Low-velocity impacts were inflicted upon two elbow sections of carbon/epoxy feedline that are to be a part of the Delta Clipper-XA flight vehicle. A soap-based liquid leak detector solution was used to inspect the impact sites for leaks of pressurized gas that was pumped into the tube. Visual surface damage was noted and recorded for each impact site. After impact testing of each of the two sections of tubes was completed, the damage zones were disected from the tube and cross sectioned through the impact site. These specimens were polished after potting them in epoxy and were examined for microcracking using a fluorescent dye penetrant technique. The results showed that nonvisible damage could cause microcracking, thereby resulting in leak...
A compilation of papers presented at this conference is given. The science dealing with materials an...
Contaminant generation studies were conducted at the component level using two different methods, ra...
Recent work has been done with the goal of establishing ultralow emission aircraft gas turbine combu...
Instrumented drop weight impact testing was utilized to examine a puncture-type impact on thin carbo...
Low velocity instrumented impact testing was utilized to examine the effects of an outer lamina of u...
The protection scheme developed for long duration space platforms relies primarily upon placing thin...
Four fiber/resin systems were compared for resistance to damage and damage tolerance. One toughened ...
A debris/ice/thermal protection system assessment and integrated photographic analysis was conducted...
The design and development of an airborne flight-test experiment to study nonreacting gas jets injec...
The issue of the effects of the space environment on spacecraft needs to be understood for the long ...
The goal of this research was to utilize statistical methods to evaluate the probability of detectio...
The Small Expendable Deployer System (SEDS) was designed to deploy an endmass at the end of a 20-km-...
Fuel irradiation experiments were designed, built, and operated to test uranium mononitride (UN) fue...
Continuing on the successful progress of NIAC (NASA Innovative Advanced Concepts) Phase I, this repo...
The lunar surface is covered by a thick blanket of fine dust. This dust may be readily suspended fro...
A compilation of papers presented at this conference is given. The science dealing with materials an...
Contaminant generation studies were conducted at the component level using two different methods, ra...
Recent work has been done with the goal of establishing ultralow emission aircraft gas turbine combu...
Instrumented drop weight impact testing was utilized to examine a puncture-type impact on thin carbo...
Low velocity instrumented impact testing was utilized to examine the effects of an outer lamina of u...
The protection scheme developed for long duration space platforms relies primarily upon placing thin...
Four fiber/resin systems were compared for resistance to damage and damage tolerance. One toughened ...
A debris/ice/thermal protection system assessment and integrated photographic analysis was conducted...
The design and development of an airborne flight-test experiment to study nonreacting gas jets injec...
The issue of the effects of the space environment on spacecraft needs to be understood for the long ...
The goal of this research was to utilize statistical methods to evaluate the probability of detectio...
The Small Expendable Deployer System (SEDS) was designed to deploy an endmass at the end of a 20-km-...
Fuel irradiation experiments were designed, built, and operated to test uranium mononitride (UN) fue...
Continuing on the successful progress of NIAC (NASA Innovative Advanced Concepts) Phase I, this repo...
The lunar surface is covered by a thick blanket of fine dust. This dust may be readily suspended fro...
A compilation of papers presented at this conference is given. The science dealing with materials an...
Contaminant generation studies were conducted at the component level using two different methods, ra...
Recent work has been done with the goal of establishing ultralow emission aircraft gas turbine combu...