Scalable and precise resistive impact sensor for smallsats, architecture description and tests
|
Enzo, Samuele
|
|
|
223 |
C |
p. 25-35
|
artikel
|
| 52 |
2023 State of the industry report on investment and development of space solar power
|
Barry, Kevin
|
|
|
223 |
C |
p. 355-372
|
artikel
|
| 53 |
Sunbeam: Near-sun statites as beam platforms for beam-driven rockets
|
Greason, Jeffrey K.
|
|
|
223 |
C |
p. 262-269
|
artikel
|
| 54 |
Swarm-to-swarm orbital pursuit method under delta-v maneuver for space pursuit-evasion
|
Luo, Yuelong
|
|
|
223 |
C |
p. 702-722
|
artikel
|
| 55 |
Temperature mapping methods for thermoelastic analyses of the ARIEL spacecraft payload module
|
García-Pérez, Andrés
|
|
|
223 |
C |
p. 77-97
|
artikel
|
| 56 |
The history of the Italian astronautical sector and the A.I.R., the Italian Rocket Association
|
Marchetti, Mario
|
|
|
223 |
C |
p. 210-220
|
artikel
|
| 57 |
The influence of lunar environment exposure on characteristics of nuclear energy He–Xe closed Brayton cycle
|
Sun, Zijian
|
|
|
223 |
C |
p. 481-494
|
artikel
|
| 58 |
The ion beam interceptor concept for a space station collision avoidance with space debris
|
Aslanov, V.S.
|
|
|
223 |
C |
p. 49-57
|
artikel
|
| 59 |
The need to improve registration practices in the context of space traffic management
|
Masson-Zwaan, Tanja
|
|
|
223 |
C |
p. 242-248
|
artikel
|
| 60 |
Thermite-for-demise (T4D): Experiments and numerical modelling on ball-bearing unit mock-ups containing thermite in an arc-heated wind tunnel
|
Finazzi, A.
|
|
|
223 |
C |
p. 550-576
|
artikel
|
| 61 |
Time- and angular-distribution of ion current in pulse-laser ablation plume of aluminum
|
Nakamura, Yusuke
|
|
|
223 |
C |
p. 426-434
|
artikel
|
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