Long-life (10-30 years) large space structures are considered by NASA for a number of future earth-orbiting missions. The use of very thin graphite-fiber composites have been considered as structural materials for the fabrication of these structures. A combination of analytical and experimental approaches will be needed to provide a reliable data base on engineering properties of these materials to be used in the design and fabrication of these structures, which will be able to withstand the space environment
The effects of simulated space environmental parameters on microdamage induced by the environment in...
Repair techniques for graphite/epoxy and graphite/polyimide composite structures are discussed. Tens...
A monograph is presented which establishes structural design criteria and recommends practices to en...
Long-life (10-30 years) large space structures are considered by NASA for a number of future earth-o...
Long-life (10-30 years) large space structures are considered by NASA for a number of future earth-o...
Nonmetallic composites such as the graphite/epoxy system were investigated as possible substrates fo...
The need for safe, lightweight, less expensive, and more reliable launch vehicle components is being...
The use of composite materials continues to increase in the aerospace community due to the potential...
Graphite/epoxy composite materials are being used increasingly for numerous space applications. Engi...
Filamentary composite materials reviewed for potential applications in spacecraft structure
In this paper, the aircraft and space vehicle requirements for composite structures are compared. It...
Abstract:- New technology emerged in super composite material such as Kevlar ® that supported experi...
Commercially available composite structural shapes were evaluated for use. These composites, fibergl...
Technology utilization of fiber reinforced composite materials is discussed in the areas of physical...
Over 200 graphite/aluminum and graphite/magnesium composites were flown on the leading and trailing ...
The effects of simulated space environmental parameters on microdamage induced by the environment in...
Repair techniques for graphite/epoxy and graphite/polyimide composite structures are discussed. Tens...
A monograph is presented which establishes structural design criteria and recommends practices to en...
Long-life (10-30 years) large space structures are considered by NASA for a number of future earth-o...
Long-life (10-30 years) large space structures are considered by NASA for a number of future earth-o...
Nonmetallic composites such as the graphite/epoxy system were investigated as possible substrates fo...
The need for safe, lightweight, less expensive, and more reliable launch vehicle components is being...
The use of composite materials continues to increase in the aerospace community due to the potential...
Graphite/epoxy composite materials are being used increasingly for numerous space applications. Engi...
Filamentary composite materials reviewed for potential applications in spacecraft structure
In this paper, the aircraft and space vehicle requirements for composite structures are compared. It...
Abstract:- New technology emerged in super composite material such as Kevlar ® that supported experi...
Commercially available composite structural shapes were evaluated for use. These composites, fibergl...
Technology utilization of fiber reinforced composite materials is discussed in the areas of physical...
Over 200 graphite/aluminum and graphite/magnesium composites were flown on the leading and trailing ...
The effects of simulated space environmental parameters on microdamage induced by the environment in...
Repair techniques for graphite/epoxy and graphite/polyimide composite structures are discussed. Tens...
A monograph is presented which establishes structural design criteria and recommends practices to en...