Add to ORKGThe conceptual design, performance projections, and materials development for the maypole (hoop/column) reflector concept are summarized. Factors influencing configuration choices are discussed along with quad aperture/feed characteristics and antenna requirements based on missions
A type of antenna reflector was studied in which a stiff structure is constructed to hold a membrane...
Future space missions such as the Earth Science Geostationary Platform (ESGP) will require highly ac...
The program was initiated to investigate the availability of critical large deployable antenna techn...
The design and application of the offset wrap rib and the maypole (hoop/column) antenna configuratio...
The first phase in the development of a solid surface, deployable, antenna reflector is outlined and...
Several analytical studies of topics relevant to the design of large space structures are presented....
With vast changes in spacecraft developments over its short history, a new and cheaper method was ne...
This paper describes a number of large deployable antenna (LDA) reflector structure concepts develop...
The development of large furlable spacecraft antennas using conical main reflectors is described. Tw...
The design, development, and implementation status of the Surface Control Actuator System (SCAS) for...
A 15-meter diameter deployable antenna has been built and is being used as an experimental test syst...
The 5-meter technology antenna program demonstrated the overall feasibility of integrating a mesh re...
Preliminary assessments by both government and industry indicate that applications exist in the area...
The 15-meter hoop-column antenna fabricated by the Harris Corporation under contract to the NASA Lan...
There is a need for completely deployable large antenna reflectors capable of efficiently handling m...
A type of antenna reflector was studied in which a stiff structure is constructed to hold a membrane...
Future space missions such as the Earth Science Geostationary Platform (ESGP) will require highly ac...
The program was initiated to investigate the availability of critical large deployable antenna techn...
The design and application of the offset wrap rib and the maypole (hoop/column) antenna configuratio...
The first phase in the development of a solid surface, deployable, antenna reflector is outlined and...
Several analytical studies of topics relevant to the design of large space structures are presented....
With vast changes in spacecraft developments over its short history, a new and cheaper method was ne...
This paper describes a number of large deployable antenna (LDA) reflector structure concepts develop...
The development of large furlable spacecraft antennas using conical main reflectors is described. Tw...
The design, development, and implementation status of the Surface Control Actuator System (SCAS) for...
A 15-meter diameter deployable antenna has been built and is being used as an experimental test syst...
The 5-meter technology antenna program demonstrated the overall feasibility of integrating a mesh re...
Preliminary assessments by both government and industry indicate that applications exist in the area...
The 15-meter hoop-column antenna fabricated by the Harris Corporation under contract to the NASA Lan...
There is a need for completely deployable large antenna reflectors capable of efficiently handling m...
A type of antenna reflector was studied in which a stiff structure is constructed to hold a membrane...
Future space missions such as the Earth Science Geostationary Platform (ESGP) will require highly ac...
The program was initiated to investigate the availability of critical large deployable antenna techn...