|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/15 ; 89/15 ; R ; 244/45A ; 244/100A|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 5 인용 특허 : 2|
A recoverable remotely piloted vehicle (RPV) having: a deflectable canard/elevator placed very close to the nose tip; a constant (cross) section fuselage; wings mounted low and well aft on the fuselage; elevons; a centrally positioned weapons/payload bay, with doors, located internal of the upper portion of the fuselage; and, inflatable landing skids. The weapon/payload is dropped from the RVP, while the RVP is in flight in an inverted position.
A remotely piloted vehicle, having a center of gravity and a longitudinal axis, comprising: a. a fuselage having a longitudinal axis coincident with said longitudinal axis of said remotely piloted vehicle, a port side, a starboard side, an upper portion, a lower portion, a fore section with a nose, and an aft section, with said fuselage also having a transverse cross section that is essentially constant in shape; b. a canard comprising a first section and a symmetrical second section, with each said canard section located essentially at, and connected to...