| no |
title |
author |
magazine |
year |
volume |
issue |
page(s) |
type |
| 1 |
Ablation characteristics and reaction mechanism of insulation materials under slag deposition condition
|
Guan, Yiwen
|
|
2017
|
136 |
C |
p. 80-89
|
article
|
| 2 |
Ablation spot area and impulse characteristics of polymers induced by burst irradiation of 1µm laser pulses
|
Tsuruta, Hisashi
|
|
2017
|
136 |
C |
p. 46-54
|
article
|
| 3 |
Aluminum agglomeration involving the second mergence of agglomerates on the solid propellants burning surface: Experiments and modeling
|
Ao, Wen
|
|
2017
|
136 |
C |
p. 219-229
|
article
|
| 4 |
Analysis of orbit determination from Earth-based tracking for relay satellites in a perturbed areostationary orbit
|
Romero, P.
|
|
2017
|
136 |
C |
p. 434-442
|
article
|
| 5 |
A new concept of space solar power satellite
|
Li, Xun
|
|
2017
|
136 |
C |
p. 182-189
|
article
|
| 6 |
Asteroid deflection using a spacecraft in restricted keplerian motion
|
Ketema, Yohannes
|
|
2017
|
136 |
C |
p. 64-79
|
article
|
| 7 |
A wall grid scale criterion for hypersonic aerodynamic heating calculation
|
Yang, Jianlong
|
|
2017
|
136 |
C |
p. 137-143
|
article
|
| 8 |
Cruise status of Hayabusa2: Round trip mission to asteroid 162173 Ryugu
|
Tsuda, Yuichi
|
|
2017
|
136 |
C |
p. 176-181
|
article
|
| 9 |
Design for CubeSat-based dust and radiation studies at Europa
|
Goel, Ashish
|
|
2017
|
136 |
C |
p. 204-218
|
article
|
| 10 |
Diamagnetic antimatter storage
|
Semyonov, Oleg G.
|
|
2017
|
136 |
C |
p. 190-203
|
article
|
| 11 |
Dynamics and mixing mechanism of transverse jet injection into a supersonic combustor with cavity flameholder
|
Liu, Chaoyang
|
|
2017
|
136 |
C |
p. 90-100
|
article
|
| 12 |
Effect of static shape deformation on aerodynamics and aerothermodynamics of hypersonic inflatable aerodynamic decelerator
|
Guo, Jinghui
|
|
2017
|
136 |
C |
p. 421-433
|
article
|
| 13 |
Finite time attitude takeover control for combination via tethered space robot
|
Lu, Yingbo
|
|
2017
|
136 |
C |
p. 9-21
|
article
|
| 14 |
Finite time coordinated formation control for spacecraft formation flying under directed communication topology
|
Ran, Dechao
|
|
2017
|
136 |
C |
p. 125-136
|
article
|
| 15 |
High accuracy GNSS based navigation in GEO
|
Capuano, Vincenzo
|
|
2017
|
136 |
C |
p. 332-341
|
article
|
| 16 |
IFC - Publication Information
|
|
|
2017
|
136 |
C |
p. IFC
|
article
|
| 17 |
Ignition kinetics of boron in primary combustion products of propellant based on its unique characteristics
|
Ao, Wen
|
|
2017
|
136 |
C |
p. 450-458
|
article
|
| 18 |
In-situ grown MgO-ZnO ceramic coating with high thermal emittance on Mg alloy by plasma electrolytic oxidation
|
Li, Hang
|
|
2017
|
136 |
C |
p. 230-235
|
article
|
| 19 |
Kinematic accuracy and dynamic performance of a simple planar space deployable mechanism with joint clearance considering parameter uncertainty
|
Li, Junlan
|
|
2017
|
136 |
C |
p. 34-45
|
article
|
| 20 |
Long-range AIS message analysis based on the TianTuo-3 micro satellite
|
Li, Shiyou
|
|
2017
|
136 |
C |
p. 159-165
|
article
|
| 21 |
Method of interplanetary trajectory optimization for the spacecraft with low thrust and swing-bys
|
Konstantinov, M.S.
|
|
2017
|
136 |
C |
p. 297-311
|
article
|
| 22 |
Modeling of aerodynamic heat flux and thermoelastic behavior of nose caps of hypersonic vehicles
|
Persova, Marina G.
|
|
2017
|
136 |
C |
p. 312-331
|
article
|
| 23 |
Multi-objective trajectory optimization of Space Manoeuvre Vehicle using adaptive differential evolution and modified game theory
|
Chai, Runqi
|
|
2017
|
136 |
C |
p. 273-280
|
article
|
| 24 |
Nonablative lightweight thermal protection system for Mars Aeroflyby Sample collection mission
|
Suzuki, Toshiyuki
|
|
2017
|
136 |
C |
p. 407-420
|
article
|
| 25 |
Nose-to-tail analysis of an airbreathing hypersonic vehicle using an in-house simplified tool
|
Piscitelli, Filomena
|
|
2017
|
136 |
C |
p. 148-158
|
article
|
| 26 |
Numerical investigation of switching mechanism for the supersonic jet element
|
Xu, Y.
|
|
2017
|
136 |
C |
p. 342-353
|
article
|
| 27 |
Numerical simulations on unsteady operation processes of N2O/HTPB hybrid rocket motor with/without diaphragm
|
Zhang, Shuai
|
|
2017
|
136 |
C |
p. 115-124
|
article
|
| 28 |
On the advantages of exploiting the hierarchical structure of astrodynamical models
|
Dei Tos, Diogene Alessandro
|
|
2017
|
136 |
C |
p. 236-247
|
article
|
| 29 |
Optimal capture occasion determination and trajectory generation for space robots grasping tumbling objects
|
Luo, Jianjun
|
|
2017
|
136 |
C |
p. 380-386
|
article
|
| 30 |
Optimal thrust level for orbit insertion
|
Cerf, Max
|
|
2017
|
136 |
C |
p. 55-63
|
article
|
| 31 |
Protection of surface assets on Mars from wind blown jettisoned spacecraft components
|
Paton, Mark
|
|
2017
|
136 |
C |
p. 395-406
|
article
|
| 32 |
Research into topology optimization and the FDM method for a space cracked membrane
|
Hu, Qingxi
|
|
2017
|
136 |
C |
p. 443-449
|
article
|
| 33 |
Robust distributed control of spacecraft formation flying with adaptive network topology
|
Shasti, Behrouz
|
|
2017
|
136 |
C |
p. 281-296
|
article
|
| 34 |
Robust, fast and accurate vision-based localization of a cooperative target used for space robotic arm
|
Wen, Zhuoman
|
|
2017
|
136 |
C |
p. 101-114
|
article
|
| 35 |
Robust high-precision attitude control for flexible spacecraft with improved mixed H 2/H ∞ control strategy under poles assignment constraint
|
Liu, Chuang
|
|
2017
|
136 |
C |
p. 166-175
|
article
|
| 36 |
Robust spacecraft attitude tracking control using hybrid actuators with uncertainties
|
Cao, Xibin
|
|
2017
|
136 |
C |
p. 1-8
|
article
|
| 37 |
Self-calibration rank filter for unknown dynamic inputs mitigation during the Mars powered descent phase
|
Xiao, Qiang
|
|
2017
|
136 |
C |
p. 360-368
|
article
|
| 38 |
Strategies to utilize advanced heat shield technology for high-payload mars atmospheric entry missions
|
Braun, Max
|
|
2017
|
136 |
C |
p. 22-33
|
article
|
| 39 |
Study of the unsteady mode transition process for an over-under TBCC exhaust system
|
Lv, Zheng
|
|
2017
|
136 |
C |
p. 259-272
|
article
|
| 40 |
Study on atomization and combustion characteristics of LOX/methane pintle injectors
|
Fang, Xin-xin
|
|
2017
|
136 |
C |
p. 369-379
|
article
|
| 41 |
The final year of the Rosetta mission
|
Accomazzo, Andrea
|
|
2017
|
136 |
C |
p. 354-359
|
article
|
| 42 |
Thermal design and validation of radiation detector for the ChubuSat-2 micro-satellite with high-thermal-conductive graphite sheets
|
Park, Daeil
|
|
2017
|
136 |
C |
p. 387-394
|
article
|
| 43 |
Thermal protection performance of magnetohydrodynamic heat shield system based on multipolar magnetic field
|
Kai, Li
|
|
2017
|
136 |
C |
p. 248-258
|
article
|
| 44 |
The ultimate limits of the relativistic rocket equation. The Planck photon rocket
|
Haug, Espen Gaarder
|
|
2017
|
136 |
C |
p. 144-147
|
article
|
Journal description