A Study on the Trade-off Analysis of Combat Weight for Conceptual design of a Landing Craft Air Cushion

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Journal of the Korea Institute of Military Science and Technology 2000;3(1):66-75.

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공기부양상륙정의 개념설계를 위한 전투중량 대안분석 연구

이제동, 신용석

¹해군 제1함대
²군사과학대학원 무기공학과

Abstract

The purpose of this study is to develop and illustrate methods of applying trade-off techniques to landing craft air cushion design evaluation. The problem areas of concern are the application of quantitative analytical methods to conceptual design. The interrelationships between composite system measures and selected performance requirements(speed, cruising range, cargo etc.) are analyzed and the expressions for gross weight are developed as functions of performance parameters. Trade-offs of performance parameters in terms of weight are then calculated. The application of these results to evaluation of Require Operational Capabilities are illustrated.

Key Words: Landing Craft Air Cushion, Trade-Off Techniques, Require Operational Capabilities