The invention discloses a method for fabricating a deployable, inflatable aerodynamic control structure for aerospace vehicles which has a desired noncircular or noncylindrical cross-section. In a preferred embodiment, the control structure is configured as an inflatable airfoil and includes a...http://www.google.fr/patents/US5725709?utm_source=gb-gplus-shareBrevet US5725709 - Fabrication method for an inflatable deployable control structure for aerospace vehicles
Fabrication method for an inflatable deployable control structure for ...
