公开(公告)号：KR101266970B1

公开(公告)日：2013-05-30

申请号：KR1020110127135

申请日：2011-11-30

Applicant: 한국항공대학교산학협력단 ,  한국항공우주연구원

Inventor： 박정선 ,  김현덕 ,  김성훈 ,  임재혁

IPC: B64G1/62 ,  B64G1/14

CPC classification number: B64G1/62 ,  B64G2001/1071

Abstract: PURPOSE: A deployment apparatus for landing a space exploration satellite is provided to increase the internal space utilization of the space exploration satellite because the installed space of the deployment apparatus is reduced by applying a hinge rotation structure. CONSTITUTION: A deployment apparatus for landing space exploration satellite comprises a first support rod(100), a second support rod(200), and an elastic rotation unit. The second support rod is installed to restrict the rotation by a structure of the space exploration satellite. The elastic rotation unit connects the first and second support rods and rotates the second support rod against the first support rod when the restriction of the second support rod is released.

Abstract translation: 目的：提供用于着陆空间探测卫星的部署装置，以增加空间探测卫星的内部空间利用，因为通过施加铰链旋转结构来减少展开装置的安装空间。 构成：着陆空间探测卫星的展开装置包括第一支撑杆（100），第二支撑杆（200）和弹性旋转单元。 安装第二支撑杆以通过空间探测卫星的结构限制旋转。 当释放第二支撑杆的限制时，弹性旋转单元连接第一和第二支撑杆并使第二支撑杆旋转抵靠第一支撑杆。

公开(公告)号：KR1020130060855A

公开(公告)日：2013-06-10

申请号：KR1020110127134

申请日：2011-11-30

Applicant: 한국항공대학교산학협력단 ,  한국항공우주연구원

Inventor： 박정선 ,  김현덕 ,  김성훈 ,  임재혁

IPC: B64G1/22 ,  B64G1/16 ,  B64C25/10 ,  B64G1/14

CPC classification number: B64G1/62 ,  B64G2001/1071

Abstract: PURPOSE: A deployment device for landing a space exploring satellite is provided to improve utilization of an inner space of the space exploring satellite by reducing a space occupied inside the space exploring satellite through supplying hinge rotation structure. CONSTITUTION: A deployment device for landing a space exploring satellite comprises a first support rod(100), a second support rod(200), a hinge bracket(300), and an elasticity deployment unit(400). The second support rod is installed to be rotated by the structure of the space exploring satellite. The hinge bracket connects the first support rod and the second support rod and is equipped on the first support rod and the second support rod to be hinge-rotated. The elasticity deployment unit surrounds the first support rod and rotates the second support rod and the hinge bracket with respect to the first support rod by elastically pressurizing the hinge bracket when the restricting state of the second support rod is released.

Abstract translation: 目的：提供用于着陆探空卫星的部署装置，通过减少通过提供铰链旋转结构探索卫星的空间，从而提高对探空卫星空间的利用。 构成：用于着陆探空卫星的展开装置包括第一支撑杆（100），第二支撑杆（200），铰链支架（300）和弹性展开单元（400）。 第二支撑杆安装成由探空卫星的结构旋转。 铰链支架连接第一支撑杆和第二支撑杆，并且装配在第一支撑杆和第二支撑杆上以进行铰链旋转。 当释放第二支撑杆的限制状态时，弹性展开单元围绕第一支撑杆并相对于第一支撑杆旋转第二支撑杆和铰链支架，弹性地对铰链支架施加压力。