real world flight test projects at your usaf test pilot school
TRANSCRIPT
THE UNITED STATES AIR FORCE TEST PILOT SCHOOLSCIENTIA EST VIRTUS
“KNOWLEDGE IS POWER”
Colonel Noel “Shamu” Zamot
Commandant, USAF Test Pilot School
Real World Flight Test Projects at Your USAF Test
Pilot School
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Agenda
• What are Test Management Projects (TMPs)
• Highlights from the Past
• Current Projects
• Plans for the Future
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VISION:
World’s premiere school for applied
flight test engineering – where the world comes to educate future test leaders
MISSION:
Produce highly-adaptive, critical-thinking flight test professionals and future senior leaders to lead & conduct
full-spectrum test & evaluation of aerospace weapon systems
USAF TPS Vision & Mission
TPS Grads exert huge (often unseen) influence over weapon system development
LINE
AVIATORS
WEAPON SYSTEM
ACQUISITIONERSWAR-WINNING
CAPABILITIES
FLIGHT
TESTERS
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• 48-week Program, MSFTE
• 3 Curricula:– Experimental Test Pilot
– Experimental Test CSO/RPA Pilot
– Flight Test Engineer
• 4 Major Subdisciplines– Performance
– Flying Qualities
– Systems
– Test Management
• 13 Academic Courses = 50 sem-hrs total – 2500 Graduate hrs Average (+300 Ancillary Training hrs)
– 21 Scored Academic Exams 19 Individual Academic Exams
Comprehensive Written & Oral Exams
– 85 Flights (or Airborne Laboratories)
– 38 Graded Reports (31 written + 7 oral) Capstone Test Management Project (Report + Defense)
Curriculum
Performance:
X-47, KC-46, JSF, C-130J
Flying Qualities:
JSF, B-1 DFLCS, F-15E/F-16
Stores Cert
Systems:
F-22 Inc 3.1, B-1B FIDL,
INSR, B-2 EHF
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J F M A M J J A S O N D J F M A M J
TM 600 (4)TM 900 (9)
QE 900 (3)
PF 600 (3) FQ 600 (4)
SY 600 (3)FQ 700 (4)
FQ 800 (4)
FQ 900 (4)
PF 700 (3)
PF 800 (3)
SY 700 (3)
SY 800 (3) GR
AD
UA
TIO
N
AN
50
0/C
F 5
00
CU
RR
ICU
LU
M B
RE
AK
FIE
LD
TR
IP
TEST MANAGEMENT
QUAL-EVAL
SYSTEMS
FLYING
QUALITIESPERF
GR
AD
UA
TIO
N
CH
EC
KO
UT
CU
RR
ICU
LU
M B
RE
AK
FIE
LD
TR
IP
TMPTM 600 (4)
TM 900 (9)
QE 900 (3)
PF 600 (3) FQ 600 (4)
SY 600 (3)FQ 700 (4)
FQ 800 (4)
FQ 900 (4)
PF 700 (3)
PF 800 (3)
SY 700 (3)
SY 800 (3) GR
AD
UA
TIO
N
AN
50
0/C
F 5
00
CU
RR
ICU
LU
M B
RE
AK
FIE
LD
TR
IP
A - CLASS
B - CLASS
AN = Ancillary Training SY = Systems Subdiscipline
CF = Check Flights TM = Test Management Subdiscipline
PF = Performance Subdiscipline TMP = Test Management Project
FQ = Flying Qualities Subdiscipline QE = Qualitative-Evaluation Program
Phase / Course Layout
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THEORY
PLAN
FLY
REDUCE
DEDUCE
REPORT
TEAMWORK
= Full-Spectrum Flight Test Professional
Graduate Core Competencies
• Diverse Aerospace Vehicle Exposure
• Flight Test Engineering
• Flight Test Techniques
• Flight Test Planning
• Safety Planning & Risk Management
• Flight Test Execution
• Data Management
• Flight Test Evaluation
• Flight Test Reporting
• Integrated Test Teaming
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•What are TMPs?– End-to-End Staff/Student Real-World Flight Test Projects
– Conduct ~ 8 Projects/Year (4 in Spring, 4 in Fall)
– Peer-Reviewed, Published Written Report & Oral Defense
•Customer Provides:– Cutting edge research concept to be flight tested
– Funding for any specialized support or major acft mods
•TPS Provides:– Lots of Preliminary Planning and Preparation by Staff
– Test Aircraft - Usually flown on AFFTC Assets
– Dedicated Test Team of Pilots/Engineers (4-6 individuals)
– Flight Test Data, Data Reduction, Data Analysis
Test Management Projects
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• Statement of Capability
• Test Plan Working Groups
• Technical Review Board
• Safety Review Board
• Approval Brief
• Test Execution
• Data Reduction & Analysis
• Program Assessment Reviews
• Technical Information Memorandum
• Report Murder Board
• Final Presentation
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TMP Program Elements
REPORT
THEORY
PLAN
FLY
REDUCE
DEDUCE
TEAMWORK
Opportunity to apply
entire loop in a real
world exercise
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HIGHLIGHTS FROM THE PAST
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Successfully performed
Compatibility Flight Profile
testing to gain flight clearance
on F16 aircraft
Reconfigurable
Airborne Sensor,
Communications and
Laser (RASCAL) pod
Provides a platform for
testing avionics and
sensors without the cost
and schedule penalties
associated with
modifying aircraft
SENIOR RASCAL
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TALON SPOT
• TMP Objective:
Determine the optimal combination of aimpoint,
glideslope and throttle modulation method, from a
selection of landing techniques, to perform a safe and
repeatable T-38C approach and landing within AETC
requirements.
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NO GYRO
AFIT Dean’s Awd
#1 of 79 Aero/Astro Dept
AFIT Commandant’s Awd
#1 of 277+ all Depts
AIAA Awd
IoN Awd
1st ever for a Non-EE
7 Dec 2007
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Other Recent TMPs
• Pace Maker (F-16D) – Pitot-static system calibration
• Huron Six-D and Have Haste (C-12) – C-12
aerodynamic stability derivative estimation
• Icarus (NF-16D Vista) – Handling Qualities evaluation of
interaxis control coupling
• Shuttermatch (C-12) – Precision weapon guidance using
a coupled INS and a high resolution camera
• Have Fins (F-16) – Aim-9 control surface effects on F-16
LCO characteristics
• Have Gas (T-38 and Learjet) – Optical tracking
combined with differential GPS to simulate unmanned AR
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98B HAVE TRACK HUD Target as Substitute Aircraft Target for HQ Evals
00A HAVE OLOP PIO in the Presence of Rate Limiting
00B HAVE ATTITUDE Off-Axis Attitude Cueing for Helmet Mounted Sights
01A HAVE ROVER PIO Detection and Suppression
01B HAVE GRAPE Collect GPS TSPI data for follow-on TCAS testing
02A HAVE PREVENT Comparison of PIO Prevention Algorithms
02B HAVE SYCLOPS Flight Reference Displays
03A MAX GAP PIO Prediction Algorithms
03B SELF SERVE Autonomous Rendezvous for AAR
04A SOLO FORM Automatic Formation Flight
04B DOLLAR DRAFT Refine Positioning for Formation Cruise Drag Reduction
VISTA Projects: Students
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05B HAVE JIVE Voice Recognition System functionality at elevated-g
06A BAT DART Limit Investigation of Boundary Avoidance Tracking Tasks
08A AT BAT Limited Investigation of Auxiliary Tasking during BAT
09A HAVE MURDOC Multi-Use Rate Disturbance Observer Controller
09B ICARUS Limited HQ Eval of Interaxis Control Coupling
10B BEAR CLAW Basic Envelope Air Refueling Control Laws
VISTA Projects: Students
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2003 Auto Air Collision Avoidance Systems (Auto ACAS)
2004 Arc Segment Attitude Reference System, Heads Up Display
2006 Voice Recognition System
2006 Target Drone Mission (HAVE DEMO)
2008 F-16 Autoland System
2009 Advanced Vision Helmet System
In-work/Upcoming:
2012 Auto Air Collision Avoidance
2012 Automated Aerial Refueling Program
VISTA Projects: Staff
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CURRENT PROJECTS
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OBJECTIVE
Collect data to develop outer loop control
law design guidelines for the Variable
Stability In-Flight Simulator Aircraft (VISTA)
automated aerial refueling (AAR) with
KC-135 tanker
CONCEPT / CONDUCT
Characterize manned Air Refueling to
determine autonomous safety trips
IMPACT
AAR required for global RPA strike – VISTA
is designated test platform
CUSTOMER
•Automated Air Refueling Program,
AFRL/RBCCZ
• Fighter Risk Reduction Program, AFRL/RB
•RPA Surrogate Program, USAF TPS18
BEAR CLaw
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HAVE RAVEN
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OBJECTIVE
Determine the detection and track range of
small, low flying aircraft
CONCEPT / CONDUCT
•Various aircraft/sensors executing level
radar intercepts against small,
nontraditional targets
•Buildup to attempt detection of small
rotorcraft over mountainous terrain
IMPACT
•Improved capability to detect LO incursions
into CONUS
•First in a series of cooperative efforts
between TPS and external Government
Agencies
CUSTOMER
Department of Homeland Security
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HAVE MABLE
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OBJECTIVE
•Evaluate C-12J flying /handling qualities
with AN/ALQ-188v4 pod.
•Determine ECM POD performance
Differences between C-12J and AT-38B
CONCEPT / CONDUCT
•Qualitatively evaluate C-12J FQ/HQ with
AN-ALQ-188
•Fly C-12J and AT-38B with AN/ALQ-188 pod
versus APG-68 in IFAST and on F-16
IMPACT
Potential for significantly reduced cost,
timeline of testing ECM mission loads for
emerging threats
CUSTOMER
586th Flight Test Squadron, Holloman AFB
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HAVE RPA
OBJECTIVE
Evaluate the ability of the Calspan Learjet to
function as a surrogate Remotely Piloted
Aircraft (RPA) for future test utility
CONCEPT / CONDUCT
•Determine datalink performance, autopilot
response to Ground Control Station inputs,
observe and evaluate Pilot-Vehicle Interface
•Demonstrate remotely-piloted approach
IMPACT
•Demo autonomous landing control
•Ability to do cutting edge RPA testing
without airspace control issues
•Significant risk, cost reductions in
developing future RPA capability
CUSTOMER
AFMC/A3 21
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OBJECTIVE
Evaluate alternative pacer calibration
techniques
CONCEPT / CONDUCT
Compare results from the following
methods: atmospheric analysis, self-
survey, Orbis, cloverleaf, Beav, trailing
cone, tower flyby, level
acceleration/deceleration, and stabilized
cruise methods
IMPACT
A pacer aircraft is required to calibrate
the air data system of test aircraft (F-35,
F-22, KC-X)
CUSTOMER
Air Force Flight Test Center
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SPEED PACER
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OBJECTIVE
Compare the physiological response of
full coverage Anti-G Suits (Mustang and
Beaufort) to legacy g-suits
CONCEPT / CONDUCT
Test will collect physiological data on
pilot performance with each suit in high
g monitored centrifuge and flight
environments
IMPACT
Goal is to ultimately improve pilot
performance in a high-g environment
and reduce the number of GLOCs
CUSTOMER
•AFMC/A3 (initially)
•ACC, AETC, Foreign Allies (ultimately)
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HAVE PAIN
Mustang Survival
Advanced
Tactical Anti-G Suit
(ATAGS)
RFD Beaufort
Full Coverage Anti-G
Trouser (FCAGT)
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OBJECTIVE
Reconstruct the trajectory (position and
velocity) of an air-to-air missile (simulated by
aircraft) relative to a target (simulated by
sensors on ground)—vector scoring
CONCEPT / CONDUCT
•The vector scoring system will involve the
Lexus Doppler radar sensors mounted at
known ground locations
•C-12 will be flown over sensors at various
aspects and angles
•Sensors will then be moved and test repeated
IMPACT
Cost effective vector scoring system
CUSTOMER
Air Force Institute of Technology24
HAVE SPLASH
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HAVE HAL
OBJECTIVE
Evaluate enhancements to the Calspan
Learjet functioning as a surrogate
Remotely Piloted Aircraft (RPA)
CONCEPT / CONDUCT
Determine upgraded datalink
performance, autopilot (including
autothrottle) response to Ground Control
Station inputs, observe and evaluate Pilot-
Vehicle Interface improvements
IMPACT
•Improve ability to do cutting edge RPA
testing without airspace control issues
•Significant risk, cost reductions in
developing future RPA capability
CUSTOMER
AFMC/A325
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PLANS FOR THE FUTURE
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Future Directions for TMPs
• RPAs
• Airborne Networks
• Cyber Warfare
• Continued Work with AFRL
• Projects for RASCAL Pod
• Collaboration with New Folks
– NPS
– DHS
– DARPA
– Civilian Universities
• Design of Experiments &
Statistically Relevant Test
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Critical thinking flight test professionals need to have
hands-on experience with real world flight test
projects before wearing the TPS Grad Patch
TMPs provide the opportunity for small scope
advanced development projects that provide relevant
results to DoD customers
TMPs provide collaborative opportunities with other
Govt agencies, research centers, and universities
which help advance the state of the art in Flt Test
Bottom Line
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Backup Slides
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313131
Col
Noel ―Shamu‖ Zamot
Commandant
Mr. Dave Vanhoy
Technical Director
Lt Col
John ―Rider‖ Kanuch
Deputy Commandant
Lt Col (s)
Swami ―Shotgun‖ Iyer
Operations
DO
Maj
Clint ―Void‖ Armani*
Education
ED
Lt Col
Fred ―Steamer‖ Bivetto
Curriculum Standards
CS
Lt Col
Mike ―Slash‖ Young
Plans & Programs
XP
CDR
Mick ―Chum‖ Williams
Technical Support
TS
Master InstructorsPerformance Mr Russ Erb
Flying Qualities Vacant
Systems Mr Randy Kelly
Test Mgmt Ms Lyn McNeely
Manning Auth / AsgnAD Faculty 27 / 20 IMAs 11 / 8LTs 2 / 7Enlisted 5 / 4Civilian 24 / 22Contractor 24 / 24Matrixed 21 / 24Staff Total 114 / 109 Students 40 / 48School Total 144 / 157
USAF TPS Organization
MSgt Daniel Halverstadt
Superintendent
Mr. ―Evil‖ Bill Gray
Chief Test Pilot
Col
Dawn Dunlop
412 TW/CC
Brig Gen
Robert Nolan
AFFTC/CC
AFMC/A3
Brig Gen Bill Thornton
AETC/AU
Lt Gen Peck
Dr. Bruce Murphy
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REPORT
THEORY
PLAN
FLY
REDUCE
DEDUCE
Teach the way we Test… …Test the way we Teach
TEAMWORK
Learning ParadigmAn Applications-Oriented pedagogy
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Course (credits) Academic TopicsFlights, Sims &
ChecksReports
PF 600 (3)Fixed-Wing Aerodynamics
Intro to AerodynamicsCompressible AerodynamicsCruise
C-12 Mission directorAero ModelingCruise DataFighter Performance CheckGlider High L/DT-38 Low L/D
Aero Model Validation TLR
PF 700 (3)Performance Data Standardization
Pitot-Statics & Std AtmosphereData StandardizationModeling & SimulationPropulsion
Tower Fly-ByPacer / GPSPropulsion
Air Data Sys Calibration TLR
PF 800 (3)Performance Optimization
Takeoff & LandingEnergy Concepts
Level Accel / Sawtooth ClimbTurn PerformanceC-12 Practice CheckHU-16 Performance Final Check
Performance Oral PRRHU-16 Check Expanded 5314
Purpose • Basic Flight Test Methodology
• Learn Test Program conduct
• Motion of the aircraft C.G.
(e.g., “how far, how fast, how high…”)
Performance Subdiscipline9 sem-hrs 452 graduate hrs
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Course (credits) Academic TopicsFlights, Sims &
ChecksReports
FQ 600 (4)Unaugmented Airplane Motion
Equations of MotionTrim & StabilityParameter Estimation
C-12 Long-Stat & Lat-DirLJ-24 Long-Stat & Lat-DirT-38 Long-Stat & Lat-DirT-38 Dynamics
T-38 Long-Stat 5314T-38 Long-Stat TRT-38 Lat-Dir 5314T-38 Lat-Dir TR
FQ 700 (4)Flight Control System(FCS) Testing
Intro to FCSAnalog & Digital FCSAero-Servo-ElasticityCriteria for FCS DesignFreq Content, Aliasing, FiltersFreq Response EstimationRedundancy Mgmt SystemsFCS Ground TestingFlight Test Simulators
FQ & HQ SimulatorsVISTA HQ DemoLJ-24 FCS Project
VISTA HQ 5314
FQ 800 (4)Stall, Departure, Spin,& Failure State Testing
Stall-Departure-Spin TestingFailure State Testing
Glider SpinT-38 Stall & HQC-12 & KC-135 Eng-OutF-16 Departure
T-38 HQ/Stall 5314T-38 HQ/Stall Oral PRREng-Out Expanded 5314F-16 Departure Oral PRR
FQ 900 (4)Handling Qualities (HQ)& Envelope Expansion
FQ Testing Config & OverviewTaxi testingFirst-Flight FQ TestingHandling Qualities EvaluationOne-Flight FQ EvaluationStores CertificationStructures
F-16 limit Cycle OscillationKC-135 & Glider FQC-12 First-Flight CheckF-16 HQF-15 CFP & Asymmetric StoresAT-38 FQ CheckF-16 Structural Loads Check
Purpose • Evaluate aircraft flying qualities
• Aero & Flight Control System models
• Motion of aircraft about its C.G.
Flying Qualities Subdiscipline16 sem-hrs 815 graduate hrs
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Course (credits) Academic TopicsFlights, Labs, Sims &
ChecksReports
SY 600 (3)Human Factors& Avionics
Human FactorsIntegrated Navigation SystemsCommunications & Data LinksAvionics Systems IntegrationUnmanned Aircraft Systems
ASI Lab (IFAST)F-15E Systems Eval
Cockpit Eval Expanded 5314AMC Sims 5314
SY 700 (3)Airborne Sensors
Electro-Optics/Infrared SystemsRadar Systems
EO Lab (TPS & IFAST)F-16 EO DemoRadar Lab (TPS & IFAST)Air to Air Radar Lab (TPS)ASTARS Day/Night Sensor Eval
F-16C/D EO Expanded 5314ASTARS Expanded 5314
SY 800 (3)Weapons & IntegratedSystems Evaluation (ISE)
Electronic WarfareWeapons Delivery TestingF-16 Weapons DeliveryF-16C/D A/G Weapons DeliverySmart Weapons A/ASmart Weapons A/GWeapons & Tactics Overview
Elec Combat Gnd/Flight Test LabsT-38 ALQ Pod vs IFASTF-16C/D Wpns Delivery IFAST SimF-16C/D Weapons DeliveryT-38C ISE Check & Target
F-16 Wpn Del Expanded 5314T-38C Sys Eval Check Oral PRR
Purpose • Evaluate Aircraft Systems
Performance Suitability
Human Factors
Pilot Vehicle Interface
• Exposure to wide variety of Systems
Systems Subdiscipline9 sem-hrs 478 graduate hrs
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Course (credits) Academic TopicsFlights, Sims &
ChecksReports
TM 600 (4)Test Planning& reporting
Probability & StatisticsTest ConductTest InstrumentationIntermediate T&E (TST-202)Test ManagementUnit Test Safety Officer (UTSO)Modification PlanningDesign of ExperimentsAll-Weather TestingDeficiency Reporting
TM 900 (9)Test Management Project& Comprehensive Exams
Comprehensive Written ExamComprehensive Oral Exam
TMP Data Flights Test Concept LetterTest PlanProgram Assessment Review #1Program Assessment Review #2Technical Info MemorandumFinal Oral PRR
Purpose • Spans Entire Curriculum
• Test Mgt / Sys Acquisition Process
• Reporting in Multiple Formats
• Capstone Test Management Project
Test Management Subdiscipline13 sem-hrs 635 graduate hrs
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NF-16D VISTA
Airborne Laboratories
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• Variable-Stability In-Flight Simulator Test Aircraft
• Rapidly reconfigurable H/W & S/W
• Capable of hi-fi sim of aircraft “model” in real flight environment
FQ700 Flight Control Systems Testing
Includes two flights to demonstrate & practice test
techniques in a variable stability aircraft to examine the
effects of differing flight control systems
TM 900 Test Management Project & Comp Exam
VISTA support provides cutting-edge research capability for
test management projects
What is VISTA?
A unique national asset…sets TPS apart!
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RASCAL:
Reconfigurable
Airborne
Sensor
Comm
And
Laser Pod
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RASCAL CONOPS
• Long Term Plan to Support TPS TMPs
– Especially Tailored to AFIT/TPS Joint TMPs
– May be transported for lab engineering
• ―PODular‖
– Fleet of 4 Pods
– NO specific A/C Mods Required
– Initial flight certification on AFFTC F-16C/D
– Any Fleet Support F-16 or T-38B A/C
– F-15/A-10/Other Certification Later if Desired
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Telemetry Station• 2 IADS control rooms
• UHF/VHF comm
• 2 directional, 2 omni antennas
• Real Time PCM/TM recording
• L/S/C-Band Capable
• 125 control room missions / yr
• ILIAD Data Reduction Software
Control Rooms
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Control Rooms
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Pilot in-the-loop Sim
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Philosophy
• TPS Teaches Discipline and Philosophy of Flight Test– Basic concepts and processes– Not how to conduct every possible test
• TPS Produces Well Rounded Test Professionals– Highly adaptive and critical thinking– Can apply flight test process to new programs and
situations– Grads won’t know all the answers – They will know
where and how to find them
• Pursue innovative ways to advance curriculum
– Collaboration with New Partners
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Bottom Line Up Front
TPS grads are:
The cream of the crop of the operational world – we
take the best and make them better, educating
them in Test, Evaluation and Acquisition
A potential Cost Savings – TPS grads can test
weapon systems with minimal external
assistance/support
With the correct deliberate development, potential
future leaders in our Air Force: PEOs, Sq/Gp/Wg
Commanders, Materiel Leaders and more
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What do our grads really do?
Given minimal resources,
Lead highly skilled personnel in flat organizations
through complex efforts. . .
Communicate arcane technical concepts clearly
and cogently to decision makers. . .
In order to extract truth from chaos.
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