Folding wing structure with a flexible cover

摘要: A folding wing structure for improved missile aerodynamic performance and manuverability with a minimum payload space requirement which comprises leading edge spar at least one trailing spaced apart from each other by plurality of transverse ribs, the spars being approximately parallel to ribs positioned along divide into series parallelograms. The are pivotally joined together further an air frame vehicle or missile. In folded position rib collapse occupy minimal amount volume in recessed area frame. spring piston member secured one, forces out fuselage erected predetermined sweep angles relative fuselage.