To provide a solid fuel composition for rockets which expands the design range of a rocket in accordance with desired applications by lowering the burning rate and decreases the pressure dependence of the burning rate and to provide a method of improving the burning rate of a solid fuel for roc...
多点抛撒 1. A Research on the Explosion Character of Multi-point Dispersal Cloud; 多点抛撒云雾爆炸特性研究3) submunition dispenser 子弹药抛撒装置4) rocket casting Bt powder 火箭抛撒剂型5) dispersing [英][dis'pə:s] [美][dɪ'spɝs] 抛撒 1. The simulating results show that...
aSprocket 扣练齿轮[translate] aformulation and implement 公式化和贯彻[translate] aentry 词条[translate] aKicaZ 正在翻译,请等待...[translate] aOh,it says parking isn't allowed here. 噢,它认为停车处这里没有承认。[translate] aAnalysis of this vendor does not have any abnormal 正在翻译,请等待...
An incendiary device such as artillery round, rocket warhead, bomb, or grenade in which a high explosive charge within a casing has imbedded therein a plurality of balls of incendiary material which is a mixture of silicone rubber, powdered magnesium, and an oxidizing agent. The balls are ignit...
It is an object of the present invention to provide a liquid hydrocarbon fuel composition of high density and high heat of combustion which has low pour point and which is suitable for rocket or jet engine fuel composition. It is another object of the present invention to provide a fuel comp...
An igniter composition is provided including metal fuel particles having a predetermined average diameter and metallic oxide oxidizer particles having a predetermined average diamet
A composition consisting of 80% polytetrafluoroethylene and 20% boron (by weight) was considered as a potential high-density solid fuel mixture for mixed hybrid rocket propulsive applications. Constant-pressure strand burner experiments ... SP Section,B Factor,S Calorimetry,... 被引量: 1发表: ...
The patent describes a high energy propellant composition comprising a binder, oxidant, fuel and plasticizer. An energetic binder for said composition is p... DV Sickman,MJ Kamlet,RD Rich,... - US 被引量: 14发表: 1973年 Composite rocket propellant composition with a controllable pressure expon...
PALMS acquired mass spectra of over 2300 exhaust particles within the plumes of an Athena II rocket and the Space Shuttle. The majority of positive spectra indicated the presence of primary and trace components of the aluminum fuel and the combustion catalyst. Negative spectra showed chlorine from ...
A composition consisting of 80% polytetrafluoroethylene and 20% boron (by weight) was considered as a potential high-density solid fuel mixture for mixed hybrid rocket propulsive applications. Constant-pressure strand burner experiments ... SP Section,B Factor,S Calorimetry,... 被引量: 1发表: ...