A moonlet configuration deployed for constellations comprises a load module (1-0), a service module (2-0), a propulsion module (3-0), a + Y plate (41), a -Y plate (42), a solar wing (411) and a battery pack. The load module (1-0) comprises a + Z plate (11), a + X plate (12), a partition plate (13) and load equipment mounted on the + Z plate (11), the + X plate (12) and the partition plate (13); the service module 2-0 comprises a -Z plate (21) and platform equipment mounted on the -Z plate (21); the propulsion module 3-0 comprises a -X plate (31) and electric propulsion equipment mounted on the -X plate (31); the storage battery pack (312) is mounted on the outer side of the -X plate (31) or the outer side of the + X plate (12) according to the mass of the whole satellite; the solar wing (411) is mounted on the + Y plate (41) and the -Y plate (42); the + X plate (12), the -X plate (31), the + Y plate (41), the -Y plate (42), the + Z plate (11) and the -Z plate (21) form a right-angle hexahedron with a trapezoidal cross section; and the partition plate is located in the right-angle hexahedron.
一种面向星座部署的小卫星构型,包括载荷模块(1‑0)、服务模块(2‑0)、推进模块(3‑0)、+Y板(41)、‑Y板(42)、太阳翼(411)、电池组;载荷模块(1‑0)包括+Z板(11)、+X板(12)、隔板(13),以及安装在+Z板(11)、+X板(12)、隔板(13)上的载荷设备;服务模块2‑0包括‑Z板(21)、安装在‑Z板(21)上的平台设备;推进模块3‑0包括‑X板(31)、安装在‑X板(31)上的电推进设备;蓄电池组(312)根据整星质量安装在‑X板(31)的外侧或+X板(12)的外侧;太阳翼(411)安装在+Y板(41)和‑Y板(42)上;+X板(12)、‑X板(31)、+Y板(41)、‑Y板(42)、+Z板(11)、‑Z板(21)组成横截面为梯形的直角六面体;隔板位于直角六面体内。
Moonlet configuration deployed for constellations and modular assembly method
一种面向星座部署的小卫星构型及模块化组装方法
2021-08-20
Patent
Electronic Resource
Chinese
IPC: | B64G Raumfahrt , COSMONAUTICS |
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