|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||B64G-001/40 B64G-001/26 F42B-010/66 F02K-009/34|
|미국특허분류(USC)||060/253; 060/255; 060/256; 244/003.21; 244/003.22|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 2 인용 특허 : 57|
Embodiments of a flight vehicle are provided, as are embodiments of a method for manufacturing a flight vehicle. In one embodiment, the flight vehicle includes a solid-propellant rocket motor, control circuitry, and an electrically-interconnective support structure. The electrically-interconnective support structure includes a load-bearing frame and a plurality of electrical conductors embedded within the load-bearing frame. The solid-propellant rocket motor is mounted to the load-bearing frame, and the plurality of electrical conductors embedded within ...
1. A flight vehicle, comprising: a solid-propellant rocket motor;control circuitry; andan electrically-interconnective support structure, comprising:a singular load-bearing frame to which the rocket motor and the control circuitry are mounted such that the rocket motor and the control circuitry are non-rotatable relative to one another, the load bearing frame comprising first, second and third woven layers; anda plurality of electrical conductors embedded within the load-bearing frame and electrically coupling the rocket motor to the control circuitry,a ...