Pathogen
发表于 2025-3-28 16:36:24
Current Problems in Energetic Materials Ignition Studiesr. Scientific investigation of the EMs ignition has started at the end 1930th when the first field missiles (Katyusha) were developed in the USSR. Later the investigations were actively performed in USA and Europe but despite rather long history there still remain unsolved problems related to comple
FAZE
发表于 2025-3-28 21:47:55
Transient Burning of nAl-Loaded Solid Rocket Propellantsion community. While steady combustion regimes of solid rocket propellants loaded with nanometals are discussed in a companion paper, several instances of unsteady combustion regimes are examined in this paper. Ignition, extinction by fast depressurization, self-sustained oscillatory burning, pressu
洞穴
发表于 2025-3-29 02:37:24
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coddle
发表于 2025-3-29 04:20:52
Bimetal Fuels for Energetic Materialsials. However, the use of aluminum is complicated by the fact that during storage and combustion on the surface of the particles an inert oxide layer is formed, which prevents the access of an oxidizer and increases the ignition and burning times of particles. Prospective solution to the problem of
Crumple
发表于 2025-3-29 08:01:49
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Accommodation
发表于 2025-3-29 11:27:06
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Harpoon
发表于 2025-3-29 19:38:03
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流利圆滑
发表于 2025-3-29 20:19:37
Survey of Low-Burn-Rate Solid Rocket Propellantsrn rates, several applications benefit from propellants with decreased regression rates. This includes solid rocket motors as well as gas generators. Background descriptions of the general aspects that impact on the burn rate of composite propellants are provided. Focus is given to means that enable
happiness
发表于 2025-3-30 00:05:22
Burning Rate of PVC—Plastisol Composite Propellants and Correlation Between Closed Vessel and Strandt correlation of the measured data. The well-known strand burner test (Crawford test) and the closed vessel test were employed. In order to clarify the relation between the two techniques, a composite propellant containing polyvinyl chloride (PVC) as matrix and ammonium perchlorate (AP) as an oxidiz
放气
发表于 2025-3-30 05:50:26
Modern Approaches to Formulation Design and Productionr propellants. It is now possible to approach the problem of matching formulation to desired characteristics in a systematic manner. This approach can cover all aspects from conception to disposal and includes performance optimization. This chapter will discuss and illustrate this: beginning with th