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V-22 Osprey First Flight on Unpaved Surfaces. SETP Safety Symposium Vienna Austria Nov 10-12, 2009. PURPOSE OF TEST. V-22 Landing Gear: Previous EMD testing only done between 5-20 knots on “benign” surface No Testing outside of paved surfaces. Small nose gear capabilities unknown. - PowerPoint PPT Presentation
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V-22 Osprey First V-22 Osprey First Flight on Unpaved Flight on Unpaved
SurfacesSurfaces
V-22 Osprey First V-22 Osprey First Flight on Unpaved Flight on Unpaved
SurfacesSurfaces
PURPOSE OF TESTPURPOSE OF TESTV-22 Landing Gear:V-22 Landing Gear:
Previous EMD testing Previous EMD testing only done between 5-20 only done between 5-20 knots on “benign” knots on “benign” surfacesurface
No Testing outside of No Testing outside of paved surfaces. paved surfaces.
Small nose gear Small nose gear capabilities unknown.capabilities unknown.
User (USMC / AFSOC) User (USMC / AFSOC) desire as much desire as much capability as possible. capability as possible.
Tiltrotor has unique Tiltrotor has unique capabilities that result capabilities that result in a large scope of tests.in a large scope of tests.
DefinitionsDefinitionsSemi prepared Semi prepared runway runway operationsoperations
Landing Landing zones/areas zones/areas where fixed wing where fixed wing aviation aviation operations are operations are intendedintended
Grass stripsGrass strips
Unpaved/gravel/Unpaved/gravel/dirt runwaysdirt runways
DefinitionsDefinitionsUn-prepared Un-prepared field operationsfield operations
Landing zones Landing zones not intended for not intended for fixed wing ops fixed wing ops but may be but may be suitable for a suitable for a smaller envelopesmaller envelope
Athletic fieldsAthletic fields
Agricultural areasAgricultural areas
Cleared LZs/DZsCleared LZs/DZs
DefinitionsDefinitionsSTOLSTOL
Short Take Off and Short Take Off and LandingLanding
6060˚̊ or 75 or 75˚̊ Nacelle Nacelle9090˚̊ Helicopter Mode Helicopter Mode
6060˚̊ for Heavy GW for Heavy GW
7575˚̊ for Tactical Mid GW for Tactical Mid GW
Can increase take off Can increase take off capability by up to capability by up to 5000 lbs5000 lbs
Test MethodologyTest MethodologyFixed Step Obstacle TestFixed Step Obstacle Test
Grass Field TestingGrass Field TestingTaxi/STO/ROLTaxi/STO/ROL46K, 49.5K, 52.6K46K, 49.5K, 52.6K
Semi-prepared Field Semi-prepared Field Testing (CBR 20+)Testing (CBR 20+)
Taxi/STO/ROLTaxi/STO/ROL46K, 52.6K, 57K46K, 52.6K, 57K
““Un-prepared” Field Un-prepared” Field Testing (CBR 7.5-20)Testing (CBR 7.5-20)
Taxi/STO/ROLTaxi/STO/ROL46K, 49.5K, 52.6K46K, 49.5K, 52.6K
Identify RisksIdentify RisksStructural FailureStructural Failure
Excessive LoadsExcessive LoadsAirfield not to Airfield not to specified valuesspecified values
Loss of Situational Loss of Situational AwarenessAwareness
Brown out / DUCEBrown out / DUCE
Loss of Directional Loss of Directional ControlControl
Hard LandingHard Landing
FODFOD
Blown TiresBlown Tires
Risk MitigationRisk MitigationBuild up Build up
Gross WeightGross Weight
Ground Speed Ground Speed Brown out Brown out considerationsconsiderations
Build downBuild downCBRCBR
Higher CBR = “harder Higher CBR = “harder field” (CBR 20+)field” (CBR 20+)
Lower CBR = “softer Lower CBR = “softer field” (CBR 7.5 – 20)field” (CBR 7.5 – 20)
Test PreparationTest PreparationPre-test TrainingPre-test Training
Engineer training with Engineer training with MAWTS-1 AGSMAWTS-1 AGS
DCP trainingDCP trainingAirfield assessmentAirfield assessment
US Army Engineering US Army Engineering Research and Research and Development CenterDevelopment Center
Test plan reviewTest plan reviewSite survey DCP data reviewSite survey DCP data reviewComputer Computer analysis/predictions/model analysis/predictions/model correlationcorrelation
Test PreparationTest PreparationC-17 SPRO TestingC-17 SPRO Testing
Engine FOD damage Engine FOD damage due to reverse thrustdue to reverse thrustLG damage due to LG damage due to short landingshort landingRunway deterioration Runway deterioration due to max brakingdue to max brakingAvionic fans dust Avionic fans dust ingestioningestion
Testing on going at Testing on going at multiple off-sites to multiple off-sites to evaluate multiple evaluate multiple surface surface types/conditionstypes/conditions
Test PreparationTest PreparationC-130J TestingC-130J Testing
Similar to C-17 Similar to C-17 LLLL
Erosion of Erosion of underside of AC underside of AC and antennasand antennas
FOD APU/EnginesFOD APU/Engines
Brown out on Brown out on decelerationdeceleration
Runway Runway deteriorationdeterioration
Test PreparationTest PreparationMV-22 Austere Ops MV-22 Austere Ops TestingTesting
VTOL landings in VTOL landings in DUCEDUCE
Maintenance IssuesMaintenance Issues
FODFOD
AVIONICS FILTERSAVIONICS FILTERS
GEAR BOX TEMPSGEAR BOX TEMPS
POST FLIGHT POST FLIGHT REQUIREMENTSREQUIREMENTS
Fixed Step Bump Fixed Step Bump TestingTesting
AM-2 MattingAM-2 MattingShimmed to 2” and Shimmed to 2” and 4”4”
Anchored to runwayAnchored to runway
GW 46K, 52.6K & GW 46K, 52.6K & 57K57K
GS 10-70 (+/- 5 KGS)GS 10-70 (+/- 5 KGS)
1600-2400 ft 1600-2400 ft remaining after remaining after bumpbump
Fixed Step Bump Fixed Step Bump TestingTesting
07FA04 NLG DSRA Load vs Ground Speed
-40,000
-30,000
-20,000
-10,000
0
10,000
20,000
30,000
40,000
0 10 20 30 40 50 60
Ground Speed (kts)
07F
A0
4 N
LG
DS
RA
Lo
ad (
lb)
46k lbs GW 2"53k lbs GW 2"57k lbs GW 2"46k lbs GW 1.5"53k lbs GW 1.5" Flt 91053k lbs GW 1.5" Flt 91153k lbs GW 1.5" Flt 91257k lbs GW 1.5"53k lbs GW 1.5" Flt 914Tension AlertComp Alert
25 to 35 knots required 25 to 35 knots required to touchdown with no to touchdown with no brown outbrown out
Semi Prepared Semi Prepared Austere EvalAustere Eval
Minimum Landing Speed
20
25
30
35
40
45 47 49 51 53 55 57 59
Gross Weight (1000 lbs.)
Gro
und
Spee
d (k
nots
)
Semi-Prepared LZSemi-Prepared LZ
High CBR 25-100High CBR 25-100
Very low loads on all Very low loads on all structural structural componentscomponents
Airfield Post Airfield Post Collapse SurveyCollapse Survey
NLG Collapse Local Survey
1M
4M
13M
5M
2M
11M
6M
7M
12M 9M8M 10M
11 CBR
60 CBR
4”
20”
8 CBR
37 CBR
4”
20”
12 CBR
50 CBR
4”
20”
6 CBR
15 CBR
4”
20”
10 CBR
15 CBR
4”
20”
9 CBR
12 CBR
4”
20”
10 CBR
20 CBR
4”
20”
6.5 CBR
15 CBR
4”
20”
7 CBR
20 CBR
4”
20”6 CBR
28 CBR
4”
20”
7 CBR
50 CBR
4”
20”
6 CBR
55 CBR
4”
20”
WIT
HIN
LIM
ITS
BE
LO
W M
IN L
IMIT
S
CB
R IN
AC
CU
RA
TE
Lessons LearnedLessons LearnedUnprepared surfaces Unprepared surfaces have features that are have features that are not identifiable by not identifiable by standard surveysstandard surveys
Flight test requires very Flight test requires very specific conditionsspecific conditions
Onsite subject matter Onsite subject matter experts can be valuableexperts can be valuable
Full scale structures tests Full scale structures tests (load cart with landing (load cart with landing gear) in controlled gear) in controlled environments can reduce environments can reduce problems down the roadproblems down the road
Despite all the planning Despite all the planning in world, Flight Test is in world, Flight Test is Unpredictable and Risky!!Unpredictable and Risky!!