Large space-based deployable antenna structures are needed for a varie
ty of applications. However, recent reductions of antenna user resourc
es have resulted in a real need for low-cost, large-size, lightweight,
and reliable deployable space antenna structures. Fortunately, a new c
lass of deployable space structures, called ''inflatable space structu
res is under development at L'Garde, Inc. The potential of this new co
ncept was recognized by NASA who selected it for a flight experiment.
The objective of the experiment was to develop a large, low-cost infla
table antenna structure and demonstrate its mechanical performance in
the space environment. The carrier for this free-flying experiment was
the STS-launched and recovered Spartan spacecraft. The experiment har
dware consisted of a 14-meter diameter off-set parabolic reflector str
ucture. The Spartan 207/IAE was successfully flown on STS 77, deployed
on May 20, 1996 with Spartan recovery on May 21, 1996. The basic ante
nna structure deployed successfully, but in an uncontrolled manner, th
at clearly demonstrated the robustness of this new type of space struc
ture. The low cost of the flight antenna structure hardware and the ou
tstanding mechanical packaging demonstrated on orbit clearly validated
the potential of this new class of space structure for enabling new,
low-cost missions. (C) 1998 International Astronautical Federation. Pu
blished by Elsevier Science Ltd.