| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
An adaptive paradigm for human space settlement
|
Smith, Cameron M.
|
|
2016
|
119 |
C |
p. 207-217
11 p.
|
artikel
|
| 2 |
An approximate model for pulsar navigation simulation
|
Jovanovic, Ilija
|
|
2016
|
119 |
C |
p. 101-109
9 p.
|
artikel
|
| 3 |
A new terminal guidance sensor system for asteroid intercept or rendezvous missions
|
Lyzhoft, Joshua
|
|
2016
|
119 |
C |
p. 147-159
13 p.
|
artikel
|
| 4 |
A study on simultaneous design of a Hall Effect Thruster and its low-thrust trajectory
|
Kwon, Kybeom
|
|
2016
|
119 |
C |
p. 34-47
14 p.
|
artikel
|
| 5 |
Bending analysis of embedded carbon nanotubes resting on an elastic foundation using strain gradient theory
|
Akgöz, Bekir
|
|
2016
|
119 |
C |
p. 1-12
12 p.
|
artikel
|
| 6 |
Constrained tension control of a tethered space-tug system with only length measurement
|
Wen, Hao
|
|
2016
|
119 |
C |
p. 110-117
8 p.
|
artikel
|
| 7 |
Design of geodesic cable net for space deployable mesh reflectors
|
Deng, Hanqing
|
|
2016
|
119 |
C |
p. 13-21
9 p.
|
artikel
|
| 8 |
Design of robotic manipulators for orbit removal of spent launchers’ stages
|
Felicetti, Leonard
|
|
2016
|
119 |
C |
p. 118-130
13 p.
|
artikel
|
| 9 |
Determination of the force transmitted by an ion thruster plasma plume to an orbital object
|
Alpatov, A.
|
|
2016
|
119 |
C |
p. 241-251
11 p.
|
artikel
|
| 10 |
Dipole solution and angular-momentum minimization for two-satellite electromagnetic formation flight
|
Huang, Xian-lin
|
|
2016
|
119 |
C |
p. 79-86
8 p.
|
artikel
|
| 11 |
Electrostatic spacecraft rate and attitude control—Experimental results and performance considerations
|
Stevenson, Daan
|
|
2016
|
119 |
C |
p. 22-33
12 p.
|
artikel
|
| 12 |
Hypervelocity impact performance of aluminum egg-box panel enhanced Whipple shield
|
Zhang, Xiaotian
|
|
2016
|
119 |
C |
p. 48-59
12 p.
|
artikel
|
| 13 |
Identification of new orbits to enable future mission opportunities for the human exploration of the Martian moon Phobos
|
Zamaro, Mattia
|
|
2016
|
119 |
C |
p. 160-182
23 p.
|
artikel
|
| 14 |
IFC - Publication Information
|
|
|
2016
|
119 |
C |
p. IFC-
1 p.
|
artikel
|
| 15 |
Mass breakdown model of solar-photon sail shuttle: The case for Mars
|
Vulpetti, Giovanni
|
|
2016
|
119 |
C |
p. 87-100
14 p.
|
artikel
|
| 16 |
Minimum ΔV for the transfer to permanent lunar orbits with hyperbolic approach
|
Qi, Yi
|
|
2016
|
119 |
C |
p. 183-195
13 p.
|
artikel
|
| 17 |
Model of turbulent destruction of molecular clouds
|
Rybakin, B.P.
|
|
2016
|
119 |
C |
p. 131-136
6 p.
|
artikel
|
| 18 |
Polyhedral representation of invariant manifolds applied to orbit transfers in the Earth–Moon system
|
Pontani, Mauro
|
|
2016
|
119 |
C |
p. 218-232
15 p.
|
artikel
|
| 19 |
Pull-in instability of paddle-type and double-sided NEMS sensors under the accelerating force
|
Keivani, M.
|
|
2016
|
119 |
C |
p. 196-206
11 p.
|
artikel
|
| 20 |
Regression rate behaviors of HTPB-based propellant combinations for hybrid rocket motor
|
Sun, Xingliang
|
|
2016
|
119 |
C |
p. 137-146
10 p.
|
artikel
|
| 21 |
Retraction notice to: “Analytical orbit predictions for low and high eccentricity orbits using uniformly regular KS canonical elements in an oblate atmosphere” [Acta Astronaut. 110 (2015) 214–224]
|
Rajendran, P.S.
|
|
2016
|
119 |
C |
p. 252-
1 p.
|
artikel
|
| 22 |
Robust Mars atmospheric entry integrated navigation based on parameter sensitivity
|
Lou, Taishan
|
|
2016
|
119 |
C |
p. 60-70
11 p.
|
artikel
|
| 23 |
The effects of low earth orbit atomic oxygen on the properties of Polytetrafluoroethylene
|
Hooshangi, Zhila
|
|
2016
|
119 |
C |
p. 233-240
8 p.
|
artikel
|
| 24 |
Torque distribution of The Integrated Magnetically Suspended Inertia Actuator for attitude maneuvers
|
Yu, Yuanjin
|
|
2016
|
119 |
C |
p. 71-78
8 p.
|
artikel
|
Tijdschrift beschrijving