The application of existing and new technology to the problem of determining the long-term performance capability of liquid rocket propulsion feed systems is discussed. The long term performance of metal to metal valve seats in a liquid propellant fuel system is stressed. The approaches taken in conducting the analysis are: (1) advancing the technology of characterizing components through the development of new or more sensitive techniques and (2) improving the understanding of the physical of degradation
Lewis Research Center is developing broad-based new technologies for space chemical engines to satis...
Bipropellant rocket engines with radiation cooled thrust combustion chambers of molybdenum fired for...
State of the art and design criteria for components used in liquid propellant rocket propulsion syst...
A study was conducted of techniques having the capability of determining the performance and reliabi...
The search for advanced measurement techniques for determining long term compatibility of materials ...
With the advent of the space age, new adjustments in technical thinking and engineering experience a...
The objective was to apply powder metallurgy techniques for the production of improved bearing eleme...
A chemical analysis of the emission and absorption spectra in the combustion chamber of a nitrogen t...
Selection technique to determine most suitable liquid propellant pressurization systems for various ...
The analyses and results of a test program to establish the effects of long term (10 years or more) ...
A monograph on valves for use with liquid rocket propellant engines is presented. The configurations...
Apparatus, techniques, and instrumentation for experimental correlation of nonreactive injection sch...
Compatibility measurements were made for aluminum 2219-T87 alloy and titanium 6Al-4V alloy in the pr...
Boundary flow composition in rocket motor combustion chamber with exhaust system samplin
Mechanical stress effects on permeability of engineering materials to cryogenic and storable launch ...
Lewis Research Center is developing broad-based new technologies for space chemical engines to satis...
Bipropellant rocket engines with radiation cooled thrust combustion chambers of molybdenum fired for...
State of the art and design criteria for components used in liquid propellant rocket propulsion syst...
A study was conducted of techniques having the capability of determining the performance and reliabi...
The search for advanced measurement techniques for determining long term compatibility of materials ...
With the advent of the space age, new adjustments in technical thinking and engineering experience a...
The objective was to apply powder metallurgy techniques for the production of improved bearing eleme...
A chemical analysis of the emission and absorption spectra in the combustion chamber of a nitrogen t...
Selection technique to determine most suitable liquid propellant pressurization systems for various ...
The analyses and results of a test program to establish the effects of long term (10 years or more) ...
A monograph on valves for use with liquid rocket propellant engines is presented. The configurations...
Apparatus, techniques, and instrumentation for experimental correlation of nonreactive injection sch...
Compatibility measurements were made for aluminum 2219-T87 alloy and titanium 6Al-4V alloy in the pr...
Boundary flow composition in rocket motor combustion chamber with exhaust system samplin
Mechanical stress effects on permeability of engineering materials to cryogenic and storable launch ...
Lewis Research Center is developing broad-based new technologies for space chemical engines to satis...
Bipropellant rocket engines with radiation cooled thrust combustion chambers of molybdenum fired for...
State of the art and design criteria for components used in liquid propellant rocket propulsion syst...