Vulnerability of high pressure vessels subjected to high velocity impact of space debris is analyzed with the response of pressurized vessels to hypervelocity impact of aluminum sphere. Investigated tanks are CFRP (carbon fiber reinforced plastics) overwrapped Al vessels. Explored internal pressure of nitrogen ranges from 1 bar to 300 bar and impact velocity are around 4400 m/s. Data obtained from Xrays radiographies and particle velocity measurements show the evolution of debris cloud and shock wave propagation in pressurized nitrogen. Observation of recovered vessels leads to the damage pattern and to its evolution as a function of the internal pressure. It is shown that the rupture mode is not a bursting mode but rather a catastrophic da...
Hypervelocity impact experiments were performed on two types of cylindrical pressure vessels made fr...
A primary spacecraft design consideration is the anticipation and mitigation of the possible damage ...
There is a limited amount of hypervelocity impact (HVI) data on pressurized composite overwrapped pr...
Vulnerability of high pressure vessels subjected to high velocity impact of space debris is analyzed...
Vulnerability of high pressure vessels subjected to high velocity impact of space debris is analyzed...
AbstractVulnerability of high pressure vessels subjected to high velocity impact of space debris is ...
AbstractResponse of pressurized composite-Al vessels to hypervelocity impact of aluminum spheres hav...
Response of pressurized composite-Al vessels to hypervelocity impact of aluminum spheres have been n...
AbstractResponse of pressurized composite-Al vessels to hypervelocity impact of aluminum spheres hav...
Most spacecraft have at least one pressurized vessel on board. Because of the potential of serious m...
Thin-walled cylindrical gas-filled pressure vessels made of aluminium alloy and unalloyed titanium w...
Most spacecraft have at least one pressurized vessel on board. Because of the serious damage that mi...
A primary spacecraft design consideration is the anticipation and mitigation of the possible damage ...
A primary spacecraft design consideration is the anticipation and mitigation of the possible damage ...
Most spacecraft have a pressurized tank on board, such as a liquid propellant tank or a breathable a...
Hypervelocity impact experiments were performed on two types of cylindrical pressure vessels made fr...
A primary spacecraft design consideration is the anticipation and mitigation of the possible damage ...
There is a limited amount of hypervelocity impact (HVI) data on pressurized composite overwrapped pr...
Vulnerability of high pressure vessels subjected to high velocity impact of space debris is analyzed...
Vulnerability of high pressure vessels subjected to high velocity impact of space debris is analyzed...
AbstractVulnerability of high pressure vessels subjected to high velocity impact of space debris is ...
AbstractResponse of pressurized composite-Al vessels to hypervelocity impact of aluminum spheres hav...
Response of pressurized composite-Al vessels to hypervelocity impact of aluminum spheres have been n...
AbstractResponse of pressurized composite-Al vessels to hypervelocity impact of aluminum spheres hav...
Most spacecraft have at least one pressurized vessel on board. Because of the potential of serious m...
Thin-walled cylindrical gas-filled pressure vessels made of aluminium alloy and unalloyed titanium w...
Most spacecraft have at least one pressurized vessel on board. Because of the serious damage that mi...
A primary spacecraft design consideration is the anticipation and mitigation of the possible damage ...
A primary spacecraft design consideration is the anticipation and mitigation of the possible damage ...
Most spacecraft have a pressurized tank on board, such as a liquid propellant tank or a breathable a...
Hypervelocity impact experiments were performed on two types of cylindrical pressure vessels made fr...
A primary spacecraft design consideration is the anticipation and mitigation of the possible damage ...
There is a limited amount of hypervelocity impact (HVI) data on pressurized composite overwrapped pr...