| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
A fluid structure coupling of the Ariane-5 nozzle section during start phase by detached eddy simulation
|
Lüdeke, Heinrich
|
|
2010
|
|
1-4 |
p. 33-44
|
artikel
|
| 2 |
Airborne re-entry observation experiment SLIT: UV spectroscopy during STARDUST and ATV1 re-entry
|
Löhle, Stefan
|
|
2010
|
|
1-4 |
p. 59-69
|
artikel
|
| 3 |
An experimental demonstration of Network Coding for satellite networks
|
Bischl, Hermann
|
|
2011
|
|
1-4 |
p. 75-83
|
artikel
|
| 4 |
Antennas for multiple spot beam satellites
|
Schneider, Michael
|
|
2011
|
|
1-4 |
p. 59-66
|
artikel
|
| 5 |
A reliability as an independent variable (RAIV) methodology for optimizing test planning for liquid rocket engines
|
Strunz, Richard
|
|
2011
|
|
1-4 |
p. 17-30
|
artikel
|
| 6 |
Design and implementation of an internal stress wave force balance in a shock tunnel
|
Robinson, M. J.
|
|
2010
|
|
1-4 |
p. 45-57
|
artikel
|
| 7 |
Design of hypersonic flight vehicles: some lessons from the past and future challenges
|
Hirschel, E. H.
|
|
2010
|
|
1-4 |
p. 3-22
|
artikel
|
| 8 |
Editorial
|
Stavrinidis, Constantinos
|
|
2011
|
|
1-4 |
p. 1-2
|
artikel
|
| 9 |
Editorial
|
Müller-Wiesner, Detlef
|
|
2011
|
|
1-4 |
p. 1
|
artikel
|
| 10 |
Flame response to acoustic excitation in a rectangular rocket combustor with LOx/H2 propellants
|
Hardi, Justin
|
|
2011
|
|
1-4 |
p. 41-49
|
artikel
|
| 11 |
Implementation of concurrent engineering to Phase B space system design
|
Findlay, R.
|
|
2011
|
|
1-4 |
p. 51-58
|
artikel
|
| 12 |
Laser communication applied for EDRS, the European data relay system
|
Heine, F.
|
|
2011
|
|
1-4 |
p. 85-90
|
artikel
|
| 13 |
Lessons learnt from ground testing the Saturn family of rockets
|
Lawrie, Alan
|
|
2013
|
|
1-4 |
p. 1-12
|
artikel
|
| 14 |
Life prediction of thermally highly loaded components: modelling the damage process of a rocket combustion chamber hot wall
|
Schwarz, W.
|
|
2011
|
|
1-4 |
p. 83-97
|
artikel
|
| 15 |
Link budget analysis for future E-band gigabit satellite communication links (71–76 and 81–84 Ghz)
|
Lewark, U. J.
|
|
2013
|
|
1-4 |
p. 41-46
|
artikel
|
| 16 |
New materials and processes for field emission ion and electron emitters
|
Tajmar, M.
|
|
2013
|
|
1-4 |
p. 47-54
|
artikel
|
| 17 |
On the importance of reduced scale Ariane 5 P230 solid rocket motor models in the comprehension and prevention of thrust oscillations
|
Hijlkema, J.
|
|
2011
|
|
1-4 |
p. 99-107
|
artikel
|
| 18 |
Physical and numerical aspects of the high-speed unsteady flow around concave axisymmetric bodies
|
Panaras, Argyris
|
|
2010
|
|
1-4 |
p. 23-32
|
artikel
|
| 19 |
Precision pointing H∞ control design for absolute, window-, and stability-time errors
|
Ott, T.
|
|
2013
|
|
1-4 |
p. 13-30
|
artikel
|
| 20 |
Reusability aspects for space transportation rocket engines: programmatic status and outlook
|
Preclik, D.
|
|
2011
|
|
1-4 |
p. 71-82
|
artikel
|
| 21 |
Simulation of a GOX–kerosene subscale rocket combustion chamber
|
Höglauer, Christoph
|
|
2011
|
|
1-4 |
p. 31-40
|
artikel
|
| 22 |
Test facilities for SCORE-D
|
Greuel, Dirk
|
|
2013
|
|
1-4 |
p. 55-69
|
artikel
|
| 23 |
The cosmic dust analyser onboard cassini: ten years of discoveries
|
Srama, R.
|
|
2011
|
|
1-4 |
p. 3-16
|
artikel
|
| 24 |
Validation of equivalent viscous damping methodologies
|
Vaquer Araujo, Xavier
|
|
2013
|
|
1-4 |
p. 31-39
|
artikel
|
| 25 |
Verification of new technologies as main task of the communication payload of the Heinrich-Hertz mission
|
Schallner, Martin
|
|
2011
|
|
1-4 |
p. 67-73
|
artikel
|
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