Add to ORKGIgnition sensor, utilizing fluidic oscillator device and its ability to react to flow system's molecular weight and temperature changes, detects propellant ignition. Commercial applications include fields of fire protection equipment and fluidics
There are many advantages to LOX/methane propulsion, such as in-situ resource utilization from Mars ...
A series of contracts were issued by the Marshall Space Flight Center (MSFC) of the National Aeronau...
A feedback free fluidic oscillator was designed and integrated into a single element rocket combusto...
In-like transducers system measures flow rate of chemically active propellant fluids. The system use...
Test program evaluates thermal and electric ignition mechanisms in selected nonmetallic materials fo...
A device has been developed which monitors the presence of a flame within a combustion chamber. The ...
Device simulates incipient fire conditions in closely-controlled adjustable manner, to give predeter...
A fluidic oscillator was investigated for use in measuring fuel-air ratios in hydrocarbon combustion...
A hydrogen gas sensor that can replace catalytic combustion sensors used to detect leaks in the liqu...
Fire protection of critical space assets, including launch and fueling facilities and manned flight ...
In recent years NASA has had a renewed interest in oxygen and methane as propellants for propulsion....
Because the liquid hydrogen which NASA stores for the space shuttle engines is easily ignited, a han...
In recent years NASA has had a renewed interest in oxygen and methane as propellants for propulsion....
Heated element sensor for fluid flow detection in thermal conductive conduit with adaptive means to ...
Prototype propellant leakage detection system for space flight propulsion system
There are many advantages to LOX/methane propulsion, such as in-situ resource utilization from Mars ...
A series of contracts were issued by the Marshall Space Flight Center (MSFC) of the National Aeronau...
A feedback free fluidic oscillator was designed and integrated into a single element rocket combusto...
In-like transducers system measures flow rate of chemically active propellant fluids. The system use...
Test program evaluates thermal and electric ignition mechanisms in selected nonmetallic materials fo...
A device has been developed which monitors the presence of a flame within a combustion chamber. The ...
Device simulates incipient fire conditions in closely-controlled adjustable manner, to give predeter...
A fluidic oscillator was investigated for use in measuring fuel-air ratios in hydrocarbon combustion...
A hydrogen gas sensor that can replace catalytic combustion sensors used to detect leaks in the liqu...
Fire protection of critical space assets, including launch and fueling facilities and manned flight ...
In recent years NASA has had a renewed interest in oxygen and methane as propellants for propulsion....
Because the liquid hydrogen which NASA stores for the space shuttle engines is easily ignited, a han...
In recent years NASA has had a renewed interest in oxygen and methane as propellants for propulsion....
Heated element sensor for fluid flow detection in thermal conductive conduit with adaptive means to ...
Prototype propellant leakage detection system for space flight propulsion system
There are many advantages to LOX/methane propulsion, such as in-situ resource utilization from Mars ...
A series of contracts were issued by the Marshall Space Flight Center (MSFC) of the National Aeronau...
A feedback free fluidic oscillator was designed and integrated into a single element rocket combusto...