Add to ORKGThe influence of using different chemistry model and different chemical kinetics schemes on modeling combustion inside a rocket engine igniter are investigated. An igniter for a LOX/CH4 rocket engine is designed and a CFD model is developed which is used to model the designed igniter. Verification and validation methods are discussed.Aerospace Engineerin
There are many advantages to LOX/methane propulsion, such as in-situ resource utilization from Mars ...
The article describes a method of simulating combustion processes in a low-thrust rocket engine. The...
Over the years methane and natural gas (NG) as a fuel have become an important source of energy in t...
Methane has never been used as rocket fuel in a flight mission up to now. However, for upper stage ...
The current work is devoted to studying combustion initiation inside the methane-oxygen torch ignite...
The current work is devoted to studying combustion initiation inside the methane-oxygen torch ignite...
The rocket ejector refers to a core component of a rocket-based combined cycle (RBCC) engine. The ig...
It is known that during a launch of a rocket, the interaction of the exhaust gases of rocket engines...
Methane, which has properties intermediate between hydrogen and kerosene, is a fuel of several devel...
Methane, which has properties intermediate between hydrogen and kerosene, is a fuel of several devel...
Methane, which has properties intermediate between hydrogen and kerosene, is a fuel of several devel...
The ignition of methane by laser spark in a small combustion chamber has been modelled using CFD-cod...
It is known that during a launch of a rocket, the interaction of the exhaust gas...
It is known that during a launch of a rocket, the interaction of the exhaust gas...
There are many advantages to LOX/methane propulsion, such as in-situ resource utilization from Mars ...
There are many advantages to LOX/methane propulsion, such as in-situ resource utilization from Mars ...
The article describes a method of simulating combustion processes in a low-thrust rocket engine. The...
Over the years methane and natural gas (NG) as a fuel have become an important source of energy in t...
Methane has never been used as rocket fuel in a flight mission up to now. However, for upper stage ...
The current work is devoted to studying combustion initiation inside the methane-oxygen torch ignite...
The current work is devoted to studying combustion initiation inside the methane-oxygen torch ignite...
The rocket ejector refers to a core component of a rocket-based combined cycle (RBCC) engine. The ig...
It is known that during a launch of a rocket, the interaction of the exhaust gases of rocket engines...
Methane, which has properties intermediate between hydrogen and kerosene, is a fuel of several devel...
Methane, which has properties intermediate between hydrogen and kerosene, is a fuel of several devel...
Methane, which has properties intermediate between hydrogen and kerosene, is a fuel of several devel...
The ignition of methane by laser spark in a small combustion chamber has been modelled using CFD-cod...
It is known that during a launch of a rocket, the interaction of the exhaust gas...
It is known that during a launch of a rocket, the interaction of the exhaust gas...
There are many advantages to LOX/methane propulsion, such as in-situ resource utilization from Mars ...
There are many advantages to LOX/methane propulsion, such as in-situ resource utilization from Mars ...
The article describes a method of simulating combustion processes in a low-thrust rocket engine. The...
Over the years methane and natural gas (NG) as a fuel have become an important source of energy in t...