| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
A bionic approach to mathematical modeling the fold geometry of deployable reflector antennas on satellites
|
Feng, C.M.
|
|
2014
|
103 |
C |
p. 36-44
9 p.
|
artikel
|
| 2 |
Active debris multi-removal mission concept based on hybrid propulsion
|
Tadini, P.
|
|
2014
|
103 |
C |
p. 26-35
10 p.
|
artikel
|
| 3 |
A decision analysis approach for risk management of near-earth objects
|
Lee, Robert C.
|
|
2014
|
103 |
C |
p. 362-369
8 p.
|
artikel
|
| 4 |
Advanced degrees in astronautical engineering for the space industry
|
Gruntman, Mike
|
|
2014
|
103 |
C |
p. 92-105
14 p.
|
artikel
|
| 5 |
Airburst warning and response
|
Boslough, Mark
|
|
2014
|
103 |
C |
p. 370-375
6 p.
|
artikel
|
| 6 |
An empirical modified fatigue damage model for impacted GFRP laminates
|
Naderi, S.
|
|
2014
|
103 |
C |
p. 119-128
10 p.
|
artikel
|
| 7 |
A real-time prognostic method for the drift errors in the inertial navigation system by a nonlinear random-coefficient regression model
|
Wang, Zhaoqiang
|
|
2014
|
103 |
C |
p. 45-54
10 p.
|
artikel
|
| 8 |
A space-to-space microwave wireless power transmission experiential mission using small satellites
|
Bergsrud, Corey
|
|
2014
|
103 |
C |
p. 193-203
11 p.
|
artikel
|
| 9 |
Automated image analysis for space debris identification and astrometric measurements
|
Piattoni, Jacopo
|
|
2014
|
103 |
C |
p. 176-184
9 p.
|
artikel
|
| 10 |
Blow-off momentum from melt and vapor in nuclear deflection scenarios
|
Howley, Kirsten
|
|
2014
|
103 |
C |
p. 376-381
6 p.
|
artikel
|
| 11 |
China׳s space development history: A comparison of the rocket and satellite sectors
|
Erickson, Andrew S.
|
|
2014
|
103 |
C |
p. 142-167
26 p.
|
artikel
|
| 12 |
Closed loop terminal guidance navigation for a kinetic impactor spacecraft
|
Bhaskaran, Shyam
|
|
2014
|
103 |
C |
p. 322-332
11 p.
|
artikel
|
| 13 |
Dawn׳s operations in cruise from Vesta to Ceres
|
Rayman, Marc D.
|
|
2014
|
103 |
C |
p. 113-118
6 p.
|
artikel
|
| 14 |
Design and development of a gossamer sail system for deorbiting in low earth orbit
|
Fernandez, Juan M.
|
|
2014
|
103 |
C |
p. 204-225
22 p.
|
artikel
|
| 15 |
Detecting accelerometric nonlinearities in the international space station
|
Sáez, N.
|
|
2014
|
103 |
C |
p. 16-25
10 p.
|
artikel
|
| 16 |
Dynamics of highly-flexible solar sail subjected to various forces
|
Liu, Jiafu
|
|
2014
|
103 |
C |
p. 55-72
18 p.
|
artikel
|
| 17 |
Hazardous near Earth asteroid mitigation campaign planning based on uncertain information on fundamental asteroid characteristics
|
Sugimoto, Y.
|
|
2014
|
103 |
C |
p. 333-357
25 p.
|
artikel
|
| 18 |
Hypersonic static aerodynamics for Mars science laboratory entry capsule
|
Yang, Xiaofeng
|
|
2014
|
103 |
C |
p. 168-175
8 p.
|
artikel
|
| 19 |
IFC - Publication Information
|
|
|
2014
|
103 |
C |
p. IFC-
1 p.
|
artikel
|
| 20 |
Impact decision support diagrams
|
Boslough, Mark
|
|
2014
|
103 |
C |
p. 358-361
4 p.
|
artikel
|
| 21 |
Improved laser ablation model for asteroid deflection
|
Vasile, Massimiliano
|
|
2014
|
103 |
C |
p. 382-394
13 p.
|
artikel
|
| 22 |
Influencing factors on the mode transition in a dual-mode scramjet
|
Yan, Zhang
|
|
2014
|
103 |
C |
p. 1-15
15 p.
|
artikel
|
| 23 |
International space station accomplishments update: Scientific discovery, advancing future exploration, and benefits brought home to earth
|
Thumm, Tracy
|
|
2014
|
103 |
C |
p. 235-242
8 p.
|
artikel
|
| 24 |
Mars transportation vehicle concept
|
Smirnova, Maria
|
|
2014
|
103 |
C |
p. 250-256
7 p.
|
artikel
|
| 25 |
Maximum-likelihood estimation optimizer for constrained, time-optimal satellite reorientation
|
Melton, Robert G.
|
|
2014
|
103 |
C |
p. 185-192
8 p.
|
artikel
|
| 26 |
Measurement of regression rate in hybrid rocket using combustion chamber pressure
|
Kumar, Rajiv
|
|
2014
|
103 |
C |
p. 226-234
9 p.
|
artikel
|
| 27 |
Mission operations of the handicapped FORMOSAT-2
|
Lin, Shin-Fa
|
|
2014
|
103 |
C |
p. 243-249
7 p.
|
artikel
|
| 28 |
Mission opportunities for the flight validation of the kinetic impactor concept for asteroid deflection
|
Hernandez, Sonia
|
|
2014
|
103 |
C |
p. 309-321
13 p.
|
artikel
|
| 29 |
Modeling tether–ballast asteroid diversion systems, including tether mass and elasticity
|
French, David B.
|
|
2014
|
103 |
C |
p. 282-306
25 p.
|
artikel
|
| 30 |
Multiple spacecraft formation reconfiguration using solar radiation pressure
|
Shahid, Kamran
|
|
2014
|
103 |
C |
p. 269-281
13 p.
|
artikel
|
| 31 |
NEO Planetary Defense 2013: Gathering for impact
|
Carnelli, Ian
|
|
2014
|
103 |
C |
p. 307-308
2 p.
|
artikel
|
| 32 |
Numerical investigation of air stability in space capsule under low gravity conditions
|
Wang, Yadi
|
|
2014
|
103 |
C |
p. 81-91
11 p.
|
artikel
|
| 33 |
Numerical simulation of non-equilibrium plasma flow in a cylindrical MPD thruster using a high-order flux-difference splitting method
|
Ahangar, Mahdy
|
|
2014
|
103 |
C |
p. 129-141
13 p.
|
artikel
|
| 34 |
Psychosocial issues during an expedition to Mars
|
Kanas, Nick
|
|
2014
|
103 |
C |
p. 73-80
8 p.
|
artikel
|
| 35 |
Shape optimization and material gradient design of the sharp hot structure
|
Ma, Yinji
|
|
2014
|
103 |
C |
p. 106-112
7 p.
|
artikel
|
| 36 |
Sliding mode control for Lorentz-augmented spacecraft hovering around elliptic orbits
|
Huang, Xu
|
|
2014
|
103 |
C |
p. 257-268
12 p.
|
artikel
|
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