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Active Solid State Dosimetry for Lunar EVA PDF

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Active Solid State Dosimetry for Lunar EVA. J.D. Wrbanek,1 G.F. Fralick,1 S.Y. Wrbanek1 and L.Y. Chen2 1NASA Glenn Research Center, Instrumentation & Controls Division, Cleveland, Ohio. 2Ohio Aerospace Institute, Brook Park, Ohio. Introduction: The primary threat to astronauts luminescence using thin film coated scintillation detec- from space radiation is high-energy charged particles, tors fabricated at NASA GRC as part of the Vehicle such as electrons, protons, alpha and heavier particles, Systems Program, shown in figure 2.[6] originating from galactic cosmic radiation (GCR), so- NASA GRC is leveraging these efforts to investi- lar particle events (SPEs) and trapped radiation belts in gate small and large area MEMS devices for sensitivity Earth orbit. There is also the added threat of secon- to radiation and to compare with commercial devices. dary neutrons generated as the space radiation interacts If these initial results look promising as a path for the with atmosphere, soil and structural materials.[1] design and fabrication of a prototype solid state do- For Lunar exploration missions, the habitats and simeter, further testing would be required in conjunc- transfer vehicles are expected to provide shielding tion with other researchers in the space radiation field from standard background radiation. Unfortunately, over the next few years. The long term objective of the Lunar Extravehicular Activity (EVA) suit is not this effort is to provide a compact, low power active expected to afford such shielding. Astronauts need to electronic dosimetry system that would not be ad- be aware of potentially hazardous conditions in their versely affected by radiation, with improved sensitivity immediate area on EVA before a health and hardware and detection capability for real-time monitoring of risk arises. These conditions would include fluctua- Lunar EVA conditions. tions of the local radiation field due to changes in the space radiation field and unknown variations in the local surface composition. Should undue exposure occur, knowledge of the dynamic intensity conditions during the exposure will allow more precise diagnostic Figure 1: Examples of NASA GRC SiC Fabrica- assessment of the potential health risk to the exposed tion: Defect free (far left) & typical (center left) SiC individual.[2] surfaces, and a SiC circuit (right). Technology Need: An active personal dosimeter for Low Earth Orbit (LEO) EVA use is specifically recommended by NASA JSC’s Radiation Dosimetry Working Group, and the National Council on Radia- tion Protection and Measurements (NCRP) recom- mends personal radiation monitoring for real-time dose rate and integrated dose in LEO.[3] Compared to the current LEO missions, the expeditions to the Moon Figure 2: Radiation Detector Development: NASA will place crews at a significantly increased risk of GRC is attempting to verify claims of nuclear energy hazardous radiation exposure. in sonoluminescence (left) using thin film coated scin- Current radiation measurement and warning sys- tillation detectors fabricated at NASA GRC (right). tems may be not adequate for the future Lunar mis- References: [1] Johnson A.S., Badhwar G.D., sions, and currently instruments do not exist that can Golightly M.J., Hardy A.C., Konradi A. and Yang make these measurements and be incorporated into the T.C. (1993) NASA TM-104782. [2] R. Turner (2000) Lunar EVA suit. However, MEMS devices fabricated LWS Community Workshop. [3] Vetter R.J., et al. from silicon carbide (SiC) to conduct low-noise neu- (2002) NCRP Report No. 142, 47-49. [4] Ruddy F.H., tron and alpha particle spectrometry have recently Dulloo A.R., Seidel J.G., Palmour J.W. and Singh R. been reported outside of the context of personal do- (2003) Nucl. Instr. and Meth. A 505, 159–162. simetry.[4] [5] Hunter G.W., Neudeck P.G., Xu J., Lucko D., Development Effort: NASA GRC has been lead- Trunek A., Artale M., Lampard P., Androjna D., ing the world in the development of SiC semiconduc- Makel D., Ward B. and Liu C.C. (2004) Mat. Res. Soc. tor technology, producing SiC semiconductor surfaces Symp. Proc. 815, 287-297. [6] Wrbanek J.D., Fralick of much higher quality than commercially available, as G.C., Wrbanek S.Y. and Weiland K.E. (2005) NASA shown in figure 1. These surfaces have demonstrated TM-2005-213419, 46-7. advantages over standard materials for other sensor applications.[5] In other activities, NASA GRC is attempting to verify claims of nuclear energy in sono- 1 A V E 5 0 0 2 ct- r 5-O a 2 n u n o L i s r ) i e I r v A o i t D n O y f ek ck ek ls Ce n e ( metr ban Frali ban ontro arch Ohio Che stitut Ohio r r W C e n , si W C. d es nd, Yu e I ark o . n R a c P D D. ave n Y n a nn vel ng- spa ok te ohn ust sa atio Gle Cle Lia ero Bro a J G u nt A A S t e S S o m A hi u d N O r t i s d ol n on el I si Fi S vi s Di wi s e e ol L v ntr at ti Co nter c d e n C A a h n c o r ti a a e t s n e e R m u n r n st e n Gl I 2 A V E 5 0 0 2 ct- r 5-O a 2 h n c u r a L s e m s r e o e R f t s n t y n y o r e S t si t m n l e u n nt e p m o m o e i at vir m p e pr s s s s o e En ut e e o ti ro r g l r e D Th n na ur ms en ve pe A tate tion adiatio Astro Meas Syste Chall y De RC Ex ons of S a R o & g G i olid Radi pace hreat t ation urrent eeds hnolo ASA pplicat on eld S e S T di C N c N A visi s Fi h a e Di wi e T – – R – – T – – ols Le v ntr at ti • • • Co nter c d e n C A a h n c o r ti a a e t s n e e R m u n r n st e n Gl I 3 ) s n ) ) o n ) s 5 0 i s e 20 u su n r 5-Oct- m o u 2 m r t c a t / o c u V r e r f l t e e s G s n & & on n ( io s e n c ) o V ati ati Ge io rfa etc. i u u d di ( m s , Ra nt Ra nt a m G’s e e / m c v V o T e r c n mi E Ge (f R o ( a s e s p ir o l ( n s v c n e C o S n ti o r c E r i t r c a t u u s 9 n ti P a e o li 3 o c di N S ra S- i a ar a st T on eld Radiat R –Gal E –Sol pped R ondary n-made Aurora Au from S Controls Divisi ter at Lewis Fi e c n c C P a e a nd Ce a G S Tr S M n a ch p tio ar a e S t s • • • • • n e e R m u n r n st e n Gl I 4 t n , a a e c : e g fi ) s a e i c n u m g 5 A. oni na a ) s ka sig Oct-200 DN hr or n d 998 nic ea re. a 25- n Threat o an astronaut’s d/or long term (c ation burns and/ sterilization, brai Health Research,“ es and Applications (1 con microelectro increasing the l unction and failu nd equipment is The Radiatio pace radiation can cause damage t amage can be short term (acute) an Acute effects typically include radi (“radiation sickness”) Chronic effects include cataracts, and/or an increased risk of cancer "Strategic Program Plan for Space Radiation NASA Office of Life and Microgravity Scienc pace radiation can also damage sili by affecting the carrier density and current, leading to equipment malf stronauts are Radiation Workers! Radiation exposure to personnel a health and operational issue. tion and Controls Division arch Center at Lewis Field a e S D S A t s • • • n e e R m u n r n st e n Gl I 5 l a n l S a 4 o 1 n S i 1 t o - 05 I ec ti TS Oct-20 n r c S 25- e r o Di r e m i t s D n o e r m l u f c e o S i l S e t c C r I t a ti s r l P a a y P n S d o e ) ) d i nt g ry e ry rt r t g t o e a e e p r r e m h m a m o r o t C e h e r e re r el C el P nit m u a t r t nt o si s ul e a e e M o a c v ul v l D i i i a a Me eh act hic act uiv y) re e) ve e) -V ( Ve ( q etr A iv si iv on ra er - er E m on ss as ss on eld ati Ext met ntra met sue ele iati (pa w P (pa s Divisi ewis Fi Radi VCPDS: Spectro CPDS: I Spectro EPC: Tis (active t AM: Rad (TLD’s) PD: Cre (TLD’s) tion and Control arch Center at L a e V E T R C nt es I e R m u n r n st e n Gl I 6 p u o r G / v so i sg y. la as na S An hen c. n IS s from tRadiatiorag-nt.js 25-Oct-2005 o urece ://s s PictSpahttp m e t s y S t n e m e r u s a e M S D D n P d n o C S P o el si Fi ati M / C PD VC s Divi ewis di A EP C E ntrol at L a V & o er R R T I d C ent n C a h • • • n c o r ti a a e t s n e e R m u n r n st e n Gl I 7 s A ’ ) C V O n S E o E J n g ti L o n a ( A i 2005 duri form Orbit NAS 3). and onal e & he at a adiat 25-Oct- ons e in th by 200 on ers rat s, t ws us r d onditi ulativ w Ear nded oup ( otecti nds p dose ssion e cre zardo Mission Nee of radiation c ission, accum eter badges. simeter for Lo cally recomme ry Working Gr n Radiation Pr 02) recomme g for real-time LEO. urrent LEO mi Moon will plac sed risk of ha toring ost-m dosim nal do pecifi simet ncil o ts (20 nitorin se in the c o the ncrea oni o p y so s s Do ou en mo do to s t y i sion Field Current m is limited t provided b Active per EVA use i Radiation National C Measurem radiation integrated Compared expedition significantl exposure. tion and Controls Divi arch Center at Lewis a e t s n e • • • • e R m u n r n st e n Gl I 8 s n n. u o o rdo e a mati cs cks uld ety uati nges haza befor nfor not troni on la by his n wo t saf al sit 25-Oct-2005 e y A r i y ec ic d t ig au rn Chall entiall n EV imete rrentl on el but sil ffecte ess of er des stron e exte ment e of pot e area o ses. nal dos ns is cu on silic mation itself a ectiven osimet prove a ss of th elop war diat k ari erso ditio ased nfor nd is e eff sic d o im ene Technology Dev ronauts need to be a nditions in their imme alth and hardware ris al-time feedback of p arding astronaut con ailable. al-time dosimeters b uld provide real-time i desired sensitivity a iation, decreasing th hnology. provements in the ba vide a valuable tool t d provide better awar d Controls Division enter at Lewis Field Ast co he Re reg av Re co the rad tec Im pro an tion an arch C a e t s n e • • • • e R m u n r n st e n Gl I 9 n n o o e i t si d c ula) a pk vi ce p aniane i n s mb 05 D a o oWr ct-20 r O s v er MicY. 25- d . a S ol a cal( r or pti t n O n f o o s s s e m C h c i c g ni e s k) n re & ar olo ro yst io nt nsoban n e n : ct s at e SeWr o es h ns e d nt m al D. i r c o el e e e sicJ. at d te ati er as m ls ag Phyk& ument applie ontrols applic sensors gh pow ology b al instru t contro nd man Thin Film (G.C.Fralic str nd d c wer ent e hi chn ptic gen g a C In ic a n an d po onm ratur anote ate o ntelli itorin ckaging sion Field R as io n vir pe n r d i on Pa)Divi wis SA G ucts b mentat sion a rsh en gh tem EMS & gh data tive an alth m vironment (L.Y.Chennd Controls Center at Le l a c e n a NA ond stru opu H Hi M Hi A H arsh E ntation esearch C n pr • • • • • • H me R i u n r n st e n Gl I

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