| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
A beacon configuration optimization method based on Fisher information for Mars atmospheric entry
|
Zhao, Zeduan
|
|
2017
|
133 |
C |
p. 467-475
|
artikel
|
| 2 |
Academy transaction note characterization of FRAM microcontrollers to radiations
|
Lacirignola, Federica
|
|
2017
|
133 |
C |
p. 30-32
|
artikel
|
| 3 |
Analysis of flowfield characteristics for equal polygon opposing jet on different freeflow conditions
|
Li, Shi-bin
|
|
2017
|
133 |
C |
p. 50-62
|
artikel
|
| 4 |
A novel ram-air plasma synthetic jet actuator for near space high-speed flow control
|
Zhou, Yan
|
|
2017
|
133 |
C |
p. 95-102
|
artikel
|
| 5 |
Asteroid Origins Satellite (AOSAT) I: An On-orbit Centrifuge Science Laboratory
|
Lightholder, Jack
|
|
2017
|
133 |
C |
p. 81-94
|
artikel
|
| 6 |
Attitude stabilization of flexible spacecrafts via extended disturbance observer based controller
|
Yan, Ruidong
|
|
2017
|
133 |
C |
p. 73-80
|
artikel
|
| 7 |
Concept of a self-pressurized feed system for liquid rocket engines and its fundamental experiment results
|
Matsumoto, Jun
|
|
2017
|
133 |
C |
p. 166-176
|
artikel
|
| 8 |
Disturbance observer-based fuzzy control for flexible spacecraft combined attitude & sun tracking system
|
Chak, Yew-Chung
|
|
2017
|
133 |
C |
p. 302-310
|
artikel
|
| 9 |
Drag reduction for the combination of spike and counterflow jet on blunt body at high Mach number flow
|
Eghlima, Z.
|
|
2017
|
133 |
C |
p. 103-110
|
artikel
|
| 10 |
Dynamic characteristics and performance evaluation for the part strut failure of the vibration isolation platform on satellites
|
Zhang, Yao
|
|
2017
|
133 |
C |
p. 403-415
|
artikel
|
| 11 |
Dynamic modeling and simulation of an integral bipropellant propulsion double-valve combined test system
|
Chen, Yang
|
|
2017
|
133 |
C |
p. 346-374
|
artikel
|
| 12 |
Effect of heat release on movement characteristics of shock train in an isolator
|
Zhang, Chenlin
|
|
2017
|
133 |
C |
p. 185-194
|
artikel
|
| 13 |
Electromagnetic absorption properties of spacecraft and space debris
|
Micheli, D.
|
|
2017
|
133 |
C |
p. 128-135
|
artikel
|
| 14 |
Enabling technologies for Chinese Mars lander guidance system
|
Jiang, Xiuqiang
|
|
2017
|
133 |
C |
p. 375-386
|
artikel
|
| 15 |
Evolution of weak shock waves in non-ideal magnetogasdynamics
|
Nath, Triloki
|
|
2017
|
133 |
C |
p. 397-402
|
artikel
|
| 16 |
Experimental evaluation of a Dielectric Elastomer robotic arm for space applications
|
Branz, F.
|
|
2017
|
133 |
C |
p. 324-333
|
artikel
|
| 17 |
Experimental investigation of the combustion products in an aluminised solid propellant
|
Liu, Zhu
|
|
2017
|
133 |
C |
p. 136-144
|
artikel
|
| 18 |
Experimental study on multiple-pulse performance characteristics of ammonium perchlorate/aluminum powder rocket motor
|
Li, Yue
|
|
2017
|
133 |
C |
p. 455-466
|
artikel
|
| 19 |
Experimental study on the flow separation and self-excited oscillation phenomenon in a rectangular duct
|
Xiong, Bing
|
|
2017
|
133 |
C |
p. 158-165
|
artikel
|
| 20 |
Flexible operation strategy for environment control system in abnormal supply power condition
|
Liping, Pang
|
|
2017
|
133 |
C |
p. 334-345
|
artikel
|
| 21 |
IFC - Publication Information
|
|
|
2017
|
133 |
C |
p. IFC
|
artikel
|
| 22 |
Ignition of a polymer propellant of hybrid rocket motor by a hot particle
|
Glushkov, D.O.
|
|
2017
|
133 |
C |
p. 387-396
|
artikel
|
| 23 |
Instantaneous GNSS attitude determination: A Monte Carlo sampling approach
|
Sun, Xiucong
|
|
2017
|
133 |
C |
p. 24-29
|
artikel
|
| 24 |
Investigation of two degrees of freedom on vortex-induced vibration under the wake interference of an oscillating airfoil
|
Zhang, G.Q.
|
|
2017
|
133 |
C |
p. 423-435
|
artikel
|
| 25 |
Mechanism analysis of Magnetohydrodynamic heat shield system and optimization of externally applied magnetic field
|
Li, Kai
|
|
2017
|
133 |
C |
p. 14-23
|
artikel
|
| 26 |
MHD slip flow of a dissipative Casson fluid over a moving geometry with heat source/sink: A numerical study
|
Raju, C.S.K.
|
|
2017
|
133 |
C |
p. 436-443
|
artikel
|
| 27 |
Nonlinear model and attitude dynamics of flexible spacecraft with large amplitude slosh
|
Deng, Mingle
|
|
2017
|
133 |
C |
p. 111-120
|
artikel
|
| 28 |
Numerical investigation of improving the performance of a single expansion ramp nozzle at off-design conditions by secondary injection
|
Lv, Zheng
|
|
2017
|
133 |
C |
p. 233-243
|
artikel
|
| 29 |
Online attitude determination of a passively magnetically stabilized spacecraft
|
Burton, R.
|
|
2017
|
133 |
C |
p. 269-281
|
artikel
|
| 30 |
On-orbit assembly of a team of flexible spacecraft using potential field based method
|
Chen, Ti
|
|
2017
|
133 |
C |
p. 221-232
|
artikel
|
| 31 |
Optimal mission planning of GEO on-orbit refueling in mixed strategy
|
Chen, Xiao-qian
|
|
2017
|
133 |
C |
p. 63-72
|
artikel
|
| 32 |
Propulsion options for very low Earth orbit microsatellites
|
Leomanni, Mirko
|
|
2017
|
133 |
C |
p. 444-454
|
artikel
|
| 33 |
Recovery rate prediction in lunar regolith simulant drilling
|
Quan, Qiquan
|
|
2017
|
133 |
C |
p. 121-127
|
artikel
|
| 34 |
Simultaneous detection of multiple debris via a cascade of numerical evaluations and a voting scheme for lines in an image sequence
|
Fujita, Koki
|
|
2017
|
133 |
C |
p. 416-422
|
artikel
|
| 35 |
Southern Meridiani Planum - A candidate landing site for the first crewed mission to Mars
|
Clarke, J.D.A.
|
|
2017
|
133 |
C |
p. 195-220
|
artikel
|
| 36 |
The cislunar polygonal-like periodic orbit: Construction, transition and its application
|
Liang, Yuying
|
|
2017
|
133 |
C |
p. 282-301
|
artikel
|
| 37 |
The optimisation of low-acceleration interstellar relativistic rocket trajectories using genetic algorithms
|
Fung, Kenneth K.H.
|
|
2017
|
133 |
C |
p. 258-268
|
artikel
|
| 38 |
Thermoelastic buckling analysis of pre-twisted functionally graded beams with temperature-dependent material properties
|
Shenas, Amin Ghorbani
|
|
2017
|
133 |
C |
p. 1-13
|
artikel
|
| 39 |
The science planning process on the Rosetta mission
|
Vallat, Claire
|
|
2017
|
133 |
C |
p. 244-257
|
artikel
|
| 40 |
Toward lean satellites reliability improvement using HORYU-IV project as case study
|
Faure, Pauline
|
|
2017
|
133 |
C |
p. 33-49
|
artikel
|
| 41 |
Transfer from Earth to libration point orbit using lunar gravity assist
|
Qi, Yi
|
|
2017
|
133 |
C |
p. 145-157
|
artikel
|
| 42 |
Transfer to near-Earth asteroids from a lunar orbit via Earth flyby and direct escaping trajectories
|
Wang, Yamin
|
|
2017
|
133 |
C |
p. 177-184
|
artikel
|
| 43 |
Vortex-induced vibration for an isolated circular cylinder under the wake interference of an oscillating airfoil: Part II. Single degree of freedom
|
Zhang, G.Q.
|
|
2017
|
133 |
C |
p. 311-323
|
artikel
|
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