+ Home
+ Lebenslauf
+ Veröffentlichungen
+ Links
+ Kontakt
Veröffentlichungen
(pdf-Datei)
[1]
Lux, J.; Suslov, D.; Bechle, M.; Oschwald, M; Haidn, O.:
Investigation of Sub- and Supercritical LOX/Methane Injection using Optical Diagnostics
. 42nd
AIAA
/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. Sacramento, CA, July 2006.
[2]
Lux, J.; Zell, D.; Suslov, D.; Haidn, O.:
Untersuchungen transkritischer CH4/O2-Mischungen
.
Deutscher Luft- und Raumfahrtkongress
, Braunschweig, 2006.
[3]
Suslov, D.; Lux, J.; Haidn, O.:
Investigation of porous injectors for LOX/CH4 and LOX/H2 combustion at sub- and supercritical conditions
. 2nd European Conference for Aero-Space Sciences
EUCASS
, Brussels, Belgium, 2007.
[4]
Lux, J.; Suslov, D.; Haidn, O.:
Porous Injectors in Cryogenic Liquid Propellant Rocket Engines at Sub- and Supercritical Pressures
. 46th
AIAA
Aerospace Sciences Meeting and Exhibit. Reno, NV, 2008.
[5]
Lux, J.; Suslov, D.; Haidn, O.:
On porous liquid propellant rocket engine injectors
.
Aerospace Science and Technology
, Vol. 12, No. 6, pp. 469-477, 2008.
[6]
Lux, J.; Suslov, D.; Haidn, O.:
Experimental Investigation of Porous Injectors for Liquid Propellant Rocket Engines
. 44th
AIAA
/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. Hartford, CT, 2008.
[7]
Lux, J.; Haidn, O.:
Flame stabilization in high pressure Liquid Oxygen (LOX)/Methane rocket engine combustion
. Journal of Propulsion and Power, Vol. 25, No. 1, pp. 15-23, 2009.
[8]
Lux, J.; Haidn, O.:
Effect of recess in high pressure Liquid Oxygen (LOX)/Methane coaxial injection and combustion
. Journal of Propulsion and Power, Vol. 25, No. 1, pp. 24-32, 2009.
[9]
Konopka, M.; Lux, J.; Haidn, O.:
Optimierung eines neuartigen Injektors für kryogene Raketentriebwerke
.
Deutscher Luft- und Raumfahrtkongress
, Darmstadt, 2008.
[10]
Wilkosz, B.; Lux, J.; Haidn, O.:
Theoretische Grundlagen und Konzeptanalyse eines Laserzündsystems für kryogene Raketentriebwerke
.
Deutscher Luft- und Raumfahrtkongress
, Darmstadt, 2008.