Launcher for meteorological sounding rocket

A sounding rocket and launcher technology, applied in the field of meteorological detection, can solve the problems of inconvenient adjustment of launch angle, difficulty in field power supply, easy deviation of launch angle, etc. Effect

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  • Abstract
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  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] At present, under severe weather conditions, the overall stability of the sounding rocket is poor when it is launched, and the launch angle is easy to deviate, so that the follow-up sounding rocket cannot reach the predetermined detection height and can not reduce the distance between the ballistic apex and the landing point. Scattering, and at the same time, the launch angle is not easy to adjust, and it is difficult to supply power in the field, which affects the follow-up meteorological sounding work

Method used

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  • Launcher for meteorological sounding rocket
  • Launcher for meteorological sounding rocket
  • Launcher for meteorological sounding rocket

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Embodiment Construction

[0032] The following will be combined with Figure 1-9 The present invention is described in detail, and the technical solutions in the embodiments of the present invention are clearly and completely described. Apparently, the described embodiments are only some of the embodiments of the present invention, not all of them. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.

[0033] The present invention provides a meteorological sounding rocket launcher through improvement, including a connecting rod 1, a pivot pin A2, a pivot pin B3, a first washer 4, a first nut 5, a second nut 6, an orienter 7, and a support base 8 and traction chassis 9, one end of the top of the connecting rod 1 is connected to the bottom middle of the orienter 7, one end of the bottom side is connected to the upper end of the support seat 8 throug...

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Abstract

The invention discloses a launcher for a meteorological sounding rocket. The launcher for the meteorological sounding rocket comprises a connecting rod, a shaft pin A, a shaft pin B, a first gasket, afirst nut, a second nut, an orientator, a supporting seat and a traction chassis. The launcher for the meteorological sounding rocket is stable in overall structure and suitable for operation under severe weather conditions; a launching angle adjusting mechanism adopts a connecting rod mechanism for driving a screw rod to transmit by a motor; the orientator adopts four guide rails to be combinedwith a middle ring A and a middle ring B to form a launching rail, the launching caliber is 122 mm, the maximum angle of the high-low launching angle is not less than 80 degrees, the height of the launcher in the transportation state is not larger than 3 m, and the stability is high; a supporting part adopts the motor to drive a trapezoidal lead screw shaft to rotate to drive the connecting rod tomove front and back so as to achieve the purpose of adjusting the launching angle, and a manual mode can be quickly switched; and a rocket operation automatic parameter recording instrument or a wireless launching controller can be used for control, and a high-power lithium battery is carried, so that the field power supply problem is solved.

Description

technical field [0001] The invention relates to the related field of meteorological detection, in particular to a meteorological sounding rocket launcher. Background technique [0002] Sounding rockets are rockets used for detection and scientific experiments in near-Earth space. Sounding rockets can be used to detect the structural components and parameters of each layer of the atmosphere in the altitude direction. Sounding rockets are effective detection tools under severe weather conditions. [0003] At present, under severe weather conditions, the overall stability of the sounding rocket is poor when it is launched, and the launch angle is easy to deviate, so that the follow-up sounding rocket cannot reach the predetermined detection height, and it is impossible to reduce the distance between the ballistic apex and the landing point. At the same time, it is not easy to adjust the launch angle, and it is difficult to supply power in the field, which affects the follow-up ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F41F3/04
CPCF41F3/04
Inventor 龚毅王璞朱科平邵文政顾春涛邹春根曾闰平刘磊黄欢常江何玥帅
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