.ME - NASA · - Crane hooks - Liftingfixtures ... ll-AxisRobot and gantry Structural Health...
Transcript of .ME - NASA · - Crane hooks - Liftingfixtures ... ll-AxisRobot and gantry Structural Health...
.ME_KSC ENGINEERINGAND TECHNOLOGY
-----------------------
•
•
Spacecraft Pre-launch/Turnaround NDE needs at theKennedy Space Center
Rick Russell
NASA Materials Science Division
In~Space Non-Destructive Inspection Technology Workshop
March 1, 2012
Houston, TX
https://ntrs.nasa.gov/search.jsp?R=20120003446 2018-06-24T05:32:11+00:00Z
NASA RoadmapsKSC ENGINEERING~ANO TECHNOLOGY
NDE included •In
Sp~ce Technology Roadmaps STR • TABSTECHNOLOGY AREA BREAKDOWN STRUCTURE
••
•
CROSS-CUmNGNonde trucci....e Evaluation r Sensors~1odd-BascdCertification &Sustainment MethodLoad and En....."ironmcnts
A12 ·MATERIALS, STRUCTURES, ECHANICAl
SYSTEMS & MANUFACTURING
Table 22. WBS # 2.5.1 NDETECHNOLOGY PRODUCT Wh.'11 tn.bl.., (unoi'll TRll'Slat us Slop, I. TRl611:0' Tochnolog1'Ch.llongo•
.. NOl(.~.,.~~~S4rvct.... "'URl_ of t!l~ int.!rityof TlI.2.Vi.bl.lIKlnt""., for ~nso" for progno,tic, .ndS......." ..nd DE d09<5forhig>- ClOmp!=< builMlp st,uclur.,. inlpe:tion of "',rn'N .ulf.c.. recon,truclO,"t.dtn~,forfidelily ~1ion ....d e:ten<""i....on Of .nd inspee1ion Ib"';"!l di.." d.u .c""i...t frem limlt.d.,;.,.....ft_, ..nd d.gndetion in ClOmpeo< built-up ,.,..bly. of pene1rllling mcIietion l')1 1.structures.
~. cOIPlpVUll..".r NOl lloI>id d..-el"""",nt .nd oenmc.· TA.2-1.Ultr.,onic ,;mul.'ion, 10, V.lid.t.d ';mul.,on, of uh...•Predict1h. p..fonn.n<>e of HOI; *hri'l"~ tion of inopection ttchnique, ",. homor:ou.lT'IMIeri&l"'; It> incl... :::~=~ri:'~2oirsitton criticil slruc1ureoJmneri.l.. ClOmp!=< ClOmpo,ite configurl' ,ion 0 ';mpln.dn.......
tions.
c. ( ......." ... MDei 'M Stnoct_l AMlysl. Acxuntt "',• ......- <:J 1he TA. 1-2. M.n....1inclusion of Accuftte' resid....llift: precieticnsI""u,ion <:J .ccurneell_".,;......, <:J inlpoct of <10m.... on ,truclur.1 HOE data in.. S1nKlur.I .n'''',i, :;-~02'['9dol...cqui..dfromdlm.ge in ~ctvnl.,.fysis rou .ne-s.. inlegfily. rouunes.
d. A_o_","",o"_ Perfonnanoe of ;n5peoctDn. in TA. '·2. O......Io~rneftt of ,ystenl. ~so" .nd Al1'te..... for l.r90St_r .ndAutonomou.lnspecIion lAO co.... I~as ~re _ h""..., ;'te.raetion wi." simptiMd uman oper~ are- in~ection 02).1",1~.. lkot~n......t~perfo"".nc• j••ith.. n~po,,;bl.. c~"""9" t"ns..• ndop'min1ionofN ~m."';thoutl Ing..Of too time ccnn'"t1ng.t-.Jm'" imeraction.
o. 1l0.1-tllfto CO"'l"fo"_", Dt&<Jft0sUa Inllegrily .'....r.n<>e <:J ...n;d~, for TlI. H. I"""", t ....d I~k-<!«tc- Rul~rnll! cfi.~os'c synem forMothodd09~of I8I·tim~chgno.tics. Jong dur.tion minions. lion~' for Slwl.~ olbiter det.ction of ig.....nd i..,.oct
.ndl d.~.202S
Excerpt from the NESC Presentation on the "Stateof the NASA..
~~g 'j.'~8h/Xf5tl!./~f, Nondestructive Evaluation (NDE) Discipline" *
• NDE expertise in high demand across all NASA missions- Challenge to provide sufficient expertise- Multi-Center cooperation key
• e.g. NESC NDE TDT, NASA NDE Working Group (NNWG), OrbiterNDE Working Group (ONWG)
- Reduced research capabilities and output lead to risk in meetingfuture mission requirements
• Many mature NDE technologies - challenge applying them to complexaerospace materials and structures- Composites, ceramics, TPS, multilayer, multi-functional structures,
etc.
• Interaction with other disciplines (materials, structures, etc.) presentchallenges
- NDE requirements, expectations, and need to consider NDE in theinitial design
• Structural Health Monitoring (SHM) is new frontier with great potentialreturns- Critical for longer duration manned space missions
KSC NDE Vital to Overall NASA NDEKSC ENGINEERING'" M -I SS-IonAND TECHNOLOGY
• KSC NDE required to maintain KSC/CCAFSinstitutional facility
• KSC NDE required to support current customers(customers defined later slide)
• KSC NDE will be required for future customers- Beginning with Shuttle Program KSC has historical
worked with operations centers (JSC, MSFC) andResearch Centers (LaRC, GRC) to develop andimplement advanced NDE procedures.
- Current and future and NASA programs are dependantof KSC to maintain its current core and advancedcapabilities
KSC ENGINEERINGANO TECHNOLOGY
Where we are now: KSC NDELaboratories
• Institutional (ISC) NDE Primary Services
Provide Non-Destructive Testing andEvaluation for the Kennedy Space Center/AirForce Operational Programs and Facilities
• Examples include- Crane hooks
- Lifting fixtures
- Pressure vessels
• Includes operational ground supportequipment and flight vehicle hardware.
• Provides 24/7 support launch siteoperations customers processing andlaunching rockets and payloads.
• The Lab also develops new NDEtechniques and equipment to improveevaluation capabilities.
• USA/Hangar N NDE Primary Services
Provide Non-Destructive Testing and Evaluationfor the Space Shuttle and other KSC OperationalPrograms
• Performs inspections in support ofspace operations and maintenance ofmulti-purpose space systems
• Provides NDE Project Engineering forNew Technology Development
• Includes advanced NDE capabilities
• Flash Infrared Thermography(Orbiter Wing Leading Edge)
• Terahertz (External Tank)
• Backscatter x-ray (External Tank)Provide R&D collaboration with the NASAEngineering Safety Center (NESC) NDETechnical Development Team
Institutional (ISC) Non-DestructiveExamination Laboratory
KSC ENGINEERING ....AND TECHNOLOGY
• Skills and Capabilities- Eddy Current Testing
Infrared imaging
Leak Testing
Micro-Focus X-Ray
Magnetic Particle
Fluorescent Dye Penetrant
Radiography
High Energy X-Ray - 420 kV
- Portable X-Ray and GammaSources
- Computed Tomography (CT)
- Ultrasonic Testing
- Visual
- Certified Weld Inspection (CWI)
- ASNT-certified Level III engineeringconsulting
JC ..~~_ 1".'"" Me.:oJ .-
,-----......,'""""T"-,I .~:":!z-~~
az. to ...A. ,"" ..
»- ..
Shuttle External Tank FoamShearography Inspection
1Il:17.111 .!!J"".!lf71'1T ..J~.:JI'~.",..,
T-SCdllP-s<:all
USA/Hangar N Non-Destructive ExaminationLaboratory
poo-r-,,- .-_ _ JRadiography
CT
Film and Digital
Laminography
Ultrasonic
A-Scan, B-Scan, P-Scan
3D CAD UT Modeling
Flash Thermography imaging
Shearography - Vacuum/Acoustic
Magnetic Particle
Fluorescent Dye Penetrant
Visual
CWI, Dimensional, UV Borescope
Eddy Current
MWM, Single/Multi Channel
Bolt Hole/Surface
Custom Coil
Terahertz
Large scale X-Ray Chamber
ll-Axis Robot and gantry
Structural Health Monitoring (IVHM)
Skills and Capabilities
KSC ENGINEERINGAND TECHNOLOGY
•
..KSC ENGINEERINGAND TECHNOLOGY
Materials Science Division Support
• Materials & Processes Engineering- Program support (engineering/project management)
- ESD Composites for Exploration
- OCT Composites Cryotank
- R&D
• Applied Physics Lab- Program support (applied R&D)
- R&D
• NASA NOE Working Group (NNWG)
• NESC NOE TOT
KSC ENGINEERINGANO TECHNOLOGY
Example of Past Projects
Device for making detailed maps oforbiter window defects
Ultrasonic leak locator
Prototype device to indicate H2leakage or fire at a flanged joint.
KSC ENGINEERING'"AND TECHNOLOGY
Current/Future NDE Customers
• KSC/CCAFS Institution- e.g. Pad modifications, cyrotanks, crawler
transporter, pressure vessels
• Launch Services Program (LSP)
• 21st Century Launch Program- Orion MPCV
- SLS
• Commercial Cargo
• Commercial Crew
21St Century Launch Complex
• Modernizing the KSCand CCFAS
- Launch architecture
- Environmental
- Payload Processing
- Range Capabilities
- Partnering with AirForce, State ofFlorida and the FAA
--KSC ENGINEERINGAND TECHNOLOGY
~KSC ENGINEERINGAND TECHNOLOGY
Orion MPCV and SLS
n .. r.J-2X
Upper
LR _. t
&'O.:i/~!
389 fr.
-- c. S ge. --ild,
_ Commercial Crew - Blue OriginKSC ENGINEERINGAND TECHNOLOGY
--~----
• Developing a Crew TransportationSystem comprised of a SpaceVehicle (SV) which will be launchedfirst on an Atlas V and then on BlueOrigin's own Reusable BoosterSystem (RBS)
• Capable of carrying 7 astronautsand will transfer NASA crew andcargo to and from the ISS, serve asan ISS emergency escape vehicle forup to210 days, and perform a.landlanding to minimize the costs ofrecovery and reuse.
KSC ENGINEERING~AND TECHNOLOGY
Commercial Crew - Boeing
• Developing a IIfull service" systemfor both NASA and commercialcustomers to LEO destinations.
• CST-lOa spacecraft is configured tocarry up to 7 crew members and/orcargo to LEO destinations includingISS and SA Sundancer spacecomplex
• Compatible with multiple launchvehicles
• Designed for land landings and canbe reused for up to 10 missions
r------ _Spacecraft S~ent
CST-100
~~...----Crew Module (CM)
~--- Service Mowle (SM)
Operations Segment "'----=--0
• Crew Training• cargo Integration• Mission Plann"ng• ssion Operations• landing and Recovery• Assembly Integrationand es Facility
• Mission Operations Center• Network services• Landing Site Facilities• Ti "ng Systems
Commercial Crew - Sierra NevadaKSC ENGINEERING~AND TECHNOLOGY
• Developing the Dream ChaserSpace System (DCSS).
• Provides LEO access to the ISSand commercial customersneeding suborbital services
• Third generation design derivedfrom extensive NASA Langleyresearch providing a reusable,pressurized, lifting-body vehiclethat lands on a conventionalrunway.
• Will most likely utilize an Atlas Vlaunch vehicle
~KSC ENGINEERINGAND TECHNOLOGY
Commercial Crew - SpaceX
• SpaceX's Dragon crew vehiclewas the first commercialspacecraft to return from orbit
• Maturation of theFalcon9/Dragon transportationsystem with a particular focus ondeveloping an integrated LaunchAbort System.
• Developing prototypes of the.crew cabin, crew seats and ..........---_;;:restraints, crew control panel ~......and life support system.
KSC ENGINEERINGANO TECHNOLOGY
50 what are K5C's needs?
• The basic infrastructure of NDE support will remain but at areduced capacity, especially in advanced NDE development- Consolidation is still in work
• The new NASA programs and the new commercialcustomers do not have the "deep pockets" that the ShuttleProgram had- The challenge for KSC is to maintain a world class NDE
organization with less resources
• The NASA Materials Science Division will remain the poefor NDE operations and advance NDE development- Key challenge is to forecast future customer needs- Examples of a few recent development efforts are on the
following charts
...KSC ENGINEERINGAND TECHNOLOGY
Multifunctional Hybrid CompositeMetamaterial Systems
• Inspection of damage and subsequent repairs on composite structureswhich will involve:
• Develop a Surface Wave propagating (SWP) structure consisting of arrayed sensors(piezoelectric), in conjunction with a passive single chip RadiofrequencyIdentification (RFID) strain/accelerometer/temp sensor configuration.
• The goal will be to simultaneously transfer power/ and communicate via a wireless network/ inorder to detect damage and induce or monitor the cure of a repair in a fiber reinforcedcomposite part.
• Validation of the tools using current NDI/NDE methods
• Repair of materials for primary structures (including newly developed outof autoclave material designed for use on primary structures).
• Cradle-to-grave monitoring of the repair including monitoring repair cure, the initialquality of repair during installation and continuing the monitoring throughout itslifetime.
• Provide cost-cutting measures for repair of out-of-autoclave composite structuresfor primary structures through the development of standard repair and monitoringkits
Cross-section view
~KSC ENGINEERINGAND TECHNOLOGY
Eddy Current Stress Gages for COPVHealth Monitoring
• Utilizes MWM® Technology
- Goal is to provide a means of directly measuringthe stresses at various depths in the overwrap
Skin depth: <'i == J 1;rffla
o
P'lm<:l'Y~ WIn.jlng.......,
Sec':lIlc ar\,•....Jlndlrgs
E.5.•Q.
~c:
.Qiii..2!G>a.
:.
0.1 ~~L-J...U.UU~'-""I--L~----l-J-J.-<~~'10' 10' 10' 10'
Frequency (Hz)
scanDireetlon
D==D==D==D==D==D==
WtJ4
~KSC ENGINEERINGANO TECHNOLOGY
Eddy Current Stress Gages for COPVHealth Monitoring
Magnitude vs. Set (Average of all Channels)
252010 15Pressurization Interval
5
17° Sensor Orientation60° Sensor Orientation90° Sensor Orientation
1.01
1.005
0.995
~KSC ENGINEERINGAND TECHNOLOGY
Wire ConstructionMaterials examined during development of detection layer
• Metal foils CSlonfig&lntion
• Nickel coated carbon fiber• Conductive carbon cloth• Metallized mylar tapes• Sputter coated metals• Electroplated metals• Printed-on conductive inks• Inherently conductive polymers
Cross section of RG316 wire withCu foil and PTFE jacket
0.1 "-"/' \, ,/ \
I "j "l 'I "1 '1 \I "j '.
I ", "" ..•..
...",
Ct "__0- _~_-_-. ..... ~.__..,. ....-._-"'-"".
IHJ6
o.tJ2
Extruded FEPTape wrappedDamage profile for TDR testing