This paper describes the systems methodology created to exploit in-service aircraft experience to influence the design of a new landing gear system. The paper opens with an overview of systems requirements, evolution of the design loop, followed by the tools and techniques developed to ensure early product maturity at Entry Into Service (EIS).
Members-Only Content
This content is restricted to members only.
You must be logged in with an active membership to access this page.
Please click the link below to log in. If you do not have an account or your membership is inactive, you may need to register or renew it.