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NASA Technical Reports Server (NTRS) 20070017326: Assessment of Lithium-based Battery Electrolytes Developed under the NASA PERS Program PDF

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Preview NASA Technical Reports Server (NTRS) 20070017326: Assessment of Lithium-based Battery Electrolytes Developed under the NASA PERS Program

Assessment of Lithium-based Battery Electrolytes Developed under the NASA PERS Program William R. Bennett QSS Group, Inc. and Richard S. Baldwin NASA Glenn Research Center Recently, NASA formally completed the Polymer Energy Rechargeable System (PERS) Program, which was established in 2000 in collaboration with the Air Force Research Laboratory (AFRL) to support the development of polymer-based, lithium-based cell chemistries and battery technologies to address the next generation of aerospace applications and mission needs. The goal of this program was to ultimately develop an advanced, space-qualified battery technology, which embodied a solid polymer electrolyte (SPE) and complementary components, with improved performance characteristics that would address future aerospace battery requirements. Programmatically, the PERS initiative exploited both interagency collaborations to address common technology and engineering issues and the active participation of academia and private industry. The initial program phases focused on R&D activities to address the critical technical issues and challenges at the cell level. A variety of cell and polymeric electrolyte concepts were pursued as part of the development efforts undertaken at numerous governmental, industrial and academic laboratories. Numerous candidate electrolyte materials were developed, synthesized and optimized for evaluation. Utilizing the component screening facility and the “standardized” test procedures developed at the NASA Glenn Research Center, electrochemical screening and performance evaluations of promising candidate materials were completed. This overview summarizes test results for a variety of candidate electrolyte materials that were developed under the PERS Program. Electrolyte properties are contrasted and compared to the original project goals, and the strengths and weaknesses of the electrolyte chemistries are discussed. Limited cycling data for full-cells using lithium metal and vanadium oxide electrodes are also presented. Based on measured electrolyte properties, the projected performance characteristics and temperature limitations of batteries utilizing the advanced electrolytes and components have been estimated. Limitations for the achievement of practical performance levels are also discussed, as well as needs for future research and development. 1 s e t y m l o a r t r c g e o l r E P y S r 5 e R 3 t E 1 t 4 a P 4 B , o A i h d S O e A 5 d, s 3 n N a 1 a b e 44 vel - m h o, e l i C t h u r O r, i e e h d, t d n n t e i n a C L l u e v h f e c o d l r t C n a e et wi e d nt p nn c., d es Fiel e o Be In Bal n R wis m el . p, n e ss ev m R rou d S. Gle r at L e D lia S G har SA ente s il S c A C W i s Q R N h c A ar e s e R n n e Gl 2 d o t t e 7 . e or m e 9 b p r h 9c or p o c 1an d/ to h su s fle ear ed inform e anoned earcs to gies. ogiegeab Res mer ati srto olr A ound as forcell p olid-st envisogies. ce Ree effochnol technRecha a NAS e rve a gr wnd h sernol Foatid t ongy vi m Back tive effortbattery a stries witonents wtion tech d the Air collabormer-base -generatimer Enerram. in FY 2001 rogra llaboran liquid chemid compgenera ASA anpandedof poly of nexte PolyS) Prog elected nt (NRA) P /NASA coance Li-io um-basedmer-basebling next- Y 2000 Noratory exelopment ancement basis of them (PER articipants snnounceme er at Lewis Field Dh hiya Fbv v st PA nt on toln ae dey Ce De Lipe nLd AhS – h c I t r a e s • • • • e R n n e Gl 3 . S r o . U f y d g n o a l o y n t h i il c b e a t p y a r e c t y t e a y g v b g o r i l d e t o s s ec hn ase S gn en ost R bj ec b s. E si y, c O s t er- on P de rg ng e s m ti f t n ri a a o h u y e l c g t c l s c ld- po ppli efit wei ific ufa r n a n t c d o i h y e n el a w hip ace d be lig afet sp e ma ewis Fi blish aders erosp ipate plified, nsic s eased ity, lif rable Center at L sta le a tic m tri cr ns vo arch n i n n e a e E s s A i i d f e • • • • R n n e Gl 4 sed ace mer a p y B S ol m e P u ur m ogram Participants SELECTED CONTRACTOR AND GRANTEES Advanced Lithium Polymer Electrolyte for Li-Ion Batteries Novel Host Material for Ceramic Electrolytes Lithium Based Polymer Electrolyte Battery Nanostructured Single-Ion SPE for Lithium Batteries Development of Solvent-Free High Performance Li-Polymer Advanced Polyelectrolyte Separators for Rechargeable Lithium Batteries New Stable, More Conductive Solid Polymer Electrolyte Polymer Electrolytes for Solid-State Lithium Batteries Lithium Based Polymer Battery Development An Integrated Approach to Develop a High Energy Density Long Cycle Life LithiPolymer Battery New Solid Polymer Membranes for Rechargeable Lithium Batteries Thermal Modeling of Lithium Based SPE Battery in Microgravity Applications Development of Highly Conductive Polyelectrolytes for Lithium Batteries High Performance Li-Ion Polymer Electrolyte with Pendant Anion Receptors Advanced Li-Ion Polymer Batteries for Aerospace Applications New Polymer Electrolyte Cell Systems A Joint Simulation and Experimental Study of NanocompositePolymer Electrolytes Development of a Lithium-Based Polymer Energy Rechargeable System for FutApplications RAM GOVERNMENTAL PARTICIPANTS Novel Molecular Architectures for Improved Solid Polymer Electrolytes for LithiuBatteries Ionically-Conducting Channel Polymer Electrolytes Solid Polymer Electrolyte Development M G r A O R R P G P O S S S PR WD) PER kron PER PER Covalent Associates Eagle-Picher Technologies, LLC, Joplin, MO EIC Indiana University InvenTek Lawrence Berkeley National Laboratory (LBNL) LITHCHEM International Lithium Power Technologies Lockheed Martin / Comsat Max Power / Temple University Naval Air Warfare Center Weapons Division (NAWC National Center for Microgravity Research Northwestern University Physical Sciences, Inc. Texas Engineering Experimental Station (TAMU) University of Minnesota University of Utah Yardney Technical Products NASA Glenn Research Center (GRC)/University of A Air Force Research Laboratory (AFRL) –WPAFB Jet Propulsion Laboratory (JPL) Research Center at Lewis Field n n e Gl 5 f o t d n n s m e a m r n e e t p e n o r i c l s e s e v o t y e t l d o D e r V ) e d ct 4 m n e > c 1 yt a el g o m· ol xp S m) hin 0 t oh ectr was e PER -310S/c pproac ent Window 12 (>10 erties s stability Goals for El C Testing Facility ompare candidate ritical properties: gh ionic conductivity ( ~ +transference number a gh salt diffusion coeffici ectrochemical Stability gh Electronic Resistivity avorable Interfacial Prop able transport propertie hermal and dimensional echanical toughness h Center at Lewis Field R c c Hi Li Hi El Hi F St T M rc a e G s e • • • • • • • • • R n n e Gl 6 8 3. al o C g 0° RS 6 PE 3. 1 ) -K O T E 20 3.4 e, 1000/ n P 5°C sting ur o 2 e 40 3.2 perat ed at al t m s m Te a c nt al b / e 60 3.0 oc t S m pr s 5 e y eci mo -0 pl t 0 R 1 p i 8 8 ( · ctiv 100 GEL SPE DRY SPE IONOMER 62. mitted y) = 5 for su u 2 3 4 5 6 2. b vit y 0 0 0 0 0 t d E- E- E- E- E- u ti ti 1 1 1 1 1 s c n n mc/S ,ytivitcudnoC u a s d u e o n q l p o t C m c n e a r S o i c r s c i R h e e d f ffi on PE oac low e to on. rolyt mize n su I Gels approach goal at room emperature. Dry SPEs appr goal at >80°C. onomershave conductivity du mmobilized ani er 330 polymer elect e best dry SPE (opti omersnot provided i rch Center at Lewis Field t I i v h n ea O T o s • • • I Re n n e Gl 7 t e a e d yt C 4 es ur ui ol 3° 0. -6 r - 0 u at iq ct 2 2 1 al r L e at 0. C e l v e ° p 0 E e m t 8 SP tativ g te dry PE a 80°C 0.2 -810 at n S n n y e e i r t v s a D s e e r / r e 2m , r p p E c o e o , P f R 0+ Ds S t s n e i i ) . t 0 ) n e w er t+Ds on o d e o ( i o r l p r ( ati at , r a s o e nt r z y ct e i Pr mb cie ent ari nsit ele lif ent l n t nu ffi nc po de n, e ici or e oe o r t o ev eff sp enc n c alt c nde ren ucti nd co eld n r o s u ur d a n Fi Tra +Litransfe salt diffusi nfluence gradients Limiting c power pro utilization affected. alt diffusio rch Center at Lewis I a s e s e • • • R n n e Gl 8 5 sition v/sec. 4 po m anodic decom Ni at 10 3 Li/Li+ es n . d dow 0 mA/cm² ssive scans o 2 al, Volts vs ectro n 2 ce nti el uc 1 e i s t W 5 o s P s 0 a y l c t i t l 1 l i - o b V a n - w 3 t S o g h h n t al s or pi p wi u c C f p . t e y mi 0° ed stri al en ak lit i he at 8 miz ng/ met curr 3 V r m atib c s pti ati Li n 3. me rs mp tro ent E o y. e pl or atio at + oly acto co Field c m t f e P vi bl y d d p f d wis e S ti a c xi e d e e Le El measur for dry conduc reason efficien small o observ salt an could b nticipat arch Center at a e s e • • • • R n n e Gl ) 9 . a di " 8 / ) 5 . ( a e di od 8" et tr 5/ s k c ) ( a de ative) ene gas g nter-ele 1/2" dia. ask ectrode ve) EO m Oxi cover (neg polypropyl wavesprin spacer lithium cou SPE disc ( polymer m working el can (positi ed P i f i u d o i d m a - n n u a g V n h ty d si t i u t a c e i n w e a w z t ed d p o g i mi uil ing plor ectro al ca wind estin opti on. lls b Full Cell Test Vanadium oxide ex GRC as positive el material 200 mAh/g (practic or VO).613 3-Volt, fits stability Preliminary cycle-t coin cells with non- electrode formulati reliminary GRC ce ell as rod-coil SPE arch Center at Lewis Field f P w e s e R • • • • n n e Gl

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