MILSTAR's Flexible Substrate Solar Array (FSSA) is an evolutionary development of the lightweight, flexible substrate design pioneered at Lockheed during the seventies. Many of the features of the design are related to the Solar Array Flight Experiment (SAFE), flown on STS-41D in 1984. FSSA development has created a substantial technology base for future flexible substrate solar arrays such as the array for the Space Station Freedom. Lessons learned during the development of the FSSA can and should be applied to the Freedom array and other future flexible substrate designs
A tension mechanism is used to apply a tension force to the Space Station Freedom Solar Array Blanke...
The Advanced Photovoltaic Solar Array (APSA) program seeks to bring to flight readiness a solar arra...
The Space Platform Solar Array represents a significant step forward in lightweight photovoltaic arr...
The Space Station Freedom Solar Array Program is required to provide a 75 kW power module that uses ...
A solar array (SA) mechanical subsystem made of thin and lightweight substrates was developed, built...
Flexible, deployable arrays are an attractive alternative to conventional solar arrays for near-term...
The latest thinking about how the Flat-Plate Solar Array Project (FSA), will redirect activities awa...
The SMall EXplorer (SMEX) Fast Auroral SnapshoT (FAST) Spacecraft (S/C) was developed to investigate...
Space Station Freedom will feature six large solar arrays, called solar array wings, built by Lockhe...
The majority of existing large solar arrays are designed against the requirements imposed by communc...
Solar arrays are the main power source in space. Conventionally they are composed of stiff backing s...
The Solar Array Flight Experiment (SAFE) developed under the direction of the Marshall Space Flight ...
Recent advances in Shape Memory Alloy (SMA), Elastic Memory Composites (EMC), and ultra- light compo...
During the past decade, a number of advances have occurred in solar cell and array technology. These...
A sample module was assembled to model a portion of a flexible extendable solar array, a type that p...
A tension mechanism is used to apply a tension force to the Space Station Freedom Solar Array Blanke...
The Advanced Photovoltaic Solar Array (APSA) program seeks to bring to flight readiness a solar arra...
The Space Platform Solar Array represents a significant step forward in lightweight photovoltaic arr...
The Space Station Freedom Solar Array Program is required to provide a 75 kW power module that uses ...
A solar array (SA) mechanical subsystem made of thin and lightweight substrates was developed, built...
Flexible, deployable arrays are an attractive alternative to conventional solar arrays for near-term...
The latest thinking about how the Flat-Plate Solar Array Project (FSA), will redirect activities awa...
The SMall EXplorer (SMEX) Fast Auroral SnapshoT (FAST) Spacecraft (S/C) was developed to investigate...
Space Station Freedom will feature six large solar arrays, called solar array wings, built by Lockhe...
The majority of existing large solar arrays are designed against the requirements imposed by communc...
Solar arrays are the main power source in space. Conventionally they are composed of stiff backing s...
The Solar Array Flight Experiment (SAFE) developed under the direction of the Marshall Space Flight ...
Recent advances in Shape Memory Alloy (SMA), Elastic Memory Composites (EMC), and ultra- light compo...
During the past decade, a number of advances have occurred in solar cell and array technology. These...
A sample module was assembled to model a portion of a flexible extendable solar array, a type that p...
A tension mechanism is used to apply a tension force to the Space Station Freedom Solar Array Blanke...
The Advanced Photovoltaic Solar Array (APSA) program seeks to bring to flight readiness a solar arra...
The Space Platform Solar Array represents a significant step forward in lightweight photovoltaic arr...