1、This is particularly evident in nitrocellulose propellants.
2、Investigation on NEPE propellants "two-stage-style" ageing kinetics
3、Three propellants are measured and satisfaction results have been obtained.
4、Rapid reactions between liquid propellants can lead to inefficient mixing.
5、Since most of the HTPB propellants possess similar aging mechanism, this model can be used to predict storage life of all HTPB propellants.
6、The method is applicable to both metalized and conventional solid propellants.
7、The closed bomb tests manifest that the apparent burn rates of damaged NEPE propellants vary considerably.
8、Therefore, PEO can be used as the binder of nitrate ester plasticized propellants.
9、Energy density effects on propulsive characteristics of water propellants for laser propulsion
10、Experimental results show that pressure sensitivity of UHBR propellants may be reduced in this way.
11、This paper gives a simplified calculation method which solves equilibrium composition of the combustion products of composite propellants.
12、The high temperature reaction centre above the burning surface of the double base propellants and its variety regulation are found.
13、The combustion properties of the RDX modified small size propellants are determined by a closed vessel and analyzed theoretically.
14、The use of chain extenders ACTS as an important way to control the morphological structure of HTPB propellants binder matrix.
15、The mechanical properties of propellants formulation, which contains PEO binder and is plasticized by nitrate ester were studied.
16、The influence of combustion catalysts on the combustion properties of casting RDX CMDB propellants with middle energy is studied in present paper.
17、The surface modification has been studied on an filler of solid propellants in this paper, by using silane and titanate coupling agents.
18、But the recent confirmation of water sources on the moon and Mars may hint at a future where ALICE and similar rocket propellants become highly practical.
19、Based on an effective nonlinear viscoelastic model, the differential constitutive equation and strain-rate equation of solid composite propellants are induced.
20、Effects of bonding agent BS, cross-linking agent JC, curing agent, binder molecular weight and functionality on mechanical properties of the propellants were studied.
21、The burning rate of the fuel-rich propellants is the parameter which is important for Ducted Rocket design and performance analysis and is main inspection criterions of propellant prescriptions.
22、A clear, colorless, heavy, sweet-smelling liquid, CHCl3, used in refrigerants, propellants, and resins, as a solvent, and sometimes as an anesthetic. Chloroform, once widely used in human and veterinary surgery, has generally been replaced by less toxic, more easily controlled agents.
