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Technical Review and Analysis of Ramjet/Scramjet Technology I. Ramjet Engine (Liquid Ramjet, Ducted Rocket)  

Sung Hong-Gye (한국항공대학교 항공우주 및 기계공학부)
Yoon Hyun-Gull (국방과학연구소)
Publication Information
Journal of the Korean Society of Propulsion Engineers / v.10, no.1, 2006 , pp. 72-86 More about this Journal
Abstract
A technical review of current ramjet propulsion is presented. In addition to summarize the current status of ramjet technology, new key techniques like Boosting technique easily adapting total impulse of booster, flame stabilization technique with minimized ramjet combuster length, variable nozzle-inner-surface technique realizing wide flight-envelop, and thermal protection technique for long operating time are identified. Actually various Ramjet propulsion technology has been matured and expanding to both military and combined cycle application. Yet many opportunities remain to be challenged by future generations of explorers to utilize s typical ramjet propulsion system for multi-purpose(multi-platform and multi-target) missiles, for example, American JSSCM and Russian Yakhont missiles, improving both reliability of techniques and downsizing development cost of new propulsion system.
Keywords
Ramjet; Ducted Rocket; High Speed Air-breathing Engine;
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