The Future of Ground Testing

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Air Force Materiel Command Developing, Fielding, and Sustaining America’s Aerospace Force I n t e g r i t y - S e r v i c e - E x c e l l e n c e The Future of Ground Testing Dr. Ed Kraft AEDC/CZ Presented at the AIAA Ground Test Conference June 29, 2010

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The Future of Ground Testing. Dr. Ed Kraft AEDC/CZ Presented at the AIAA Ground Test Conference June 29, 2010. Key Points. The Nation’s test infrastructure is under serious distress - time to change the dialogue from reactive to proactive Need to quantify, articulate and improve - PowerPoint PPT Presentation

Transcript of The Future of Ground Testing

Page 1: The Future of Ground Testing

Air Force Materiel Command

Developing, Fielding, and Sustaining America’s Aerospace Force

I n t e g r i t y - S e r v i c e - E x c e l l e n c e

The Future of Ground Testing

Dr. Ed KraftAEDC/CZ

Presented at the AIAA Ground Test Conference

June 29, 2010

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Key Points

• The Nation’s test infrastructure is under serious distress - time to change the dialogue from reactive to proactive

• Need to quantify, articulate and improve– Effectiveness– Relevance– Value

• People and processes may be more important than facilities for increasing effectiveness and value

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Current State of Affairs

• Cause and effect not understood

• Minor wounds could lead to serious consequences

• Amputation primary form of surgery

• Not a very high survival rate

Analogous to Early Civil War Medicine

We need to better quantify cause and effect of test capabilities on aeronautical system development

outcomes

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Efficiency vs Effectiveness

Contractor System T&E Cost (Average $795.6M in FY 2001 $)*

*Fox et al “Test and Evaluation Costs for Aircraft and Guided Weapons” Rand Project Air Force Report., 2004

+ GAO-05-301, Assessment of Selected Major Weapon Programs, March 2005

RDT&EOverrun

EquivalentAircraft

F/A-22 $10.5B -116

F-35 $10.1B -157.8

GAO Program Reviews+

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Acquisition Cycle Time Key T&E Effectiveness Parameter

• Workload – Process driven, currently ~22,000 of wind tunnel testing and 13,000 of propulsion cell testing

• q (inverse of rework) – Process driven, typically have 10 structural failures found in flight; control surface resizing

• Capacity – Budget driven, availability x staffing x throughput

Cycle Time ~ Workloadq · Capacity

50% reduction in wind tunnel costs equates to just a few tenths of a percent reduction in program costs –Reducing acquisition cycle time by a month could save more than the cost of the entire wind tunnel campaign

Kraft, Edward M. “ Integrating Computational Science and Engineering with Testing to Re-engineer the Aeronautical Development Process,” AIAA Paper 2010-0139 , January, 2010.

Kraft, Edward M. and Huber, Arthur F II “A Vision for the Future of Aeronautical Ground Testing,” The ITEA Journal of Test and Evaluation, Vol 30, No 2, June 2009.

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Identifying ValueMeasures of Effectiveness and Key Leverage Points in the

Acquisition Process

0

20

40

60

80

100

0 20 40 60 80 100

% Design Drawings Completed at CDR

% G

row

th in

Dev

elop

men

t Sc

hedu

le

Technology Maturity @ Milestone B

Design Closure@ CDR

Late DefectsIOT&EPause TestRate

CycleTime

RDT&E$/Total $ AverageFleet Age

SystemsDelivered

Suitability

RDT&E Fraction is revealing metric

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Top Line Economic ModelQuantifying the Fraction of Systems Delivered

Fraction of Systems Delivered

Frac

tion

of B

udge

t

RDT&E“Non-Recurring Cost”

Procurement“Recurring Cost”RDT&E

Overrun

Fraction ofSystemsLost toRDT&EOverrun

0 1

RDT&EBudget

1

Final number of systems actually delivered driven by:

•Overruns in RDT&E•Changes in the average per unit cost (APUC) during production

•Congressional or DoD dictates•Final Budget constraints

Fraction of SystemsActually Delivered

RDT&E Budget fraction amplifies the RDT&E and Procurement overruns plus Budget changes!

ProcOverrun

APUC

Fraction ofSystemsActually

Delivered

= 1-RDT&EOverrun

RDT&EBudget

1 -

ProcOverrun

+ -+ DeltaBudget

Budget +

Budget -

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Comparing RDT&E and Procurement Costs to RDT&E Fraction

DoD Total Outlay for Improvements(FY08 $, Millions)

0

0.1

0.2

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1950 1960 1970 1980 1990 2000 20100

20000

40000

60000

80000

100000

120000

140000

RDT&E

Procurement0.5

0.4

0.3

0.2

0.1

0

RDT&EFraction

Note: Discreet jumps in RDT&E Fraction are triggered by Procurement downturns, but sustained by relative increase in RDT&E for each Period

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Correlating Time History of Decline in Capacity, Capability, and Competence

• Industry consolidation – Reduced capability, investments– Reduced IR&D– Loss of intellectual capital

• RDT&E infrastructure– Reduced investments– Staff reductions

• Loss of intellectual capital– Reduced staffs– Loss of govt expertise through

reductions in hands on experience, staffing,TSPR, etc

• Loss of capacity– Availability of infrastructure– Staffing to perform RDT&E– Throughput/Quality

All correlate with Macro Cycles and have become deeper declines with each cycle

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Reduced Aerospace Capacity

1.0

0.5

0

Frac

tion

of P

eak

Out

put

70 80 90 00 10

IR&D % Industry Cash Flow (22%)

% Aerospace to Total R&D S&E (25%)

US Aircraft Companies (10)

Aircraft Production Lines (30)

MRTFB Workyears (40K)

AEDC Workyears (4K)

Trend Parameter (Peak Output)

Capacity Trend Data from Multiple Elements of the Aerospace Industry Supportive of RDT&E

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Exploring Cause and Effect Simple Dynamic Model

•Simple sinusoidal Proc $ with 20 yr period , $90B±$30B

•Baseline RDT&E $ expended at 0.25 Acq $

•With perfectly balanced, infinitely elastic capacity RDT&E $ would stay at 0.25 Acquisition $

•Reduced capacity consistent with previous chart

•-15% in 70’s, •constant in 80’s @ 85%, •further reduced 25%in 90’s •constant in 00’s @ 60%

•Replicates major trends, Total RDT&E $ and RDT&E Fraction escalate after each cycle

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• Quantify effectiveness and value– Send me any data / case studies supportive of analysis– Build white papers targeted at key decision makers*

• Optimize total investments in capabilities– Optimum local elements ≠ optimum system – Use policy for Major Range Test Facility Base*

• Build, validate, and apply tools to increase effectiveness– Integrate computational science and engineering*, fly the mission

testing*, DOE response surface methodology to reduce cycle time and late defects

• Invest in technical excellence– Train in DOE, CSE, integrated T&E*– Fund hands-on approaches to learn craft*– Maintain a community with critical mass

• Change the total development process– Target success at leverage points– Reduce cycle time by >50%

SummaryNow What Do We Need to Do?

Challenge

Can the TC Lead This ?

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Additional Information

• Contact [email protected]

• Additional Reading– Kraft, Edward M. “ Integrating Computational Science and Engineering with Testing to

Re-engineer the Aeronautical Development Process,” AIAA Paper 2010-0139 , January, 2010.

– Kraft, Edward M. “After 40 Years Why Hasn’t the Computer Replaced the Wind Tunnel?” The ITEA Journal of Test and Evaluation, September 2010

– Kraft, Edward M. “DOE Application to Ground Testing – Advances and Challenges” Invited Panel Presentation at the AIAA Air Force T&E Days Conference, Nashville, TN, Feb 3, 2010.

– Kraft, Edward M. “Macro-Dynamics of Acquisition,” Draft White Paper available on request

– Kraft, Edward M. and Huber, Arthur F II “A Vision for the Future of Aeronautical Ground Testing,” The ITEA Journal of Test and Evaluation, Vol 30, No 2, June 2009.

– Huber, Arthur F II, Kraft, Edward M,, Best, John T., Stich, Phillip B., Eldridge, David A., Baker, William B., and Montgomery, Peter A. “Growing Technical Excellence in the AEDC Workforce.” AIAA Paper 2009-1762, February 2009.

– Best, John, T., Kraft, Edward M., and Huber, Col Arthur F. “Revitalizing the Technical Excellence at the Arnold Engineering Development Center (AEDC) and Beyond,” AIAA 2008-16115-7, Feb 2008.