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PULSE NOZZLE SETUP WITH A CHARGE OF HIGH-DENSITY COMPOSITE PROPELLANT BURNING IN THE LOW-VELOCITY DETONATION MODE
Author(s) -
А. А. Сулимов,
Б. С. Ермолаев,
V. E. Khrapovskii,
A. V. Roman’kov
Publication year - 2018
Publication title -
gorenie i vzryv (moskva) — combustion and explosion
Language(s) - English
Resource type - Journals
ISSN - 2305-9117
DOI - 10.30826/ce18110112
Subject(s) - propellant , detonation , nozzle , mechanics , materials science , composite number , mode (computer interface) , pulse (music) , charge (physics) , atomic physics , composite material , explosive material , thermodynamics , physics , aerospace engineering , chemistry , optics , engineering , organic chemistry , quantum mechanics , detector , computer science , operating system
The results of investigation concerning application of low-velocity detonation (LVD) in high-density block charges for developing small-size nonexplosive rocket motors with high thrust and short operation time (1–2 ms) are considered. Firings are carried out in the laboratory nozzle setup consisting of the cylindrical chamber and nozzle block with a nozzle-diffuser. The propellant charges are prepared by pressing to a porosity of 2%–4% of the mixture of ammonium perchlorate (AP) with polymethylmethacrylate (PMMA) 85/15 or three-component mixture of these compounds with 15% of RDX additive. Low-velocity detonation was induced in the charge by the igniter with the subsequent acceleration of the burning wave in a booster charge, that is, a pellet of pressed RDX. Properties of the pellet were selected so that the acceleration of burning at its butt end resulted in LVD with the velocity of 1.4–2 km/s. The same process was obtained in the propellant charge. The investigation conducted shows that the pressed mixture charges provide a steady work of the nozzle setup with a high specific impulse of the thrust. In firings of the base configuration with the loading density of 0.65 g/cm, the specific impulse was 222 s for mixture PMMA/AP 15/85 and 236 s for the mixture with the RDX additive. The key factors affecting specific impulse are the length of the afterburning cavity and the expansion ratio of the nozzle. As the expansion ratio increased to 10, the specific impulse exceeded 250 s. The most part of chemical energy releases in a dense cloud of burning particles produced behind the LVD wave front. Pressure measurements conducted with the use of high-frequency piezoelectric gauges show that pressure in the LVD wave propagating along the charge is typically 1–1.2 GPa. After the LVD wave passes from the charge into the afterburning cavity, the peak pressure reduces to 300–400 MPa. A high pressure inherent in the LVD has positive aspects: it reduces the burning time and raises the specific impulse.

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