A series of test activities has raised some concerns about the generation of orbital debris caused by failures of composite overwrapped pressure vessels (COPVs). These tests have indicated that a large number of composite fragments can be produced by either pressure burst failures or by high-speed impacts. A review of prior high-speed tests with COPV indicates that other tests have produced large numbers of composite fragments. As was the case with the test referenced here, the tests tended to produce a large number of small composite fragments with relatively low velocities induced by the impact and or gas expansion
One of the major concerns for the aging Space Shuttle fleet is the stress rupture life of composite ...
Most spacecraft have at least one pressurized vessel on board. Because of the serious damage that mi...
Investigation of composite materials response to hypervelocity impact by space debris has been carri...
There is a limited amount of hypervelocity impact (HVI) data on pressurized composite overwrapped pr...
Most spacecraft have at least one pressurized vessel on board. Because of the serious damage that mi...
Most spacecraft have at least one pressurized vessel on board. Because of the potential of serious m...
This paper reports stress rupture testing of Kevlar(TradeMark) composite overwrapped pressure vessel...
A theoretical investigation of the factors controlling the stress rupture life of the National Aeron...
The DebriSat hypervelocity impact experiment, performed at the Arnold Engineering Development Center...
Carbon fibers released from composites by aircraft fires and crashes can cause electrical shorts and...
A primary spacecraft design consideration is the anticipation and mitigation of the possible damage ...
A main design consideration for spacecraft destined to operate in the meteoroid or orbital debris (M...
How well a spacecraft component resists the damage that might occur following a high-speed impact by...
Composite Overwrapped Pressure Vessels (COPV) store gases used in four subsystems for NASA's Space S...
This slide presentation reviews the use of Modal Acoustic Emission to monitor damage progression to ...
One of the major concerns for the aging Space Shuttle fleet is the stress rupture life of composite ...
Most spacecraft have at least one pressurized vessel on board. Because of the serious damage that mi...
Investigation of composite materials response to hypervelocity impact by space debris has been carri...
There is a limited amount of hypervelocity impact (HVI) data on pressurized composite overwrapped pr...
Most spacecraft have at least one pressurized vessel on board. Because of the serious damage that mi...
Most spacecraft have at least one pressurized vessel on board. Because of the potential of serious m...
This paper reports stress rupture testing of Kevlar(TradeMark) composite overwrapped pressure vessel...
A theoretical investigation of the factors controlling the stress rupture life of the National Aeron...
The DebriSat hypervelocity impact experiment, performed at the Arnold Engineering Development Center...
Carbon fibers released from composites by aircraft fires and crashes can cause electrical shorts and...
A primary spacecraft design consideration is the anticipation and mitigation of the possible damage ...
A main design consideration for spacecraft destined to operate in the meteoroid or orbital debris (M...
How well a spacecraft component resists the damage that might occur following a high-speed impact by...
Composite Overwrapped Pressure Vessels (COPV) store gases used in four subsystems for NASA's Space S...
This slide presentation reviews the use of Modal Acoustic Emission to monitor damage progression to ...
One of the major concerns for the aging Space Shuttle fleet is the stress rupture life of composite ...
Most spacecraft have at least one pressurized vessel on board. Because of the serious damage that mi...
Investigation of composite materials response to hypervelocity impact by space debris has been carri...