SUMMARY
Atomized kerosene can ignite with a spark or plasma arc under controlled conditions of 1-2 atm and 15-45º C, but it requires a powerful ignition source, such as a capacitive discharge igniter, due to the high energy needed for combustion initiation. The discussion highlights that kerosene and diesel fuel behave similarly in combustion, allowing for operation below stoichiometric ratios. Additionally, while liquid oxygen (LOX) can facilitate combustion in space, it does not make kerosene hypergolic. Effective ignition methods are critical for applications in gas turbine and rocket engines.
PREREQUISITES
- Understanding of combustion principles and stoichiometric ratios
- Familiarity with ignition systems, particularly capacitive discharge igniters
- Knowledge of kerosene and diesel fuel properties
- Basic concepts of gas turbine and rocket engine operation
NEXT STEPS
- Research the design and function of capacitive discharge igniters for kerosene engines
- Explore the combustion characteristics of kerosene in gas turbine engines
- Study the use of LOX in rocket propulsion systems and its ignition requirements
- Investigate the differences between hypergolic and non-hypergolic fuels
USEFUL FOR
Aerospace engineers, combustion researchers, and professionals involved in fuel technology and engine design will benefit from this discussion.