|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/117A ; 244/158A ; 244/123|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 6 인용 특허 : 2|
A primary load bearing structure particularly adapted for hypersonic aerospace vehicles utilizing a cryogenic liquid fuel, and comprised of a plurality of rigid load bearing, fluid passageways or tubes connected together in the form of a panel structure. Such panel structure and the passageways or the tubes thereof form the outside surface of the aerospace vehicle and are also positioned adjacent to or integral with a wall of the cryogenic liquid fuel tank. During flight, cryogenic liquid fuel is passed through the tubes to provide cooling for the extern...
An aerospace vehicle comprising, a fuel tank containing a cryogenic liquid fuel, an external surface forming the skin of said vehicle, a primary load bearing structure disposed between said fuel tank and the external surface of said vehicle, said load bearing structure consisting of a panel structure formed of a plurality of rigid metal tubes of substantially cylindrical shape connected together in side-by-side relation at the contacting peripheral surfaces of adjacent tubes, said tubes extending lengthwise in said panel structure, the axis of each of sa...