MMA Design (MMA) has invented and is developing a revolutionary deployable antenna solution providing extremely high areal compaction for future microsatellite missions. Our solution combines the positive attributes of currently fielded antenna systems and will enable performance for microsatellites consistent with today’s large space craft payloads. The MMA patented and patent pending Deployable High Gain Reflectarray (DaHGR) antenna has both a wideband and a narrower band configuration. The antenna architecture is realized using very lightweight flexible membrane substrates incorporating a hoop structure to deploy the membranes and maintain tension. The proposed solution builds on innovations by MMA in extremely lightweight deployable sys...
The advent of VLSI and microelectronics has made it possible to reduce the size of electronic device...
The 5-meter technology antenna program demonstrated the overall feasibility of integrating a mesh re...
In this paper, an extended version of Zolesi et al. (Proceedings of the 42nd ICES (AIAA 2012-3601), ...
Increasing interest from the scientific community to utilize space-borne L- or P-Band radar antennas...
Preliminary assessments by both government and industry indicate that applications exist in the area...
Space data services provide the largest market value to the global space industry. With the increasi...
Space data services provide the largest market value to the global space industry. With the increasi...
With vast changes in spacecraft developments over its short history, a new and cheaper method was ne...
Large, space-based antennas are needed for a variety of different applications.Since there is no mea...
As the current discussions on climate changes suggest, the need for understanding the occurrences on...
Small satellites in general and cubesats in particular have been limited in their ability to perform...
The application of large antennas in spacecraft is often limited by available volume, as well as by ...
Future space missions such as the Earth Science Geostationary Platform (ESGP) will require highly ac...
A deployment strategy for a 4 m long, ultra-light, high-gain, helical Antenna made from fiber-compos...
The advent of VLSI and microelectronics has made it possible to reduce the size of electronic device...
The advent of VLSI and microelectronics has made it possible to reduce the size of electronic device...
The 5-meter technology antenna program demonstrated the overall feasibility of integrating a mesh re...
In this paper, an extended version of Zolesi et al. (Proceedings of the 42nd ICES (AIAA 2012-3601), ...
Increasing interest from the scientific community to utilize space-borne L- or P-Band radar antennas...
Preliminary assessments by both government and industry indicate that applications exist in the area...
Space data services provide the largest market value to the global space industry. With the increasi...
Space data services provide the largest market value to the global space industry. With the increasi...
With vast changes in spacecraft developments over its short history, a new and cheaper method was ne...
Large, space-based antennas are needed for a variety of different applications.Since there is no mea...
As the current discussions on climate changes suggest, the need for understanding the occurrences on...
Small satellites in general and cubesats in particular have been limited in their ability to perform...
The application of large antennas in spacecraft is often limited by available volume, as well as by ...
Future space missions such as the Earth Science Geostationary Platform (ESGP) will require highly ac...
A deployment strategy for a 4 m long, ultra-light, high-gain, helical Antenna made from fiber-compos...
The advent of VLSI and microelectronics has made it possible to reduce the size of electronic device...
The advent of VLSI and microelectronics has made it possible to reduce the size of electronic device...
The 5-meter technology antenna program demonstrated the overall feasibility of integrating a mesh re...
In this paper, an extended version of Zolesi et al. (Proceedings of the 42nd ICES (AIAA 2012-3601), ...