G. Krülle

发表

End-Of-Life De-Orbiting Strategies for Satellites

M. Kassebom, R. Janovsky, H. Lübberstedt, 2003 .

Ignition Sequence and High pressure Steady State Simulation of H2/O2 Model Engine Combustion Chamber Condition

G. Krülle, C.-A. Schley, V. Golovitchev, 1995 .

Turbulence Modeling in High Pressure H2/O2 Rocket Engines

G. Hagemann, G. Krülle, C.-A. Schley, 1995 .

Cryogenic High Pressure Coaxial Injection and Atomization: Experiments and Modeling

G. Krülle, G. Krülle, C.-A. Schley, 1995 .

Chemical Propulsion Research and Development in Germany.

G. Krülle, P. A. Kramer, 1992 .

Fluid Injection Process in High Pressure H2/O2 Rocket Engines: derived models and numerical simulations

G. Krülle, C.-A. Schley, 1995 .

Evaluation of Propulsion Systems for Satellite End-Of-Life De.Orbiting

M. Kassebom, R. Janovsky, H. Lübberstedt, 2002 .

Towards an optimal concept for numerical codes simulating thrust chamber processes in high pressure chemical propulsion systems

G. Hagemann, G. Krülle, C.-A. Schley, 1997 .

Research and Test Field at Lampoldshausen.

G. Krülle, G. Tofahrn, 1993 .