1978-02-01

Applying Design-To-Life Cycle Cost Methods During Engine Advanced Development 781030

In order to make better decisions during advanced development of turbine engines, life cycle cost (LCC) methodologies must adequately reflect the impact of engine design decisions on the total system LCC. Two applications of Teledyne CAE's APSICOST Methodology are presented herein. These demonstrate the integrated nature of turbine engine LCC analyses with total aircraft system LCC.
It is recommended that a joint airframe/propulsion/government effort be undertaken to standardize methods for reflecting aircraft system LCC impacts in turbine engine advanced development activities.

SAE MOBILUS

Subscribers can view annotate, and download all of SAE's content. Learn More »

Access SAE MOBILUS »

Members save up to 18% off list price.
Login to see discount.
Special Offer: Download multiple Technical Papers each year? TechSelect is a cost-effective subscription option to select and download 12-100 full-text Technical Papers per year. Find more information here.
We also recommend:
TECHNICAL PAPER

NASA / SATS Life Cycle Cost Model

2000-01-1690

View Details

TECHNICAL PAPER

Improved Maintenance Practices-The Airlines' Contribution to Lower Ownership Costs

760504

View Details

TECHNICAL PAPER

The Aircraft Tire Wear Problem

951391

View Details

X