An underwater rocket thrust performance test device

A test device and rocket technology, applied in ammunition testing, ammunition, offensive equipment, etc., can solve problems such as the difficulty of accurately obtaining engine performance parameters, and achieve high objectivity, improved accuracy, and strong reliability

Active Publication Date: 2022-07-29
HEBEI HANGUANG HEAVY IND
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] Normally, it is quite difficult to obtain engine performance parameters accurately in underwater rocket thrust test system experiments
Due to the complexity of the underwater test environment, there are great limitations in carrying out underwater projectile thrust test experiments

Method used

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  • An underwater rocket thrust performance test device
  • An underwater rocket thrust performance test device
  • An underwater rocket thrust performance test device

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Embodiment Construction

[0033] The present invention will be described in detail below with reference to the accompanying drawings and embodiments.

[0034] The present invention provides an underwater rocket thrust performance test device, comprising a rocket engine 1, a thrust test bench, a data acquisition system 14, a high-pressure water vapor bottle 15 and a temperature control box 16, specifically as follows figure 2 shown.

[0035] The thrust test bench is placed in the pool to simulate the underwater working environment of the rocket; in order to better simulate the underwater working environment, the thrust test bench is set at a depth of 5m under the pool in the embodiment of the layout fee.

[0036] The rocket engine 1 is connected to the whole bomb of the rocket and placed horizontally on the thrust test bench;

[0037] The thrust test bench includes a base 7, a front support, a rear support, a head support 11, a moving frame 8, a main bearing device 10, a lateral force sensor 2, a vert...

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Abstract

The invention discloses an underwater rocket thrust performance testing device, which relates to the technical field of underwater weapon thrust testing, which can simulate the underwater working environment of the rocket, objectively reflect the working performance of the underwater rocket, and further improve the Provide technical reference for optimized design. The device includes a rocket engine, a thrust test bench, a data acquisition system, a high-pressure water vapor bottle, and a temperature control box. The underwater rocket thrust performance test device provided by the invention can realize the thrust test in the underwater environment, simulate the working process of the missile engine in the real environment, and overcome the defect that the traditional ground thrust test method does not consider the influence of the water medium. The control completes multi-channel data acquisition, high-pressure water vapor inlet flow control, and online calculation of underwater projectile thrust performance parameters. The data obtained by this method can more objectively and truly reflect the working conditions of underwater bombs, and has the advantages of high precision and strong reliability.

Description

technical field [0001] The invention relates to the technical field of thrust testing of underwater weapons, in particular to an underwater rocket thrust performance testing device. Background technique [0002] As a preset equipment for underwater defense, the new underwater rocket weapon engine system usually uses nano-metal aluminum powder as fuel and water as oxidant. Under certain conditions, a violent reaction occurs and a large amount of thermal energy is released for work. The energy density is ordinary 4 times the fuel, can greatly increase its combat range and speed. [0003] The propellant in the engine system usually uses HTPB (hydroxyl-terminated polybutadiene) as the binder, a small amount of AP (ammonium perchlorate) as the oxidant, and nano-metal aluminum powder as the fuel, and the aluminum powder content is as high as 80%. After the initial combustion of the aluminum-based fuel in the combustion chamber, it reacts with the water entering the combustion cha...

Claims

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Application Information

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Patent Type & AuthorityPatents(China)
IPC IPC(8): F42B35/02
CPCF42B35/02
Inventor王金云王孟军可伟
OwnerHEBEI HANGUANG HEAVY IND