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Military Jet Engine Acquisition Technology Basics and Cost-Estimating Methodology

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Military Jet Engine Acquisition Technology Basics and Cost-Estimating Methodology ( military-jet-engine-acquisition-technology-basics-and-cost-e )

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136 Military Jet Engine Acquisition these increased system demands. In addition, in many instances, even though tools with greater capability are available, their use is curtailed by limited computing capacity or delayed due to the effort (and funding) required to develop them fully for use in a specific application. When more-capable tools are fully applied, they allow an engineer to perform many design iterations to reach the “optimal” solution. However, this solution is not produced with a reduced number of engineering hours, but it does come during the development stage rather than post development. Thus, advanced modeling and simu- lation tools allow designers to identify and correct technical prob- lems early, thereby avoiding some potentially costly hardware fail- ures either during the test program or in the field. In addition, better predictive tools provide more accurate forecasts of future operational performance. These improved predictions should allow for more accurate maintenance planning and cost savings in the operation and support phase of the engine life cycle. Development costs are not likely to decrease due to advanced tools and technologies. Rather, the payoff is in systems that are significantly more capable and more reliable with comparable development costs and a compa- rable development schedule. System performance requirements will continue to escalate as mili- tary requirements become more demanding and new or emerging technologies becomes available. The U.S. armed forces will always demand that their weapon systems continue to outperform the sys- tems of their adversaries, both tactically and logistically. Turbofan engine technology faces numerous challenges that may alter how development programs are conducted in the future. For example, in- creased stealth/LO requirements imposed on an engine/propulsion system could result in the use of more-exotic materials and coatings and more-complex inlet and exhaust designs. More-stringent noise and emissions standards will impact the complexity of the design and could require additional design and test time. The integration of flight and propulsion controls also could dictate system complexity and require additional design and test time. The prudent develop- ment and application of advanced technology will play a critical role in meeting these challenges and affordably maintaining the U.S. military’s tactical advantage.

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