𝔖 Bobbio Scriptorium
✦   LIBER   ✦

Aerothermochemical studies of energetic liquid materials. 2. Combustion and microexplosion of droplets of organic azides

✍ Scribed by A. Lee; C.K. Law; A.L. Randolph


Publisher
Elsevier Science
Year
1988
Tongue
English
Weight
942 KB
Volume
71
Category
Article
ISSN
0010-2180

No coin nor oath required. For personal study only.

✦ Synopsis


An experimental investigation has been conducted on the vaporization, combustion, and microexplosion characteristics of freely falling droplets of organic azides in hot oxidizing or inert environments. The droplet gasification rate and the state of microexplosion have been measured. Results show that, compared with the conventional hydrocarbon fuels, droplets of azido fuels gasify faster and microexplode earlier in the droplet lifetime. The effect is especially strong for n-alkyl diazides whose gasification rates can exceed those of the corresponding nalkanes by several hundred percent. Such strong responses are believed to be caused by the exothermic decomposition of the azides either in the liquid phase or upon gasification. Other important and interesting effects studied include molecular branching, OH-substitution, the proximity and number of the azide groups, and alcohol and halide blending.


πŸ“œ SIMILAR VOLUMES


Aerothermochemical studies of energetic
✍ A. Lee; C.K. Law; A. Makino πŸ“‚ Article πŸ“… 1989 πŸ› Elsevier Science 🌐 English βš– 631 KB

l)epartment of .\*Β’lechanicul Engineering, (.,'niver~ty ol ( 'tdifornia, l)m'i~', ('4 95616 l'hr.mgh either direct measurement or group additivily calculation, the densitms, normal b~filing points, latent heatof vaporization, limits of superheat, enthalpies of formation, combustion anti dccompositio

Aerothermochemical studies of energetic
✍ D.L. Zhu; C.K. Law πŸ“‚ Article πŸ“… 1987 πŸ› Elsevier Science 🌐 English βš– 571 KB

The gasification and microexplosion characteristics of droplets of liquid gun propellants under atmospheric pressure have been experimentally investigated. Results show that the propellant explosion temperature is around 200"C and is substantially in excess of previously reported values. The droplet