In 2015 and 2016, the National Aeronautics and Space Administration Marshall Space Flight Center designed, fabricated, assembled and hot-fire tested an oxygen/RP-1 propellant multi-element oxidizer-rich staged-combustion test article. The main objective was to provide thrust chamber combustion stability data as part of the Combustion Stability Tool Development program, although demonstration of performance and compatibility of oxidizer-rich main injectors was also important. Funding was provided by the Air Force Space and Missile Systems Center. Five configurations of main injectors were designed and fabricated, using conventional gas-centered swirl coaxial injector element designs generally similar to those used in oxygen/kerosene oxidizer...
A prototype integrated liquid oxygen/liquid methane propulsion system was hot-fire tested at a varie...
Results of an evaluation of high pressure combustion of fuel rich and oxidizer rich LOX/RP-1 propell...
To support the NASA Space Exploration Mission, an in-house program called Combustion Devices Injecto...
As part of the Combustion Stability Tool Development project funded by the Air Force Space and Missi...
As part of the Combustion Stability Tool Development project funded by the Air Force Space and Missi...
As part of the Combustion Stability Tool Development project funded by the Air Force Space and Missi...
The Combustion Stability Tool Development (CSTD) project, funded by the Air Force Space and Missile ...
Liquid rocket engines using oxygen and methane propellants are being considered by the National Aero...
Injector design criteria are provided for gaseous hydrogen-gaseous oxygen propellants. Design equati...
The identification and characterization of oxygen-rich compatible materials enables full-flow, stage...
NASA Marshall Space Flight Center (MSFC) has embarked upon a joint project with the Air Force to imp...
An experimental program was conducted to investigate the rocket combustion and heat transfer charact...
A summary of the design analyses for a liquid rocket injector using oxygen and RP-1 propellants at h...
Rocket engines achieve extraordinary high energy densities within the chamber in the form of high pr...
An investigation of oxygen compatibility and resistance to ignition of candidate materials for use i...
A prototype integrated liquid oxygen/liquid methane propulsion system was hot-fire tested at a varie...
Results of an evaluation of high pressure combustion of fuel rich and oxidizer rich LOX/RP-1 propell...
To support the NASA Space Exploration Mission, an in-house program called Combustion Devices Injecto...
As part of the Combustion Stability Tool Development project funded by the Air Force Space and Missi...
As part of the Combustion Stability Tool Development project funded by the Air Force Space and Missi...
As part of the Combustion Stability Tool Development project funded by the Air Force Space and Missi...
The Combustion Stability Tool Development (CSTD) project, funded by the Air Force Space and Missile ...
Liquid rocket engines using oxygen and methane propellants are being considered by the National Aero...
Injector design criteria are provided for gaseous hydrogen-gaseous oxygen propellants. Design equati...
The identification and characterization of oxygen-rich compatible materials enables full-flow, stage...
NASA Marshall Space Flight Center (MSFC) has embarked upon a joint project with the Air Force to imp...
An experimental program was conducted to investigate the rocket combustion and heat transfer charact...
A summary of the design analyses for a liquid rocket injector using oxygen and RP-1 propellants at h...
Rocket engines achieve extraordinary high energy densities within the chamber in the form of high pr...
An investigation of oxygen compatibility and resistance to ignition of candidate materials for use i...
A prototype integrated liquid oxygen/liquid methane propulsion system was hot-fire tested at a varie...
Results of an evaluation of high pressure combustion of fuel rich and oxidizer rich LOX/RP-1 propell...
To support the NASA Space Exploration Mission, an in-house program called Combustion Devices Injecto...