Simulation separation device of pico satellite and nano satellite

A satellite simulation and separation device technology, which is applied to the simulation device of space navigation conditions, transportation and packaging, space navigation equipment, etc., can solve the problems of complex structure of simulation equipment and difficult test operation, and achieve low development cost and simple structure , easy-to-control effects

Active Publication Date: 2016-02-03
ZHEJIANG UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] Although the above-mentioned simulation separation methods of pendulum method and free fall method can be used for effective simulation, there are often disadvantages such as complex structure of simulation equipment and difficult test operation.

Method used

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  • Simulation separation device of pico satellite and nano satellite
  • Simulation separation device of pico satellite and nano satellite
  • Simulation separation device of pico satellite and nano satellite

Examples

Experimental program
Comparison scheme
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Embodiment Construction

[0035] Such as Figure 1-10 As shown, the Pina satellite analog separation device of the present embodiment includes: two support frames 1, slide rails 2 horizontally installed on the two support frames, slide seats 3 matched with slide rails 2, and one end fixedly connected to the slide seats. The lanyard 4 and the fixed tooling 5 located below the slide rail 2 and fixedly connected to the separation base plate 101 of the satellite 10, the separation base plate 101 is vertically fixed to make the satellite 10 move and separate in the horizontal direction, and the two ends of the slide rail 2 are respectively fixed on two supports. top of frame 1.

[0036] Each support frame 1 includes: a base 11 , a support rod 12 fixed on the base 11 and two locking rods 13 arranged obliquely on both sides of the support rod 12 .

[0037] Each locking pull rod 13 comprises: the pull rod suspension ring 131 that is arranged on two ends, the pull rod 132 that two joints connect respectively p...

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Abstract

The invention discloses a simulation separation device of a pico satellite and a nano satellite. The simulation separation device comprises two support frames, a sliding rail, a sliding seat, a hanging rope and a fixed tool, wherein the sliding rail is horizontally mounted on the support frames; the sliding seat is matched with the sliding rail; one end of the hanging rope is fixedly connected with the sliding seat; the fixed tool is positioned under the sliding rail and is fixedly connected with the separation bottom plate of the satellite; the other end of the hanging rope is fixedly connected with the satellite, the sliding seat slides to drive the satellite to be separated from the separation bottom plate mounted on the fixed tool in the horizontal direction. According to the simulation separation device disclosed by the invention, a purely mechanical structure is used for fixing and separating a mobile satellite, so that the simulation separation device is simple in structure, convenient to assemble and disassemble and reliable to operate, can adapt to high temperature and low temperature environment, can effectively simulate the separation of the satellite, and is low in development cost.

Description

technical field [0001] The invention relates to an aviation vehicle simulation separation technology, in particular to a Pina satellite simulation separation device. Background technique [0002] With the development of microsatellites and aerospace technology, the separation methods and types of separation devices for microsatellites have become more diverse. However, there are few types of test systems suitable for small satellites to simulate space separation, complex devices, high test costs and limited parameter measurement accuracy. Therefore, the research on separation test technology of microsatellites (picosatellites and nanosatellites) has gradually attracted people's attention. Sufficient simulated separation tests before satellite launch can examine the performance and reliability of the separation system, especially for modern small satellites that quickly absorb new technologies. There are various separation methods and separation devices for modern small sate...

Claims

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Application Information

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IPC IPC(8): B64G7/00
Inventor滕来金仲和
OwnerZHEJIANG UNIV