The available information on the compatibility of materials with oxygen as applied to the production, transport, and applications experience of high pressure liquid and gaseous oxygen is compiled. High pressure is defined as about 2000 to 3000 psia. Since high pressure projections sometimes can be made from lower pressure data, some low pressure data are also included. Low pressure data are included if they are considered helpful to a better understanding of the behavior at high pressures
Particle impact and frictional heating tests of metals in high pressure oxygen, are conducted in sup...
Advances in the design of the liquid oxygen, liquid hydrogen engines for the Space Transportation Sy...
The requirements for impact testing of materials in an oxygen atmosphere at pressures from 82.7 MPa ...
Although NASA is not one of the country's major oxygen consumers, it uses oxygen under severe condit...
A repository for critical and important detailed design data and information, hitherto unpublished, ...
The sensitivity of materials in contact with gaseous oxygen (GOX) or liquid oxygen (LOX) was examine...
The use of oxygen for aerospace applications is bonded to the history of American rocketry. The firs...
Brief discussions of the materials and configurations testing techniques and requirements for the Ap...
As a result of the Apollo 13 incident, increased emphasis is being placed on materials compatibility...
SIGLEAvailable from British Library Document Supply Centre- DSC:DX178271 / BLDSC - British Library D...
Thermodynamic and related properties of oxygen from experimental pressure-volume-temperature measure...
Materials used in oxygen systems and allowable oxygen environments are specified for each material. ...
Precision measurements of the properties of oxygen over a wide range of temperature and pressure are...
The use of oxygen for aerospace applications is bonded to the history of American rocketry. The firs...
Thermophysical properties data for oxygen at pressures below 5000 psia have been extrapolated to hig...
Particle impact and frictional heating tests of metals in high pressure oxygen, are conducted in sup...
Advances in the design of the liquid oxygen, liquid hydrogen engines for the Space Transportation Sy...
The requirements for impact testing of materials in an oxygen atmosphere at pressures from 82.7 MPa ...
Although NASA is not one of the country's major oxygen consumers, it uses oxygen under severe condit...
A repository for critical and important detailed design data and information, hitherto unpublished, ...
The sensitivity of materials in contact with gaseous oxygen (GOX) or liquid oxygen (LOX) was examine...
The use of oxygen for aerospace applications is bonded to the history of American rocketry. The firs...
Brief discussions of the materials and configurations testing techniques and requirements for the Ap...
As a result of the Apollo 13 incident, increased emphasis is being placed on materials compatibility...
SIGLEAvailable from British Library Document Supply Centre- DSC:DX178271 / BLDSC - British Library D...
Thermodynamic and related properties of oxygen from experimental pressure-volume-temperature measure...
Materials used in oxygen systems and allowable oxygen environments are specified for each material. ...
Precision measurements of the properties of oxygen over a wide range of temperature and pressure are...
The use of oxygen for aerospace applications is bonded to the history of American rocketry. The firs...
Thermophysical properties data for oxygen at pressures below 5000 psia have been extrapolated to hig...
Particle impact and frictional heating tests of metals in high pressure oxygen, are conducted in sup...
Advances in the design of the liquid oxygen, liquid hydrogen engines for the Space Transportation Sy...
The requirements for impact testing of materials in an oxygen atmosphere at pressures from 82.7 MPa ...