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Aerospace Information Report 1939 Trial Application
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English
Abstract
The proposed AIR 1939, “Aircraft Engine Life Cycle Cost Guide,” states the need for a methodology capable of relating input and output data on a consistent basis. This paper demonstrates that a methodology consistent with the proposed guidelines of AIR 1939 is practical. A generic example was constructed based on the design-to-cost/life cycle cost (DTC/LCC) requirements for an Allison engine full-scale development program. The example is presented using concepts and terminology from AIR 1939 in order to demonstrate the applicability of the document.
Citation
Curry, C. and Carpenter, M., "Aerospace Information Report 1939 Trial Application," SAE Technical Paper 861787, 1986, https://doi.org/10.4271/861787.Also In
References
- “Aircraft Engine Life Cycle Cost Guide,” SAE
- “Aircraft Operating and Support Cost Development Guide,” Office of the Secretary of Defense (OSD), Cost Analysis Improvement Group (CAIG)
- Curry C. E. “Engine Life Cycle Cost Modeling in the Conceptual Phase,” AIAA Paper 75-1288 AIAA/SAE 11th Propulsion Conference Anaheim, CA September--October 1975
- MIL-STD 1388-1A Logistics Support Analysis
- MIL-STD 1388-2A Logistics Support Analysis Record
- Curry C. E. “Military Aircraft Engine Life Cycle Cost From a Commercial View,” proceedings of OSD Aircraft Engine Design and Life Cycle Cost Seminar NADC Warminster, PA May 1978