Ignition characteristics of AP-based composite solid propellants that contained either HMX or RDX, were investigated using a CO2 laser at relatively low heat flux and subatmospheric pressures, in order to simulate space environments and also simplify our understanding of the nature of ignition pheno
Ignition of composite solid propellant at subatmospheric pressures
โ Scribed by Michiko Harayama; Takeo Saito; Akira Iwama
- Publisher
- Elsevier Science
- Year
- 1983
- Tongue
- English
- Weight
- 538 KB
- Volume
- 52
- Category
- Article
- ISSN
- 0010-2180
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โฆ Synopsis
The ignition of composite solid propellants by CO 2 laser irradiation at low pressures has been investigated experimentally. Three ignition modes are found at subalJnospheric pressures: self-sustaining ignition, non-self-sustaining ignition, and pulsating ignition. Here, the self-sustaining and the non-self-sustaining ignition modes have been studied. Samples of an ammonium perehlorate/polybutadiene propellant were ignited. The incipient flame was detected with a phototransistor, and the temperatures at the surface and in the solid phase were measured by means of Type K thermocouples. Aspects of surface regression were recorded by photography. It is found that non-self-sustaining ignition occurs in the lower pressure range and with the higher incident heat flux from the laser. At ignition, the heat loss into the solid phase in the non-self-sustaining mode is much larger than that in the self-sustaining one. It is concluded that these ignition modes are determined independently of the exposure time after the flame's appearance.
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