Separate-orbit CubeSat launching device

A launching device and CubeSat technology, which is applied in the field of separate orbital CubeSat launching devices, can solve problems such as excessive rotation, anti-recovery of hatch doors, and ejection of push plates, and achieves a system with increased applicability, easy reprocessing, and guaranteed stability. Effect

Active Publication Date: 2015-04-29
NANJING UNIV OF SCI & TECH
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AI Technical Summary

Problems solved by technology

[0005] (1) Cost problem: the structure is exquisite and complex, and the processing cost and processing accuracy are high;
[0006] (2) The problem of hatch rotation: when the unlocking device is unlocked, the hatch opens and may rotate excessively, colliding with the carrying platform, causing unnecessary damage;
[0007] (3) Anti-restoration of the cabin door: During the release process of the microsatellite, if the cabin door recovers during the rotation process, it will affect the release of the microsatellite, and may even cause damage to the microsatellite;
[0008] (4) The problem of push plate coming out: the push plate is between the spring and the micro-satellite, and the small satellite is pushed out o

Method used

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  • Separate-orbit CubeSat launching device
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  • Separate-orbit CubeSat launching device

Examples

Experimental program
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Effect test

Embodiment

[0062] combine Figure 1 to Figure 17 :

[0063] In the following, for convenience, the 1-unit CubeSat is referred to as 1U, the 2-unit CubeSat is referred to as 2U, the 3-unit CubeSat is referred to as 3U or 3U+, and the 6-unit CubeSat is referred to as 6U.

[0064] A separate track type CubeSat launching device, comprising a main frame, a spring mechanism, and an unlocking mechanism; the main frame includes a cabin door 1, a door stopper 2, a bottom plate 3, a side plate 4, an upper cover plate 5 and a rear cover 6, and the side plate 4 are symmetrically arranged on both sides of the bottom plate 3, and the upper cover plate 5 is arranged on the top of the side plate 4, and the satellite slide rail for satellite sliding is fixed in the main frame by screws; the door baffle plate 2 and the rear cover 6 are respectively fixedly installed on the front and rear of the frame, The bottom end of the door baffle 2 exceeds the position of the bottom plate 3 to set the shaft seat, an...

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Abstract

The invention discloses a separate-orbit CubeSat launching device for carrying or launching a single or a plurality of standard CubeSat. The separate-orbit CubeSat launching device mainly comprises a rectangular framework, an unlocking mechanism and a spring mechanism, wherein the rectangular framework is mainly constructed by connecting a cabin door, a baffle plate, bottom plates, side plates, upper cover plates and a back cover plate in a threaded way; a separate guide rail is arranged as a satellite slide rail; a rotary electromagnet and the like are taken as the unlocking mechanism; the spring mechanism comprises a push plate and pressure springs. The separate-orbit CubeSat launching device has high generality, and is low in cost; the transportation safety and launching reliability of satellites can be ensured, displacement of the satellites during transportation can be prevented, and the cabin door is not collided with a running platform or reversed in an opening process; moreover, a push plate anti-separation measure and the like are adopted.

Description

technical field [0001] The invention belongs to the technical field of standard cubesat carrying and launching, in particular to a separate orbit type cubesat launching device. Background technique [0002] With the development of microelectronics technology, new materials, new energy and other technologies, the application of microsatellites has developed rapidly. At present, they are mainly used for communication, remote sensing of the earth, interplanetary exploration, scientific research and technical experiments, etc., and also have military applications. Wide application prospects, so many countries have included it in the national research plan, as a commanding height of technology and economic development in the 21st century. my country Aerospace Dongfanghong Satellite Company, Shanghai Microsatellite Engineering Center of the Chinese Academy of Sciences, National University of Defense Technology, Tsinghua University, Harbin Institute of Technology, Zhejiang Universi...

Claims

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Application Information

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IPC IPC(8): B64G1/64
Inventor 沈娜包家倩张祥金廖桥生吴志亮
Owner NANJING UNIV OF SCI & TECH
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