DEVELOPMENT OF ENERGETIC ADDITIVES FOR PROPELLANTS IN CHINA

Citation
Yx. Ou et al., DEVELOPMENT OF ENERGETIC ADDITIVES FOR PROPELLANTS IN CHINA, Journal of propulsion and power, 11(4), 1995, pp. 838-847
Citations number
69
Categorie Soggetti
Aerospace Engineering & Tecnology
ISSN journal
07484658
Volume
11
Issue
4
Year of publication
1995
Pages
838 - 847
Database
ISI
SICI code
0748-4658(1995)11:4<838:DOEAFP>2.0.ZU;2-4
Abstract
The development of energetic azide binders and plasticizers for solid propellants in China is described in this article. Fourteen representa tives of azides synthesized mainly by the authors on a small laborator y scale are involved. The reaction routes and conditions for preparing these azides are summerized; performance of the azides, including den sity, melting point, enthalpy of formation, thermal decomposition temp erature determined by differential scanning calorimetry or differentia l thermal analysis, impact sensitivity, etc, were tested and are prese nted. The application of these azides to solid propellants or plastic- bonded explosives is still comparatively new in this country, with ver y little information available at the present time. A few results are briefly mentioned in this article. We arrange the stated azides under the following six categories: 1) azide polyether: glycidyl azide polym er ([C3H5N3O])(n), the homopolymer of 3,3-bis(azidomethyl) oxetane (C5 H8N6O) (BAMO), and the copolymer of BAMO/tetrahydrofuran (C4H8O); 2) A zidonitramine: 1,5-diazido-3-nitrazapentane, N-nitro-N-azidomethylgemd initroethyl methylamine, and isfazidomethylgemdinitroethyl)ethylenedin itramine; 3) Azidonitro compounds:2nitro-2-methyl-1,3-diazidopropane, 2-nitro-2-azidomethyl-1,3-diazidopropane and 1-azido-2-(2,4,6-trinitro phenyl) ethane; 4) aliphatic azide: 1,2,4,triazidobutane and tetraazid omethylemethane; 5) Azidonitrate: pentaerythritol diazido dinitrate; a nd 6) oxygen heterocyclic azide: 3-azidomethyl-3-ethyloxetane, and 2,2 -dimethyl-5-azidomethyl-5-nitro-1,3-dioxane.