Add to ORKGIgnition data for tests with a LOX/methane igniter that utilized a glow plug as the ignition source are presented. The tests were conducted in a vacuum can with thermally conditioned (cold) hardware. Data showing the effects of glow plug geometry, type, and igniter operating conditions are discussed. Comparisons between experimental results and multidimensional, transient computer models are also made
Lean Direct Injection (LDI) is a combustor concept that reduces nitrogen oxides (NOx) emissions. Thi...
This study sought to develop a catalytic ignition advanced torch system with a unique catalyst micro...
The National Aeronautics & Space Administration (NASA) has identified Liquid Oxygen (LOX)/Liquid Met...
The LOX/methane propellant combination is being considered for the Lunar Surface Access Module ascen...
A coil-on-plug ignition system has been developed and tested for Liquid Oxygen (LOX) / liquid methan...
The Lunar Cargo Transportation and Landing by Soft Touchdown (Lunar CATALYST) program is establishin...
A prototype integrated liquid oxygen/liquid methane propulsion system was hot-fire tested at a varie...
In support of NASA's efforts to advance methane technology for future exploration missions, two diff...
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 use of non-toxic propellants in future exploration vehicles would enable safer, more cost effect...
The Lunar Cargo Transportation and Landing by Soft Touchdown (Lunar CATALYST) program is establishin...
A relocated rocket engine test facility, the Altitude Combustion Stand (ACS), was activated in 2009 ...
Test program evaluates thermal and electric ignition mechanisms in selected nonmetallic materials fo...
In support of a facility characterization test, the Integrated Cryogenic Propulsion Test Article (IC...
Lean Direct Injection (LDI) is a combustor concept that reduces nitrogen oxides (NOx) emissions. Thi...
This study sought to develop a catalytic ignition advanced torch system with a unique catalyst micro...
The National Aeronautics & Space Administration (NASA) has identified Liquid Oxygen (LOX)/Liquid Met...
The LOX/methane propellant combination is being considered for the Lunar Surface Access Module ascen...
A coil-on-plug ignition system has been developed and tested for Liquid Oxygen (LOX) / liquid methan...
The Lunar Cargo Transportation and Landing by Soft Touchdown (Lunar CATALYST) program is establishin...
A prototype integrated liquid oxygen/liquid methane propulsion system was hot-fire tested at a varie...
In support of NASA's efforts to advance methane technology for future exploration missions, two diff...
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 use of non-toxic propellants in future exploration vehicles would enable safer, more cost effect...
The Lunar Cargo Transportation and Landing by Soft Touchdown (Lunar CATALYST) program is establishin...
A relocated rocket engine test facility, the Altitude Combustion Stand (ACS), was activated in 2009 ...
Test program evaluates thermal and electric ignition mechanisms in selected nonmetallic materials fo...
In support of a facility characterization test, the Integrated Cryogenic Propulsion Test Article (IC...
Lean Direct Injection (LDI) is a combustor concept that reduces nitrogen oxides (NOx) emissions. Thi...
This study sought to develop a catalytic ignition advanced torch system with a unique catalyst micro...
The National Aeronautics & Space Administration (NASA) has identified Liquid Oxygen (LOX)/Liquid Met...