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Introduction to Life Cycle Cost Prof. Rajkumar S. Pant Aerospace Engineering Department IIT Bombay AE-332M / 714 Aircraft Design Capsule-4 Life Cycle Cost (LCC) Over the life cost Costs incurred from inception to disposal LCC


  1. Introduction to Life Cycle Cost Prof. Rajkumar S. Pant Aerospace Engineering Department IIT Bombay AE-332M / 714 Aircraft Design Capsule-4

  2. Life Cycle Cost (LCC)  Over the life cost  Costs incurred from inception to disposal  LCC components in Engg. Design  Design & Development  Production  Support Equipment & Initial Spares  Operation & Support (O&S)  Disposal AE-332M / 714 Aircraft Design Capsule-4

  3. Importance of LCC in Engg. Design  Reduction in system cost  Social requirements, inflation, economic recession, ..  Paradigm shift in Engg. Design ‘Performance at any cost’ ‘Design-to-cost’ ‘Design-to-LCC’  Helps in selection of competing solutions  Helps in identification of cost reduction areas  Most of LCC gets determined quite early AE-332M / 714 Aircraft Design Capsule-4

  4. Typical LCC breakup Modern Combat Aircraft Disposal RDT & E 1% 14% Operation & Support 50% Production Ground 30% Support Eqpt. & Initial Spares 5% Source: Woodford S, Recent Combat Aircraft Life Cycle Costing Developments within DERA, RTO AVT Specialists meeting on Design for Low Cost Operation and Support , Ottawa, Canada, October 1999. AE-332M / 714 Aircraft Design Capsule-4

  5. LCC Determination Phases Majority Of LCC Costs Are Determined Early I n Design AE-332M / 714 Aircraft Design Capsule-4

  6. Estimation of LCC components  Design & Development o CERs for factors, parameters and features that affect cost  Production o Mostly activity based costing • Tooling, Material, Fabrication, Assembly, QC, ……..  Support Equipment & Initial Spares o Can be reduced by careful design  Operation & Support (O&S) o Usually the largest component; models available  Disposal o Major issue of concern from environmental considerations AE-332M / 714 Aircraft Design Capsule-4

  7. Problems in Cost Estimation  Largely statistical  Based on actual costs of previous aircraft  Difficult to determine the actual cost  a/c procurement spread over many years  Non-optimal production rate; higher costs  Differences in Accounting procedure  Then-Year Rupees o Actual Money spent in each year of the program  Constant Year Rupees o Money spent ratioed by inflation to some specific year AE-332M / 714 Aircraft Design Capsule-4

  8. Then-Year v/s Constant Year Aircraft Then-Year (different years) Constant-Year (1978) F-15 USD 17.6 million USD 18.8 million F-16 USD 10.8 million USD 08.2 million % diff 60% 130% AE-332M / 714 Aircraft Design Capsule-4

  9. Production quantity & Rates a/c prodn. AE-332M / 714 Aircraft Design Capsule-4 Source: Aircraft Design: A Conceptual Approach, D R Raymer

  10. Example of Cost Over-runs  Light Combat Aircraft  Sanctioned in 1983 : Rs. 560 Crores  Amount spent till 2008: Rs. 5489.78 Crores  Two TDs and 3 Prototypes developed o Max. speed of Mach 1.4 achieved  IOC in 2010, FOC in 2012  IAF & IN wanted 220 a/c, Current Orders = 20  Kaveri Engine  Initial Sanction: Rs. 382 Crores  Expenditure till date: Rs. 2839 Crores AE-332M / 714 Aircraft Design Capsule-4

  11. A Cost Comparison Name Country Cost (Crore Rs.) F/A-22 Raptor USA 480 Rafale France 270 JAS-Gripen Sweden 160 Mirage 2000 France 130 LCA India 110 AE-332M / 714 Aircraft Design Capsule-4

  12. Aircraft LCC Estimation AE-332M / 714 Aircraft Design Capsule-4

  13. Aircraft LCC components Size of Boxes proportional to magnitude of costs AE-332M / 714 Aircraft Design Capsule-4

  14. Estimation of Research Development Test & Evaluation (RDT&E) Cost AE-332M / 714 Aircraft Design Capsule-4

  15. RDT&E Components  Technology Research  Design Engineering  Prototype Fabrication  Ground & Flight testing  Evaluation of Operational Suitability  Certification  Airworthiness  Mission Compliance  Design Documentation AE-332M / 714 Aircraft Design Capsule-4

  16. Cost Estimation Methods  Aircraft Cost (US $) =150-300* DCPR weight  DCPR = Defense Contractor’s Planning Report  W DCPR = Wt. of parts made by a/c manufacturer  Empty Weight – Weight of Bought Out items  Typical List of Bought Out Items: o Wheels, Brakes, Tires, Engines, Starter, Cooling Fluids, Instruments, Batteries, Power supplies, Fire-control systems, Air-conditioning systems, Avionics, Furnishings, APU,…  Two-main approaches  Activity Based o Detailed assessment of actual tasks, WBS creation  CER based o Formula based on DCPR weight, Max. speed, Production rate, …. AE-332M / 714 Aircraft Design Capsule-4

  17. CER based RDT&E Estimation  RAND DAPCA IV Model  Estimates hours required for RDT&E & Prodn. o Engineering, Tooling, Manufacturing, QC o Costs estimated by multiplying with MHRs  Other costs estimated directly o Development Support o Manufacturing Material o Flight Test  Additional Cost elements o Financing o Profit AE-332M / 714 Aircraft Design Capsule-4

  18. Engineering Hours  Effort Hours  Airframe Design & Analysis, Test Engineering  Configuration control, Systems Engineering  Support Hours  Propulsion and avionics system integration  Tooling & production Planning  Mainly during RDT&E, but also during prodn.  EE 500 = 3*EE 1 AE-332M / 714 Aircraft Design Capsule-4

  19. Tooling  Tooling Hours  Preparation for Production o Tools and Fixtures o Moulds and Dies o Programming of NC machines o Design & fabrication of production test apparatus  Tooling support during production AE-332M / 714 Aircraft Design Capsule-4

  20. Manufacturing & QC Labor  Manufacturing  Forming, Machining & Fastening  Sub assembly & Final assembly  Routing o Hydraulics, Pneumatics, Electrics  BO item installation o Engine, Avionics, Subsystems  Effort by Airframe subcontractors  Quality Control  Inspection at receiving, production, assembly  Tools, Fixtures, Components, sub-assemblies, Major assemblies, Final Assembly AE-332M / 714 Aircraft Design Capsule-4

  21. Development Support Costs  Mock Up  Structural test rigs  LG Drop test  System Integration test-Rigs  Iron Bird Simulators AE-332M / 714 Aircraft Design Capsule-4

  22. Iron Bird Simulator for F-728 AE-332M / 714 Aircraft Design Capsule-4

  23. CERs in DAPCA IV model AE-332M / 714 Aircraft Design Capsule-4

  24. Formula for RDT&E Cost AE-332M / 714 Aircraft Design Capsule-4

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