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.