|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/002 ; 244/158R ; 244/160 ; 244/172|
|발명자 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 42 인용 특허 : 12|
The reusable space launch system has a first stage vehicle or aerospacecraft, a second stage vehicle or reusable spacecraft and a third stage vehicle or reusable orbit transfercraft. All the stages have the basic aerodynamic vehicle elements of a fuselage, wings, and tail, with the incorporation of control surfaces to supply lift, stability and control. The aerospacecraft is configured to use ejector ramjet engines for powered flight and includes equipment to capture air to supplement oxidizer for the ejector ramjet engine during take-off and extreme hig...
[We claim:] [1.]a) a fuselage, a pair of wings with a plurality of control surface and a tail with a rudder;b) the fuselage comprising:i) a conic curve shape for an upper fuselage from a nose end to a tail end;ii) a straight line conic shape for a lower fuselage from the nose end to an engine nacelle; the engine nacelle aft of a plurality of inlets having a constant semicircular cross section to a plurality of engine exhaust nozzles; and a lower aft fuselage having a decreasing concave conic shape to the tail end;iii) a maximum cross section dimension of...