Particle impact tests were performed on three types of orbiter surface with a micrometeoroid facility. The test equipment electrostatically accelerated micron sized particles to high velocities simulating micrometeoroid impacts. Test particles were titanium diboride with typical velocities in the range 1 to 2.3 km x sec/1 and equivalent particle diameters in the range 4 to 16 microns. Impact angles to the material surface were 90, 60 and 30 degrees. The particle impact sites were located on the sample surfaces and craters were photographed with a magnification of 400X
A new facility for making small particle impacts is being developed at NASA. Current sand/particle i...
The radiator shield on the Wide Field and Planetary Camera 2 (WFPC2) was subject to optical inspecti...
Postflight surveys of the Wide Field and Planetary Camera 2 (WFPC2) on the Hubble Space Telescope ha...
This paper discusses the results of an attempt to use laboratory test data and empirically derived m...
This presentation will discuss the results of an attempt to use laboratory test data and empirically...
Dust-sized olivine particles were fired at a copper plate using the Space Power Institute hyperveloc...
The long-term effects of the orbital debris and micrometeoroid environments on materials that are cu...
Knowing the impact effects of the space environment on engineering materials is critical if we are t...
The Solar Maximum Satellite developed electronic problems after operating successfully in space for ...
The Ion Beam textured and coated surfaces EXperiment (IBEX), designated S1003, was flown on LDEF at ...
Electrostatically accelerated microparticles are used to perform simulated micrometeoroid impact cra...
The Utah State University SUSpECS project was a unique student experiment that allowed for pre- and ...
The Wide Field and Planetary Camera 2 (WFPC2) was returned from the Hubble Space Telescope (HST) by ...
The Utah State University SUSpECS project was a unique student experiment that allowed for pre- and ...
A method was developed to simulate space debris in the laboratory. This method, which is an outgrowt...
A new facility for making small particle impacts is being developed at NASA. Current sand/particle i...
The radiator shield on the Wide Field and Planetary Camera 2 (WFPC2) was subject to optical inspecti...
Postflight surveys of the Wide Field and Planetary Camera 2 (WFPC2) on the Hubble Space Telescope ha...
This paper discusses the results of an attempt to use laboratory test data and empirically derived m...
This presentation will discuss the results of an attempt to use laboratory test data and empirically...
Dust-sized olivine particles were fired at a copper plate using the Space Power Institute hyperveloc...
The long-term effects of the orbital debris and micrometeoroid environments on materials that are cu...
Knowing the impact effects of the space environment on engineering materials is critical if we are t...
The Solar Maximum Satellite developed electronic problems after operating successfully in space for ...
The Ion Beam textured and coated surfaces EXperiment (IBEX), designated S1003, was flown on LDEF at ...
Electrostatically accelerated microparticles are used to perform simulated micrometeoroid impact cra...
The Utah State University SUSpECS project was a unique student experiment that allowed for pre- and ...
The Wide Field and Planetary Camera 2 (WFPC2) was returned from the Hubble Space Telescope (HST) by ...
The Utah State University SUSpECS project was a unique student experiment that allowed for pre- and ...
A method was developed to simulate space debris in the laboratory. This method, which is an outgrowt...
A new facility for making small particle impacts is being developed at NASA. Current sand/particle i...
The radiator shield on the Wide Field and Planetary Camera 2 (WFPC2) was subject to optical inspecti...
Postflight surveys of the Wide Field and Planetary Camera 2 (WFPC2) on the Hubble Space Telescope ha...