nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
1 |
A comparative reliability analysis of ballistic deployments on binary asteroids
|
Çelik, Onur |
|
2019 |
156 |
C |
p. 308-316 |
artikel |
2 |
A concept of hazardous NEO detection and impact warning system
|
Ikenaga, Toshinori |
|
2019 |
156 |
C |
p. 284-296 |
artikel |
3 |
Advances in planetary defense in the United States
|
Landis, Rob |
|
2019 |
156 |
C |
p. 394-408 |
artikel |
4 |
Aluminum agglomeration of AP/HTPB composite propellant
|
Yuan, Jifei |
|
2019 |
156 |
C |
p. 14-22 |
artikel |
5 |
A novel push-pull asteroid magnetic Tractor(MT)
|
Brown, William |
|
2019 |
156 |
C |
p. 371-374 |
artikel |
6 |
A radar package for asteroid subsurface investigations: Implications of implementing and integration into the MASCOT nanoscale landing platform from science requirements to baseline design
|
Herique, Alain |
|
2019 |
156 |
C |
p. 317-329 |
artikel |
7 |
Asteroid de-spin and deflection strategy using a solar-sail spacecraft with reflectivity control devices
|
Kikuchi, Shota |
|
2019 |
156 |
C |
p. 375-386 |
artikel |
8 |
Bilateral control of uncertain telerobotic systems using iterative learning control: Design and stability analysis
|
Shokri-Ghaleh, Hamid |
|
2019 |
156 |
C |
p. 58-69 |
artikel |
9 |
Capabilities of Gossamer-1 derived small spacecraft solar sails carrying Mascot-derived nanolanders for in-situ surveying of NEAs
|
Grundmann, Jan Thimo |
|
2019 |
156 |
C |
p. 330-362 |
artikel |
10 |
Cargo logistics for a Notional Mars Base using Solar Electric Propulsion
|
Woolley, Ryan C. |
|
2019 |
156 |
C |
p. 51-57 |
artikel |
11 |
Characterization of flow mixing and structural topology in supersonic planar mixing layer
|
Zhang, Dongdong |
|
2019 |
156 |
C |
p. 33-43 |
artikel |
12 |
Cylindrical shock wave generated by a moving piston in a rotational axisymmetric non-ideal gas with conductive and radiative heat-fluxes in the presence of azimuthal magnetic field
|
Nath, G. |
|
2019 |
156 |
C |
p. 100-112 |
artikel |
13 |
Deflection of fictitious asteroid 2017 PDC: Ion beam vs. kinetic impactor
|
Bombardelli, Claudio |
|
2019 |
156 |
C |
p. 301-307 |
artikel |
14 |
ESA's distributed space weather sensor system (D3S) utilizing hosted payloads for operational space weather monitoring
|
Kraft, Stefan |
|
2019 |
156 |
C |
p. 157-161 |
artikel |
15 |
Exploring optical SETI's middle ground
|
Stanton, Richard H. |
|
2019 |
156 |
C |
p. 92-99 |
artikel |
16 |
Hayabusa2–Sample return and kinetic impact mission to near-earth asteroid Ryugu
|
Tsuda, Yuichi |
|
2019 |
156 |
C |
p. 387-393 |
artikel |
17 |
Heat to electricity conversion systems for moon exploration scenarios: A review of space and ground technologies
|
Mazzetti, Alessandro |
|
2019 |
156 |
C |
p. 162-186 |
artikel |
18 |
High fidelity model for the atmospheric re-entry of CubeSats equipped with the Drag De-Orbit Device
|
Rafano Carná, S.F. |
|
2019 |
156 |
C |
p. 134-156 |
artikel |
19 |
IFC - Publication Information
|
|
|
2019 |
156 |
C |
p. IFC |
artikel |
20 |
Implementation and application of digitally controlled piezoelectric vibration absorbers to truss structures
|
Yamada, Satoshi |
|
2019 |
156 |
C |
p. 70-77 |
artikel |
21 |
International coordination on planetary defence: The work of the IAWN and the SMPAG
|
Kofler, Romana |
|
2019 |
156 |
C |
p. 409-415 |
artikel |
22 |
Low-energy weak stability boundary transfers to Pluto's moons: Preliminary trajectory design via triangular libration point
|
Liang, Yuying |
|
2019 |
156 |
C |
p. 219-233 |
artikel |
23 |
Measuring ejecta characteristics and momentum transfer in experimental simulation of kinetic impact
|
Schimmerohn, Martin |
|
2019 |
156 |
C |
p. 297-300 |
artikel |
24 |
Mixing augmentation mechanism induced by the dual injection concept in shcramjet engines
|
Du, Zhao-bo |
|
2019 |
156 |
C |
p. 1-13 |
artikel |
25 |
Modeling relative motion of LEO satellites at different altitudes
|
Sarno, Salvatore |
|
2019 |
156 |
C |
p. 197-207 |
artikel |
26 |
Near and far-field hazards of asteroid impacts in oceans
|
Robertson, Darrel K. |
|
2019 |
156 |
C |
p. 262-277 |
artikel |
27 |
Neighboring optimal guidance and constrained attitude control applied to three-dimensional lunar ascent and orbit injection
|
Pontani, Mauro |
|
2019 |
156 |
C |
p. 78-91 |
artikel |
28 |
NorSat-2: Enabling advanced maritime communication with VDES
|
Bradbury, Laura M. |
|
2019 |
156 |
C |
p. 44-50 |
artikel |
29 |
OMOTENASHI trajectory analysis and design: Landing phase
|
Hernando-Ayuso, Javier |
|
2019 |
156 |
C |
p. 113-124 |
artikel |
30 |
Resonant space tethered system for lunar orbital energy harvesting
|
Liu, Jiafu |
|
2019 |
156 |
C |
p. 23-32 |
artikel |
31 |
Set-oriented design of interplanetary low-thrust trajectories using Earth Gravity Assist
|
Tamakoshi, Daisuke |
|
2019 |
156 |
C |
p. 208-218 |
artikel |
32 |
Simulation-based height of burst map for asteroid airburst damage prediction
|
Aftosmis, Michael J. |
|
2019 |
156 |
C |
p. 278-283 |
artikel |
33 |
Special Section on Planetary Defense: Detection, Deflection, Evacuation
|
Carnelli, Ian |
|
2019 |
156 |
C |
p. 250-251 |
artikel |
34 |
Systems engineering and design of a Mars Polar Research Base with a human crew
|
Rüede, Anne-Marlene |
|
2019 |
156 |
C |
p. 234-249 |
artikel |
35 |
The feasibility of deflecting asteroid 2017 PDC using neutral beam propulsion
|
DeCicco, A.J. |
|
2019 |
156 |
C |
p. 363-370 |
artikel |
36 |
The political desirability, feasibility, and sustainability of planetary defense governance
|
Schmidt, Nikola |
|
2019 |
156 |
C |
p. 416-426 |
artikel |
37 |
Timing performance evaluation of Radio Determination Satellite Service (RDSS) for Beidou system
|
Wang, Dongxia |
|
2019 |
156 |
C |
p. 125-133 |
artikel |
38 |
Towards increasing nanosatellite subsystem robustness
|
Batista, Carlos Leandro Gomes |
|
2019 |
156 |
C |
p. 187-196 |
artikel |
39 |
Uncertainty propagation in the N-body problem using Dromo elements
|
Hernando-Ayuso, Javier |
|
2019 |
156 |
C |
p. 252-261 |
artikel |