๐”– Bobbio Scriptorium
โœฆ   LIBER   โœฆ

Correlation of Specific Impulse and Ignition Delay in Liquid Rocket Propellants

โœ Scribed by K. Kishore; M. R. Sunitha


Book ID
105355053
Publisher
John Wiley and Sons
Year
1977
Tongue
English
Weight
158 KB
Volume
2
Category
Article
ISSN
0721-3115

No coin nor oath required. For personal study only.

โœฆ Synopsis


Abstract

Theoretically there seems to be a linear dependence between specific impulse and the ignition delay in liquid bipropellant systems. It has been observed that the plot of specific impulse versus mixture ratio of various systems based on red fuming nitric acid oxidizer show a maximum. The ignition delay versus mixture ratio plot of the same systems on the other hand show a minimum at a mixture ratio which corresponds to the maximum specific impulse. Thus, the mixture corresponding to maximum performance of a liquid bipropellant system could be qualitatively predicted from the ignition delay measurements.


๐Ÿ“œ SIMILAR VOLUMES


Variable structure control of time-delay
โœ Feng Zheng; Mian Cheng; Wei-Bing Gao ๐Ÿ“‚ Article ๐Ÿ“… 1995 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 699 KB

The dynamical model of combustion in liquid propellant rocket motors is an unstable time-delay system. When it is stabilized by alinear state feedback controller, the robustness of the closed-loop system is not satisfactory. In this paper a variable structure control approach to stabilize the combus