Re. Freeland et al., DEVELOPMENT OF FLIGHT HARDWARE FOR A LARGE, INFLATABLE-DEPLOYABLE ANTENNA EXPERIMENT, Acta astronautica, 38(4-8), 1996, pp. 251-260
Large, space-based antennas are needed for a variety of different appl
ications. Since there is no meaningful orbital assembly capability pla
nned at this time, any large space structures will have to be self-dep
loyable. Current concepts for large, conventional, mechanical, self-de
ployable space structures tend to be very expensive and mechanically c
omplicated. Current antenna-user requirements are so stringent (with r
espect to the need for very low-cost, high-deployment reliability, low
weight, and packaged-volume and usable aperture precision) that new a
nd innovative approaches to accommodate large space structures are nee
ded. Fortunately, a newly developed class of space structures, called
inflatable-deployable structures, has great potential for satisfying t
hese stringent user requirements. A concept under development at L'Gar
de, Inc., for a large, inflatable-deployable antenna represents an exc
ellent example of this new type of structure.