Atomization Characteristics of Liquid Propellant with Hypergolic Ignition
نویسندگان
چکیده
منابع مشابه
آتشزنه‌ها در سیستم‌های پیشرانش مایع غیرخود مشتعل شونده
Liquid propulsion systems have effective role in implementation of space and military mission due to high performance and specific impulse. Liquid propellants are divided into two categories: hypergolic and non-hypergolic propellants. Non-hypergolic propellants need an igniter system to provide the initial energy for propellant ignition compared with hypergolic propellants. Since failure in ign...
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ژورنال
عنوان ژورنال: Journal of High Temperature Society
سال: 2005
ISSN: 0387-1096
DOI: 10.7791/jhts.31.63