Add to ORKGVisual inspection revealed contamination on the surface of tiles removed from the lower section of the space shuttle orbiter after the second flight of Columbia (STS-2). Possible sources of this contamination and the effect on surface catalycity are presented
Atom recombination catalytic rates for surface coatings of various candidate thermal protection syst...
This paper describes the design and results of a surface catalysis flight experiment flown on the Or...
When LDEF entered orbit its cleanliness was approximately a MIL-STD-1246B Level 2000C. Its burden of...
During that portion of Space Shuttle orbiter entry when significant aerodynamic heat transfer occurs...
Interactions of atoms with space shuttle surface and methods for improving heat transfe
The purpose of this project was to determine the chemicals desorbing from the space shuttle heat pro...
A purge and trap technique which was employed to collect and separate the chemicals desorbing from t...
The physical and chemical processes at solid surfaces which can contribute to Space Station contamin...
Coated specimens of reusable surface insulation (RSI) were exposed to alternate radiant heating and ...
Substrates to be contaminated and contamination source were prepared. Additional information on pain...
The control of surface contamination in the manufacture of space hardware can become a critical step...
Flight experiments flown on the Space Shuttle, the International Space Station, Mir, Skylab, and fre...
Effects of mercury electron bombardment ion thruster exhaust products on surfaces located downstrea
Surfaces of materials used in the space shuttle orbiter payload bay and exposed during STS-1 through...
The Space Transportation System (STS) orbiters are known to be significant sources of outgassing in ...
Atom recombination catalytic rates for surface coatings of various candidate thermal protection syst...
This paper describes the design and results of a surface catalysis flight experiment flown on the Or...
When LDEF entered orbit its cleanliness was approximately a MIL-STD-1246B Level 2000C. Its burden of...
During that portion of Space Shuttle orbiter entry when significant aerodynamic heat transfer occurs...
Interactions of atoms with space shuttle surface and methods for improving heat transfe
The purpose of this project was to determine the chemicals desorbing from the space shuttle heat pro...
A purge and trap technique which was employed to collect and separate the chemicals desorbing from t...
The physical and chemical processes at solid surfaces which can contribute to Space Station contamin...
Coated specimens of reusable surface insulation (RSI) were exposed to alternate radiant heating and ...
Substrates to be contaminated and contamination source were prepared. Additional information on pain...
The control of surface contamination in the manufacture of space hardware can become a critical step...
Flight experiments flown on the Space Shuttle, the International Space Station, Mir, Skylab, and fre...
Effects of mercury electron bombardment ion thruster exhaust products on surfaces located downstrea
Surfaces of materials used in the space shuttle orbiter payload bay and exposed during STS-1 through...
The Space Transportation System (STS) orbiters are known to be significant sources of outgassing in ...
Atom recombination catalytic rates for surface coatings of various candidate thermal protection syst...
This paper describes the design and results of a surface catalysis flight experiment flown on the Or...
When LDEF entered orbit its cleanliness was approximately a MIL-STD-1246B Level 2000C. Its burden of...