Laser-Controlled Combustion of Solid Propellant-Reference-Cited by-同舟云学术

Laser-Controlled Combustion of Solid Propellant

Published:2014-01 Issue: Volume:884-885 Page:87-90
ISSN:1662-8985
Container-title:Advanced Materials Research
language:
Short-container-title:AMR

Author:

Qin Zhao¹,Wu Jiang¹,Shen Rui Qi¹,Ye Ying Hua¹,Wu Li Zhi¹

Affiliation:

1. Nanjing University of Science and Technology

Abstract

This paper describes experimental work on laser-controlled combustion of solid propellants. Combustion of AP/HTPB, including ignition, combustion, extinction and re-ignition could be controlled by CO2 laser irradiation at the back pressure of 0.1, 0.3 and 0.5 MPa in nitrogen. Burning rate of propellant increased linearly with the increasing of laser power density. Vieilles law was used here to check pressure effect to burning rate, pressure exponent under different power density (except 0.5 MW/m2) are very close to 0.17.

Publisher

Trans Tech Publications, Ltd.

Subject

General Engineering

Link

https://www.scientific.net/AMR.884-885.87.pdf

Reference12 articles.

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3. B.N. Kondrikov, M. Summerfield, T. Ohlemiller. Ignition and gasification of a double-base propellant induced by CO2 laser radiation. Thirteenth International. Symposium on Combustion, Paper No. 129, Aug. 23-29. Univ. of Utah, Salt Lake City, Utah. (1970).

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5. Shen Ruiqi, B.N. Kondrikov, A.P. Denisuke, Ye Yinghua. Combustion characteristics of double base propellant under laser radiation. Applied laser. 2(1) (2003): 29-33.

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