|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||60/260 ; 60/267|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 7 인용 특허 : 0|
Each of the tubes of the tube thrust chamber of a rocket engine is hooked at either end with the end at the outlet oriented horizontally relative to the rocket engine\s center line and the end at the inlet oriented vertically and bent outwardly away from the rocket thrust chamber and facing the outlet for fitting into apertures formed in the outlet and inlet manifolds. The method of construction and assembly is manifested by assembling the sub-assembly of the wedge ring/manifold above the open ends of the vertical portion of the tubes and lowering the as...
A rocket engine having a thrust chamber comprising a combustion chamber having an inlet and being generally conical or bell shaped and a nozzle having an exit and being generally conical or bell shaped and defining a throat section, said thrust chamber being formed from a plurality of tubes having passages extending from adjacent to the inlet of said combustion chamber to adjacent to the exit of said nozzle comprising a first annular manifold circumscribing said thrust chamber in proximity to said thrust chamber and adjacent to said exit, each of said tu...