Add to ORKGA new concept for deployable mesh reflectors is pre-sented. It consists of a deployable ring structure and two identical cable nets (front and rear nets) connected by ten-sion ties. The reflecting mesh is attached to the front net. The concept has been demonstrated by means of simple demonstrator hardware. A preliminary design of a 3 m diameter, 10 GHz reflector with a focal length to diam-eter ratio F/D = 0.4 that could be packaged within an envelope of 0.1 × 0.2 × 0.8 m3 is presented
Future space missions require high precision large space borne antenna reflectors working up to Ku b...
This paper describes a number of large deployable antenna (LDA) reflector structure concepts develop...
Future space missions such as the Earth Science Geostationary Platform (ESGP) will require highly ac...
Future small satellite missions require low-cost, precision reflector structures with large aperture...
A key limitation for future Small Satellite communications and radar missions will be available ante...
Future small satellite missions require low-cost, precision reflector structures with large aperture...
With vast changes in spacecraft developments over its short history, a new and cheaper method was ne...
This paper presents a new deployable reflector concept for an Earth observation mis-sion that requir...
Creation of large size, lightweight, rigid and precision reflectors is the problem that still remain...
The first phase in the development of a solid surface, deployable, antenna reflector is outlined and...
The transformation of doubly curved surfaces, without affecting their geometric integrity, into quas...
This report presents a new deployable structure concept for a low altitude L or P-Band Synthetic Ape...
The advent of VLSI and microelectronics has made it possible to reduce the size of electronic device...
The application of large antennas in spacecraft is often limited by available volume, as well as by ...
Nowadays space missions such as Earth observation, telecommunication and science require large anten...
Future space missions require high precision large space borne antenna reflectors working up to Ku b...
This paper describes a number of large deployable antenna (LDA) reflector structure concepts develop...
Future space missions such as the Earth Science Geostationary Platform (ESGP) will require highly ac...
Future small satellite missions require low-cost, precision reflector structures with large aperture...
A key limitation for future Small Satellite communications and radar missions will be available ante...
Future small satellite missions require low-cost, precision reflector structures with large aperture...
With vast changes in spacecraft developments over its short history, a new and cheaper method was ne...
This paper presents a new deployable reflector concept for an Earth observation mis-sion that requir...
Creation of large size, lightweight, rigid and precision reflectors is the problem that still remain...
The first phase in the development of a solid surface, deployable, antenna reflector is outlined and...
The transformation of doubly curved surfaces, without affecting their geometric integrity, into quas...
This report presents a new deployable structure concept for a low altitude L or P-Band Synthetic Ape...
The advent of VLSI and microelectronics has made it possible to reduce the size of electronic device...
The application of large antennas in spacecraft is often limited by available volume, as well as by ...
Nowadays space missions such as Earth observation, telecommunication and science require large anten...
Future space missions require high precision large space borne antenna reflectors working up to Ku b...
This paper describes a number of large deployable antenna (LDA) reflector structure concepts develop...
Future space missions such as the Earth Science Geostationary Platform (ESGP) will require highly ac...