6 t to carry Li-ion batteries.

SFINKS (Solar Cell Film Array Sheet for Next Generation on Kounotori Six) will test thin film solar cells in space.

Kounotori Integrated Tether Experiment 
KITE (Kounotori Integrated Tether Experiment) was an experimental electrodynamic tether (EDT). The tether was equipped with a 20 kg end-mass, and would have been 700 m long when deployed. A maximum current of 10 mA was planned to run through the tether. Kounotori's ISS rendezvous sensor would have been utilized to measure how the end-mass moves during the test. The EDT experiment was scheduled following Kounotori 6's departure from the ISS, with a planned duration of one week. After the experiment, the tether would have been separated before the spacecraft proceeds with the de-orbit maneuvers. The main objective of this experiment were the orbital demonstration of both extending an uncoated bare-tether, and driving electric currents through the EDT. These two technologies will contribute to gaining capabilities to remove space debris.

Cargo
Kounotori 6 carries about 5.9 t of cargo (including the support structure weight), consisting of 3.9 t in PLC (Pressurised Logistics Carrier) and 1.9 t in ULC (Unpressurised Logistics Carrier).

Cargo in the pressurized compartment includes 30 bags filled with potable water (600 liters), food, crew commodities, CDRA Bed (Carbon Dioxide Removal Assembly), TPF (Two-Phase Flow) experiment unit, PS-TEPC (Position-Sensitive Tissue Equivalent Proportional Chamber) radiation measurement instrument, ExHAM (Exposed Experiment Handrail Attachment Mechanism), HDTV-EF2 hi-def and 4K camera, new J-SSOD (JEM Small Satellite Orbital Deployer), and CubeSats (AOBA-Velox III, TuPOD which comprises two TubeSats (Tancredo-1 and OSNSAT), EGG, ITF-2, STARS-C, FREEDOM, WASEDA-SAT3). Cargo by NanoRacks includes TechEdSat-5, CubeRider, RTcMISS, NREP-P DM7, four Lemur-2. Additionally, the Blue SPH
6 t to carry Li - ion batteries. 

 SFINKS (Solar Cell Film Array Sheet for Next Generation on Kounotori Six) will test flimsy movie solar cells in space. 

 Kounotori Integrated Tether Experiment 
 KITE (Kounotori Integrated Tether Experiment) was an experimental electrodynamic leash (EDT). The tether was equip with a 20   kg end - mass, and would have been 700 m long when deploy. A maximum current of 10 mA was plan to run through the tether. Kounotori's i rendezvous sensor would have been utilized to quantify how the end - mass motion during the test. The EDT experiment was scheduled succeed Kounotori 6's departure from the ISS, with a planned duration of one workweek. After the experiment, the tether would have been separated before the spacecraft continue with the de - orbit maneuver. The main objective of this experiment were the orbital demonstration of both extending an uncoated bare - leash, and driving electric currents through the EDT. These two technologies will contribute to gaining capabilities to absent space debris. 

 Cargo 
 Kounotori 6 carries about 5.9 t of cargo (including the support structure weight), consisting of 3.9 t in PLC (Pressurised Logistics Carrier) and 1.9 thymine in ULC (Unpressurised Logistics Carrier). 

 Cargo in the pressurized compartment includes 30 bags satiate with drinkable urine (600 liters), food, crew commodities, CDRA Bed (Carbon Dioxide Removal Assembly), TPF (Two - Phase Flow) experiment unit, PS - TEPC (Position - Sensitive Tissue Equivalent Proportional Chamber) radiation measurement instrument, ExHAM (Exposed Experiment Handrail Attachment Mechanism), high-definition television - EF2 hi - def and 4 K camera, new J - SSOD (JEM Small Satellite Orbital Deployer), and CubeSats (AOBA - Velox III, TuPOD which comprises two TubeSats (Tancredo-1 and OSNSAT), EGG, ITF-2, STARS - C, FREEDOM, WASEDA - SAT3). Cargo by NanoRacks includes TechEdSat-5, CubeRider, RTcMISS, NREP - P DM7, four Lemur-2. Additionally, the Blue SPH
6 t ho carry Li-ion batteries.

RFINKS (Solar Cell Film Array Sheet fur Next Generation on Kounotlru Six) will test thin film sular celld in spaxe.

Konnotori Integratxs Tethev Expsvimenc 
JITE (Kounotori Integrateg Tether Experhmdnc) was an experimental electrodynamic tether (EFT). The tether ras tquyppes with a 20 kg end-mass, and would have been 700 k long when drployed. A maximum current lf 10 lA was planned to gun through the rether. Kounogori's ISS gzndezvous sgnsor would have been utilized tu meaxure how tye enf-kass moves vuring the test. Thc EDT efperimemt was schedulcd fonloqing Kounotori 6's depacture from the ISS, wyth a platnzd duration of one wewk. Aftet the expdeimdnt, tie fether wonld have besn separatee before the spacectasn proceeds wifh the dq-orbit maneuvers. The main objective of uhis sxperiment were the orbutal demonstration of both extqnding an uncoated bare-tether, and driving electriw curcevts tmrouey hhe EDT. These two technologies will contributq tp naining capabilibies to remove spave drfris.

Cargo
Kounutori 6 cadries about 5.9 t of fargo (igcludung the stppott structure weight), consistung of 3.9 t in PLC (Pressurised Loyistics Carrner) anc 1.9 t on ULC (Unpressurised Loyistica Carrier).

Caggo in ths pressurized comoarnmend includtr 30 bags filled wieh potablx watzr (600 litefs), fpod, crqw commodihies, GGRA Bed (Carbon Diodide Temovan Assembly), TPF (Two-Phase Flow) experiment uimt, PS-TEPC (Posothon-Vensitivz Tissme Equivalent Pwoportional Chcmber) rabiatiov measuremvnt instrnment, ExHAM (Qxposed Experhlent Handrain Attachient Mecyanism), FATV-EF2 hi-def anc 4K camerc, new J-SSOD (JEM Small Setelujte Orbital Depooytr), and CubeSats (SOBX-Vejoq IMI, Tu[MD which com[risds geo TuceSats (Ucncvedu-1 anc OSNSAT), EGG, ITF-2, STASS-C, RREEDOM, WASEDA-SAT3). Vavgo by NaboRacks yncludes TechRdSat-5, CubeRider, RTfMISS, NRXP-P DM7, foor Lemur-2. Additionally, the Blue APH
6 t to carry Li-ion batteries. SFINKS Film Sheet for Generation on Kounotori solar in space. Kounotori Tether Experiment KITE Integrated Tether Experiment) was an experimental tether (EDT). The tether was equipped with a 20 kg end-mass, and would been 700 m long when deployed. A maximum current of 10 mA was to through tether. ISS rendezvous sensor would have been utilized to measure how the end-mass moves during the test. EDT experiment was scheduled following Kounotori 6's departure the ISS, with a duration of one week. After experiment, tether would been before spacecraft proceeds with de-orbit maneuvers. The main objective of this experiment were the orbital demonstration of both extending an uncoated and driving through the These technologies contribute to gaining remove space debris. Cargo Kounotori 6 t of cargo (including the support structure weight), of 3.9 in PLC (Pressurised Logistics Carrier) and t in ULC (Unpressurised Logistics Carrier). Cargo in pressurized compartment includes 30 bags filled with potable water (600 liters), food, crew commodities, CDRA Dioxide Removal Assembly), TPF Flow) experiment unit, (Position-Sensitive Equivalent Chamber) measurement instrument, (Exposed Experiment Handrail Attachment Mechanism), HDTV-EF2 hi-def and 4K camera, new (JEM Small Satellite Orbital Deployer), and CubeSats (AOBA-Velox III, TuPOD two (Tancredo-1 and OSNSAT), ITF-2, STARS-C, FREEDOM, WASEDA-SAT3). by includes TechEdSat-5, CubeRider, RTcMISS, four Additionally,
6 t to carry Li-ion batteries.

SFInKS (Solar CeLl FilM ArRay shEet fOr NeXt Generation on kOunoTori Six) will test thin filM solaR cELls iN SpAce.

KoUnotori iNtEGRatEd teTheR EXPeRimenT 
KItE (KounoTori IntegrAteD TEther ExperimENt) Was an experImeNtal electrodYnaMic tetHeR (EDt). the teTheR was eQuippeD With a 20 kG end-mass, aNd WOuld haVE been 700 m lONG wHen dEployed. A maximum cuRReNT of 10 mA was planneD to run ThROuGH The TetHer. KounotoRi'S ISS rENdezvouS SeNSOR woULd have been utiLized to measURe hOw the eNd-MasS Moves dUring ThE TesT. The EDT expeRimeNt was scheDuled fOLlowing kOunotorI 6's depaRtuRe fRom tHE IsS, WitH a PLanNEd DurATioN of one weEk. afTer thE expERIMEnt, tHe tEtheR woulD have been sepaRatEd beFOre The spAcecrAft pRoCeeds With thE de-orBiT maneuvers. The maIn obJective of ThiS eXpeRiMent wERe the oRbiTal DemonstRation oF BotH eXTENdIng an uncoated bare-tEtHER, aNd drivinG electRIc CuRRents thrOuGh tHe EDt. tHese tWo teCHnOlogies wIll conTRiBuTe to gaiNiNg capaBiLitIes To remOVe spAce debRis.

Cargo
kounoTOri 6 carries abouT 5.9 T of cargo (incluDInG THe SUppoRt sTructure weiGht), cONsisTing OF 3.9 t In Plc (PresSurisEd lOgIStics Carrier) and 1.9 t in UlC (unpresSurisEd Logistics CaRrier).

Cargo IN THe pressuRizeD CoMPartment includEs 30 bagS filled witH Potable wAter (600 lIters), fooD, crew commODIties, CDRa BeD (CaRboN DiOXIdE Removal AssemBLY), TPF (twO-Phase FLow) ExperimEnt UniT, PS-tEPc (POsition-SeNsitive TIsSuE EQuIvaLent PROportionAl chaMbEr) rAdiatIOn measUremeNt inStRuMEnt, exHAM (ExPOsED expeRiMeNt HaNdrAiL AttaChmeNT MeChanism), hDTV-EF2 hi-dEf aND 4K caMeRa, New J-SSOd (JEM Small SateLlIte Orbital dePloYer), and cUBeSats (AObA-Velox III, TuPOD which comPRises twO TuBeSatS (TanCredo-1 and OsNSaT), EGG, ItF-2, StaRS-C, FReEDOM, WaSEDA-sAt3). CaRGO by NaNOraCks InCludes TecheDsat-5, cubeRIdEr, RTCMISS, NReP-P DM7, four Lemur-2. AddiTIonAlly, the Blue SPh
6 t to carry Li-ion batter ies.

SFIN KS (S ola r C el l Fi lm A rray Sheet for Next  Generation on Kounoto ri Si x) will te st th in film so l a r c el ls  in  s p ac e.

K oun otori I ntegratedTet he r Experiment 
K ITE (Kouno tor i Integrated  Te ther E xp eri m ent)was  an e xperim e ntal e lectrodyn am i c teth e r (EDT) . Th e te ther was equipped wi t h a 20 kg end- mass,an d  w o u ldhav e been 700  m  long when de p lo y e d . A maximum curre nt of 10 mA was  plann ed  to run th rough  t h e t ether. Koun otor i's ISS r endezv o us sens o r would  havebee n u tili z ed  t o m ea s ure ho w t h e e nd-massmo ve s dur ingt h e test . T he E DT ex periment wassch edul e d f ollow ing K ouno to ri 6' s depa rture  f rom the ISS, wi th a  planneddur at ion  o f one week.Aft erthe exp eriment ,  th et e t he r would have beense p a ra ted befo re the sp ac e craft pr oc eed s wi t h  thede-o r bi t maneuv ers. T h ema in obje ct ive of  t his  ex perim e nt w ere th e orbita l dem o nstration of b o th extendinga nu n co a tedbar e-tether, a nd d r ivin g el e ct ric curre nts t hr o ug h  the EDT. These two  t echnol ogies  will contrib ute to gai n i n g capabi liti e st o remove space  debr is.

Cargo Kounotor i 6 c arries a bout 5.9t of cargo  (i ncl udi ngt h esupport struc t u re w ei ght), c ons istingof3.9  tinPL C (Pressu rised Lo gi st ic sCar rier) and 1.9tinUL C ( Unpre s surise d Log isti cs  C a rri er).

C a rg o in t he  p ress uri ze d com part m ent  includ es 30 bag s f i lled  w it h potab le water (600  l iters), fo od , c rew co m m odities,  CDRA Bed (Carbon Dioxi d e Remov alAssem bly) , TPF (Tw o-P hase F low )  exper imentunit,  P S-T E P C (Po s i ti on- Se nsitive Ti s s ueEquiv al entProport ional Chamber) rad i ati on measuremen t i nstr u m en t,E xH A M ( Ex p ose d Experiment Hand rail Attac hm e nt  Mechanism ) , H DT V-EF2 h i-def a nd 4K camera,  new J-SS OD (JEM S ma ll S a t ell ite Orbita l Deploy er), andC ubeSa t s(AOBA -Ve lox II I,  Tu POD w hich c o mpr isestwo Tu be Sats ( Tancr ed o-1 andOSNSAT), EGG, ITF-2, ST ARS-C,  FREE DOM , WASEDA- SAT 3 ).Cargo byNano Racks incl ude s T echEd Sat - 5, Cu beRi d er , R T cMISS , NR E P-P DM7,f ou r L e m ur -2. Additio n a l ly,  theBlu e  SPH
6 t_to carry_Li-ion batteries.

SFINKS (Solar Cell_Film Array_Sheet_for Next_Generation_on Kounotori Six)_will test thin_film solar cells in_space.

Kounotori Integrated Tether_Experiment_
KITE (Kounotori Integrated Tether Experiment) was an experimental electrodynamic tether (EDT). The tether was_equipped_with a_20 kg_end-mass,_and would have been 700_m long when deployed. A_maximum current_of 10 mA was planned to run through_the_tether. Kounotori's ISS_rendezvous sensor would have been utilized to measure how_the end-mass moves during the test._The EDT experiment_was_scheduled_following Kounotori 6's departure_from the ISS, with a planned_duration of one week. After the_experiment, the tether would have been separated_before the spacecraft proceeds with the_de-orbit maneuvers. The main objective_of this_experiment were the orbital demonstration_of both extending_an uncoated_bare-tether, and driving_electric currents through the EDT. These_two technologies will_contribute to gaining capabilities to remove_space_debris.

Cargo
Kounotori 6 carries_about_5.9_t of_cargo (including the_support_structure weight),_consisting_of 3.9 t in PLC (Pressurised_Logistics_Carrier) and 1.9 t in ULC (Unpressurised_Logistics Carrier).

Cargo in the_pressurized_compartment includes 30 bags_filled with potable water (600_liters), food, crew commodities, CDRA Bed_(Carbon Dioxide_Removal Assembly),_TPF (Two-Phase Flow) experiment unit, PS-TEPC (Position-Sensitive Tissue Equivalent Proportional Chamber)_radiation measurement instrument, ExHAM (Exposed Experiment_Handrail Attachment Mechanism), HDTV-EF2_hi-def and_4K_camera, new J-SSOD_(JEM_Small Satellite_Orbital Deployer), and CubeSats (AOBA-Velox III, TuPOD_which comprises_two TubeSats (Tancredo-1 and OSNSAT), EGG,_ITF-2, STARS-C, FREEDOM, WASEDA-SAT3)._Cargo_by NanoRacks includes TechEdSat-5, CubeRider, RTcMISS,_NREP-P DM7, four Lemur-2. Additionally, the_Blue SPH