Ignition driving system of high-overload test device used for solid-propellant rocket engine

Abstract

The invention discloses an ignition driving system of a high-overload test device used for a solid-propellant rocket engine, relates to an ignition driving system used for a solid-propellant rocket engine experimental apparatus and in particular to an ignition driving system used for a solid-propellant rocket engine under the high-overload rotation test condition, and belongs to the field of aerospace. The ignition driving system comprises a long-distance integrated console, an ignition power supply control module, a test controller, a relay driving module, a solid-propellant rocket engine and an ignition tool, wherein the relay driving module is fixed on a noseplate on the central axis plane of a rotary test bench, and the axial line between the relay moving contact C and the relay stationary contact D in the relay driving module is tangent to a rotary table top. The ignition driving system can reduce or eliminate the adverse effect of radial centrifugal inertia and tangential acceleration impact on the relay driving module in the ignition power supply loop under the high-overload test condition. The ignition driving system has high dynamic operating precision and can be used for reliably and safely carrying out a continuous ignition test on solid-propellant rocket engines under high-overload rotary conditions.

Description

Technical field [0001] The invention relates to an ignition driving system for a solid rocket motor experimental device, in particular to an ignition driving system for a solid rocket motor under high overload rotation test conditions, and belongs to the field of aerospace. Background technique [0002] The high maneuverability and high-speed rotation during the flight of modern missiles will cause the solid rocket motor on it to bear high overload, which puts forward corresponding requirements for the design and development of solid rocket motors. On the one hand, overload acceleration will increase the burning rate of the propellant, induce the increase in combustion chamber pressure and shorten the combustion time, and ultimately lead to changes in the internal ballistic performance of the engine; on the other hand, high overload will seriously affect the movement of condensed particles. Deteriorating the working environment of the engine's thermal insulation layer, in severe ...

AI Technical Summary

Problems solved by technology

[0006] The invention discloses an ignition drive system used for a solid rocket motor high overload test device. The technical problem to be solved is to reduce or avoid the impact of the relay drive module in the ignition power circuit under the high overload (0-100g) test environment. Adverse Effects of Radial Centrifugal Inertia and Tangential Acceleration Shock

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