[go: up one dir, main page]

Tu et al., 2022 - Google Patents

Thermal decomposition, ignition process and combustion behavior of nitrate ester plasticized polyether propellant at 0.1–3.0 MPa

Tu et al., 2022

View PDF @Full View
Document ID
4526951549287615583
Author
Tu C
Feng Y
Ling Z
Chen X
Zhou C
Li Y
Li W
Cai W
Publication year
Publication venue
International Journal of Aerospace Engineering

External Links

Snippet

Nitrate ester plasticized polyether (NEPE) propellant is widely used in solid rocket motors, having both good mechanical properties and high specific impulse. However, its ignition and combustion process are complex and need to be better understood. In this study, a high …
Continue reading at onlinelibrary.wiley.com (PDF) (other versions)

Classifications

    • C—CHEMISTRY; METALLURGY
    • C06—EXPLOSIVES; MATCHES
    • C06B—EXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
    • C06B45/00—Compositions or products which are defined by structure or arrangement of component of product
    • C06B45/18—Compositions or products which are defined by structure or arrangement of component of product comprising a coated component
    • C06B45/20—Compositions or products which are defined by structure or arrangement of component of product comprising a coated component the component base containing an organic explosive or an organic thermic component
    • C—CHEMISTRY; METALLURGY
    • C06—EXPLOSIVES; MATCHES
    • C06B—EXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
    • C06B33/00—Compositions containing particulate metal, alloy, boron, silicon, selenium or tellurium with at least one oxygen supplying material which is either a metal oxide or a salt, organic or inorganic, capable of yielding a metal oxide
    • C06B33/12—Compositions containing particulate metal, alloy, boron, silicon, selenium or tellurium with at least one oxygen supplying material which is either a metal oxide or a salt, organic or inorganic, capable of yielding a metal oxide the material being two or more oxygen-yielding compounds
    • C—CHEMISTRY; METALLURGY
    • C06—EXPLOSIVES; MATCHES
    • C06B—EXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
    • C06B45/00—Compositions or products which are defined by structure or arrangement of component of product
    • C06B45/12—Compositions or products which are defined by structure or arrangement of component of product having contiguous layers or zones

Similar Documents

Publication Publication Date Title
Sandall et al. A study of solid ramjet fuel containing boron–magnesium mixtures
Liang et al. Improvement in energy release properties of boron-based propellant by oxidant coating
Liu et al. Effect of magnesium on the burning characteristics of boron particles
Li et al. The effect of pressure and oxygen concentration on the ignition and combustion of aluminum–magnesium fuel-rich propellant
Gottfried et al. Laser-shocked energetic materials with metal additives: evaluation of chemistry and detonation performance
Connell Jr et al. Boron and polytetrafluoroethylene as a fuel composition for hybrid rocket applications
US9227883B2 (en) Mechanically activated metal fuels for energetic material applications
Singh et al. Thermal degradation kinetics and reaction models of 1, 3, 5-triamino-2, 4, 6-trinitrobenzene-based plastic-bonded explosives containing fluoropolymer matrices
Collins et al. Laser‐induced Deflagration for the Characterization of Energetic Materials
Courty et al. Experimental determination of ignition and combustion characteristics of insensitive gun propellants based on RDX and nitrocellulose
Demko et al. Ignition delay times of composite solid propellants using novel nano-additive catalysts
Elghafour et al. Highly energetic nitramines: A novel platonizing agent for double-base propellants with superior combustion characteristics
Tu et al. Thermal decomposition, ignition process and combustion behavior of nitrate ester plasticized polyether propellant at 0.1–3.0 MPa
Li et al. Experimental investigation on laser ignition and combustion characteristics of NEPE propellant
Korotkikh et al. Effect of Me/B‐powder on the ignition of high‐energy materials
Zhou et al. Differences of thermal decomposition behaviors and combustion properties between CL-20-based propellants and HMX-based solid propellants
Uhlenhake et al. Laser ignition of solid propellants using energetic nAl-PVDF optical sensitizers
Hedman et al. Experimental investigation of the decomposition preceding cookoff in a composite propellant
Zhang et al. Effect of the microporous structure of ammonium perchlorate on thermal behaviour and combustion characteristics
Hu et al. Experimental investigation on combustion of high-metal magnesium-based hydroreactive fuels
Bekhouche et al. Towards understanding the effect of temperature and humidity on the safety and performance of tracer pyrotechnic composition
Yan et al. Study on the ignition process and characteristics of the nitrate ester plasticized polyether propellant
Chen et al. Heat conduction and deflagration behavior of Al/PTFE induced by thermal shock wave under temperature gradient
Zhang et al. Investigation of aluminum particle ignition dynamics in various propellant environments
Nie et al. Evolution of structural damage of solid composite propellants under slow heating and effect on combustion characteristics