Astro2020 APC White Paper Litebird: an All-Sky Cosmic Microwave Background Probe of Inflation
Total Page:16
File Type:pdf, Size:1020Kb
Load more
Recommended publications
-
XIII Publications, Presentations
XIII Publications, Presentations 1. Refereed Publications E., Kawamura, A., Nguyen Luong, Q., Sanhueza, P., Kurono, Y.: 2015, The 2014 ALMA Long Baseline Campaign: First Results from Aasi, J., et al. including Fujimoto, M.-K., Hayama, K., Kawamura, High Angular Resolution Observations toward the HL Tau Region, S., Mori, T., Nishida, E., Nishizawa, A.: 2015, Characterization of ApJ, 808, L3. the LIGO detectors during their sixth science run, Classical Quantum ALMA Partnership, et al. including Asaki, Y., Hirota, A., Nakanishi, Gravity, 32, 115012. K., Espada, D., Kameno, S., Sawada, T., Takahashi, S., Ao, Y., Abbott, B. P., et al. including Flaminio, R., LIGO Scientific Hatsukade, B., Matsuda, Y., Iono, D., Kurono, Y.: 2015, The 2014 Collaboration, Virgo Collaboration: 2016, Astrophysical Implications ALMA Long Baseline Campaign: Observations of the Strongly of the Binary Black Hole Merger GW150914, ApJ, 818, L22. Lensed Submillimeter Galaxy HATLAS J090311.6+003906 at z = Abbott, B. P., et al. including Flaminio, R., LIGO Scientific 3.042, ApJ, 808, L4. Collaboration, Virgo Collaboration: 2016, Observation of ALMA Partnership, et al. including Asaki, Y., Hirota, A., Nakanishi, Gravitational Waves from a Binary Black Hole Merger, Phys. Rev. K., Espada, D., Kameno, S., Sawada, T., Takahashi, S., Kurono, Lett., 116, 061102. Y., Tatematsu, K.: 2015, The 2014 ALMA Long Baseline Campaign: Abbott, B. P., et al. including Flaminio, R., LIGO Scientific Observations of Asteroid 3 Juno at 60 Kilometer Resolution, ApJ, Collaboration, Virgo Collaboration: 2016, GW150914: Implications 808, L2. for the Stochastic Gravitational-Wave Background from Binary Black Alonso-Herrero, A., et al. including Imanishi, M.: 2016, A mid-infrared Holes, Phys. -
X-Ray Telescope
Early results of the Hitomi satellite Hiro Matsumoto Ux group & KMI Nagoya Univ.1 Outline •Hitomi instruments •Early scientific results –DM in Perseus –Turbulence in Perseus –others 2 Japanese history of X-ray satellites Launch, Feb. 17, 2016 Weight Suzaku Ginga ASCA Hitomi Tenma Hakucho Rocket 3 International collaboration More than 160 scientists from Japan/USA/Europe 4 Attitude anomaly Loss of communication (Mar. 26, 2016) spinning Gave up recovery (Apr. 28, 2016)5 Hitomi Obs. List Target Date Perseus Cluster of galaxies Feb. 25—27, 2016 Mar. 4—8, 2016 N132D Supernova remnants Mar. 8—11, 2016 IGR J16318-4848 Pulsar wind nebula Mar. 11—15, 2016 RXJ 1856-3754 Neutron star Mar. 17—19, 2016 Mar. 23—25, 2016 G21.5-0.9 Pulsar wind nebula Mar. 19—23, 2016 Crab Pulsar wind nebula Mar. 25, 2016 6 Scienfitic Instruments 7 4 systems Name X-Ray Telescope SXS Soft Micro-calorimeter (E<10keV) SXI Soft CCD (E<10keV) HXI Hard Si/CdTe (E<80keV) SGD --- Si/CdTe (Compton) 8 Wide energy range (0.3—600keV) HXT 1keV∼ 107K SXT SGD SXI HXI SXS 9 SXT + SXS (0.3—12keV) Soft X-ray Telescope Soft X-ray Spectrometer (X-ray micro-calorimeter) f=5.6m 10 Soft X-ray Spectrometer (SXS) FOV: 3′ × 3′ Δ푇 ∝ ℎ휈 6 × 6 pix 11 Energy Resolution Hitomi SXS Suzaku CCD Δ퐸 = 5 푒푉@ 6푘푒푉 (cf. CCD Δ퐸 = 130 푒푉)12 Before Hitomi: gratings Point source Extended Not good for extended objects 13 X-ray microcalorimeter Extended Non-dispersive type. Spatial extension doesn’t matter. -
Progress with Litebird
LiteBIRD Lite (Light) Satellite for the Studies of B-mode Polarization and Inflation from Cosmic Background Radiation Detection Progress with LiteBIRD Masashi Hazumi (KEK/Kavli IPMU/SOKENDAI/ISAS JAXA) for the LiteBIRD working group 1 LiteBIRD JAXA Osaka U. Kavli IPMU Kansei U. Tsukuba APC Paris T. Dotani S. Kuromiya K. Hattori Gakuin U. M. Nagai R. Stompor H. Fuke M. Nakajima N. Katayama S. Matsuura H. Imada S. Takakura Y. Sakurai TIT Cardiff U. I. Kawano K. Takano H. Sugai Kitazato U. S. Matsuoka G. Pisano UC Berkeley / H. Matsuhara T. Kawasaki R. Chendra LBNL T. Matsumura Osaka Pref. U. KEK Paris ILP D. Barron K. Mitsuda M. Inoue M. Hazumi Konan U. U. Tokyo J. Errard J. Borrill T. Nishibori K. Kimura (PI) I. Ohta S. Sekiguchi Y. Chinone K. Nishijo H. Ogawa M. Hasegawa T. Shimizu CU Boulder A. Cukierman A. Noda N. Okada N. Kimura NAOJ S. Shu N. Halverson T. de Haan A. Okamoto K. Kohri A. Dominjon N. Tomita N. Goeckner-wald S. Sakai Okayama U. M. Maki T. Hasebe McGill U. P. Harvey Y. Sato T. Funaki Y. Minami J. Inatani Tohoku U. M. Dobbs C. Hill K. Shinozaki N. Hidehira T. Nagasaki K. Karatsu M. Hattori W. Holzapfel H. Sugita H. Ishino R. Nagata S. Kashima MPA Y. Hori Y. Takei A. Kibayashi H. Nishino T. Noguchi Nagoya U. E. Komatsu O. Jeong S. Utsunomiya Y. Kida S. Oguri Y. Sekimoto K. Ichiki NIST R. Keskitalo T. Wada K. Komatsu T. Okamura M. Sekine T. Kisner G. Hilton R. Yamamoto S. Uozumi N. -
Updated Design of the CMB Polarization Experiment Satellite Litebird
Journal of Low Temperature Physics (2020) 199:1107–1117 https://doi.org/10.1007/s10909-019-02329-w Updated Design of the CMB Polarization Experiment Satellite LiteBIRD H. Sugai, et al. [full author details at the end of the article] Received: 30 August 2019 / Accepted: 26 December 2019 / Published online: 27 January 2020 © The Author(s) 2020 Abstract Recent developments of transition-edge sensors (TESs), based on extensive experi- ence in ground-based experiments, have been making the sensor techniques mature enough for their application on future satellite cosmic microwave background (CMB) polarization experiments. LiteBIRD is in the most advanced phase among such future satellites, targeting its launch in Japanese Fiscal Year 2027 (2027FY) with JAXA’s H3 rocket. It will accommodate more than 4000 TESs in focal planes of refective low-frequency and refractive medium-and-high-frequency telescopes in order to detect a signature imprinted on the CMB by the primordial gravitational waves predicted in cosmic infation. The total wide frequency coverage between 34 and 448 GHz enables us to extract such weak spiral polarization patterns through the precise subtraction of our Galaxy’s foreground emission by using spectral dif- ferences among CMB and foreground signals. Telescopes are cooled down to 5 K for suppressing thermal noise and contain polarization modulators with transmis- sive half-wave plates at individual apertures for separating sky polarization signals from artifcial polarization and for mitigating from instrumental 1/f noise. Passive cooling by using V-grooves supports active cooling with mechanical coolers as well as adiabatic demagnetization refrigerators. Sky observations from the second Sun– Earth Lagrangian point, L2, are planned for 3 years. -
Optical Blocking Performance of Ccds Developed for the X-Ray
Optical Blocking Performance of CCDs Developed for the X-ray Astronomy Satellite XRISM Hiroyuki Uchidaa,∗, Takaaki Tanakaa, Yuki Amanoa, Hiromichi Okona, Takeshi G. Tsurua, Hirofumi Nodae,f, Kiyoshi Hayashidae,f, Hironori Matsumotoe,f, Maho Hanaokae, Tomokage Yoneyamae, Koki Okazakie, Kazunori Asakurae, Shotaro Sakumae, Kengo Hattorie, Ayami Ishikurae, Hiroshi Nakajimah, Mariko Saitod, Kumiko K. Nobukawad,b, Hiroshi Tomidag, Yoshiaki Kanemaruc, Jin Satoc, Toshiyuki Takakic, Yuta Teradac, Koji Moric, Hikari Kashimurah, Takayoshi Kohmurai, Kouichi Haginoi, Hiroshi Murakamij, Shogo B. Kobayashik, Yusuke Nishiokac, Makoto Yamauchic, Isamu Hatsukadec, Takashi Sakol, Masayoshi Nobukawal, Yukino Urabem, Junko S. Hiragam, Hideki Uchiyaman, Kazutaka Yamaokao, Masanobu Ozakip, Tadayasu Dotanip,q, Hiroshi Tsunemie, Hisanori Suzukir, Shin-ichiro Takagir, Kenichi Sugimotor, Sho Atsumir, Fumiya Tanakar aDepartment of Physics, Kyoto University, Kitashirakawa Oiwake-cho, Sakyo, Kyoto, Kyoto 606-8502, Japan bDepartment of Physics, Kindai University, 3-4-1 Kowakae, Higashi-Osaka, Osaka 577-8502, Japan cFaculty of Engineering, University of Miyazaki, 1-1 Gakuen Kibanadai Nishi, Miyazaki 889-2192, Japan dDepartment of Physics, Faculty of Science, Nara Women’s University, Kitauoyanishi-machi, Nara, Nara 630-8506, Japan eDepartment of Earth and Space Science, Osaka University, 1-1 Machikaneyama-cho, Toyonaka, Osaka 560-0043, Japan fProject Research Center for Fundamental Sciences, Osaka University, 1-1 Machikaneyama-cho, Toyonaka, Osaka 560-0043, Japan gJapan -
Arxiv:2006.06594V1 [Astro-Ph.CO]
Mitigating the optical depth degeneracy using the kinematic Sunyaev-Zel'dovich effect with CMB-S4 1, 2, 2, 1, 3, 4, 5, 6, 5, 6, Marcelo A. Alvarez, ∗ Simone Ferraro, y J. Colin Hill, z Ren´eeHloˇzek, x and Margaret Ikape { 1Berkeley Center for Cosmological Physics, Department of Physics, University of California, Berkeley, CA 94720, USA 2Lawrence Berkeley National Laboratory, One Cyclotron Road, Berkeley, CA 94720, USA 3Department of Physics, Columbia University, New York, NY, USA 10027 4Center for Computational Astrophysics, Flatiron Institute, New York, NY, USA 10010 5Dunlap Institute for Astronomy and Astrophysics, University of Toronto, 50 St George Street, Toronto ON, M5S 3H4, Canada 6David A. Dunlap Department of Astronomy and Astrophysics, University of Toronto, 50 St George Street, Toronto ON, M5S 3H4, Canada The epoch of reionization is one of the major phase transitions in the history of the universe, and is a focus of ongoing and upcoming cosmic microwave background (CMB) experiments with im- proved sensitivity to small-scale fluctuations. Reionization also represents a significant contaminant to CMB-derived cosmological parameter constraints, due to the degeneracy between the Thomson- scattering optical depth, τ, and the amplitude of scalar perturbations, As. This degeneracy subse- quently hinders the ability of large-scale structure data to constrain the sum of the neutrino masses, a major target for cosmology in the 2020s. In this work, we explore the kinematic Sunyaev-Zel'dovich (kSZ) effect as a probe of reionization, and show that it can be used to mitigate the optical depth degeneracy with high-sensitivity, high-resolution data from the upcoming CMB-S4 experiment. -
Global Satellite Communications Technology and Systems
International Technology Research Institute World Technology (WTEC) Division WTEC Panel Report on Global Satellite Communications Technology and Systems Joseph N. Pelton, Panel Chair Alfred U. Mac Rae, Panel Chair Kul B. Bhasin Charles W. Bostian William T. Brandon John V. Evans Neil R. Helm Christoph E. Mahle Stephen A. Townes December 1998 International Technology Research Institute R.D. Shelton, Director Geoffrey M. Holdridge, WTEC Division Director and ITRI Series Editor 4501 North Charles Street Baltimore, Maryland 21210-2699 WTEC Panel on Satellite Communications Technology and Systems Sponsored by the National Science Foundation and the National Aeronautics and Space Administration of the United States Government. Dr. Joseph N. Pelton (Panel Chair) Dr. Charles W. Bostian Mr. Neil R. Helm Institute for Applied Space Research Director, Center for Wireless Deputy Director, Institute for George Washington University Telecommunications Applied Space Research 2033 K Street, N.W., Rm. 304 Virginia Tech George Washington University Washington, DC 20052 Blacksburg, VA 24061-0111 2033 K Street, N.W., Rm. 340 Washington, DC 20052 Dr. Alfred U. Mac Rae (Panel Chair) Mr. William T. Brandon President, Mac Rae Technologies Principal Engineer Dr. Christoph E. Mahle 72 Sherbrook Drive The Mitre Corporation (D270) Communications Satellite Consultant Berkeley Heights, NJ 07922 202 Burlington Road 5137 Klingle Street, N.W. Bedford, MA 01730 Washington, DC 20016 Dr. Kul B. Bhasin Chief, Satellite Networks Dr. John V. Evans Dr. Stephen A. Townes and Architectures Branch Vice President Deputy Manager, Communications NASA Lewis Research Center and Chief Technology Officer Systems and Research Section MS 54-2 Comsat Corporation Jet Propulsion Laboratory 21000 Brookpark Rd. -
Science from Litebird
Prog. Theor. Exp. Phys. 2012, 00000 (27 pages) DOI: 10.1093=ptep/0000000000 Science from LiteBIRD LiteBIRD Collaboration: (Fran¸coisBoulanger, Martin Bucher, Erminia Calabrese, Josquin Errard, Fabio Finelli, Masashi Hazumi, Sophie Henrot-Versille, Eiichiro Komatsu, Paolo Natoli, Daniela Paoletti, Mathieu Remazeilles, Matthieu Tristram, Patricio Vielva, Nicola Vittorio) 8/11/2018 ............................................................................... The LiteBIRD satellite will map the temperature and polarization anisotropies over the entire sky in 15 microwave frequency bands. These maps will be used to obtain a clean measurement of the primordial temperature and polarization anisotropy of the cosmic microwave background in the multipole range 2 ` 200: The LiteBIRD sensitivity will be better than that of the ESA Planck satellite≤ by≤ at least an order of magnitude. This document summarizes some of the most exciting new science results anticipated from LiteBIRD. Under the conservatively defined \full success" criterion, LiteBIRD will 3 measure the tensor-to-scalar ratio parameter r with σ(r = 0) < 10− ; enabling either a discovery of primordial gravitational waves from inflation, or possibly an upper bound on r; which would rule out broad classes of inflationary models. Upon discovery, LiteBIRD will distinguish between two competing origins of the gravitational waves; namely, the quantum vacuum fluctuation in spacetime and additional matter fields during inflation. We also describe how, under the \extra success" criterion using data external to Lite- BIRD, an even better measure of r will be obtained, most notably through \delensing" and improved subtraction of polarized synchrotron emission using data at lower frequen- cies. LiteBIRD will also enable breakthrough discoveries in other areas of astrophysics. We highlight the importance of measuring the reionization optical depth τ at the cosmic variance limit, because this parameter must be fixed in order to allow other probes to measure absolute neutrino masses. -
Development of 60Μm Pitch Cdte Double-Sided Strip Detector for FOXSI-3 Rocket Experiment
Development of 60µm pitch CdTe double-sided strip detector for FOXSI-3 rocket experiment Kento Furukawa(U-Tokyo, ISAS/JAXA) Shin'nosuke Ishikawa, Tadayuki Takahashi, Shin Watanabe(ISAS/JAXA), Koichi Hagino(Tokyo University of Science), Shin'ichiro Takeda(OIST), P.S. Athiray, Lindsay Glesener, Sophie Musset, Juliana Vievering (U. of Minnesota), Juan Camilo Buitrago Casas , Säm Krucker (SSL/UCB), and Steven Christe (NASA/GSFC) 1 2 CdTe semiconductor and diode device Cadmium Telluride semiconductor : • High density • Large atomic number • High efficiency Issue : small µτ product especially for holes 260eV(FWHM) • Uniform & thin device @6.4keV 1400V,-40℃ • Schottky Diode (Takahashi et al. 1998 ) High bias voltage full charge collection + high energy resolution Takahashi et al. (2005) 3 Application of CdTe Diode Double-sided Strip Detector Watanabe et al. 2009 Anode(Pt): Ohmic contact Cathode(Al): Schottky contact Astrophysical Application • Hard X-ray Imager(HXI) onboard Hitomi(ASTRO-H) satellite • FOXSI rocket mission Medical Application • Small animal SPECT system (OIST/JAXA) 4 Hard X-ray study of the Sun Observation Target : the Sun Corona and flare Scientific Aim • Coronal Heating (thermal emission) • Particle Acceleration (non-thermal emission ) →Sensitive Hard X-ray imaging and spectral observation is the key especially for small scale flares study Soft X-ray image by Hinode (micro and nano) (NAOJ/JAXA) So far only Indirect Imaging e.g. RHESSI spacecraft (Rotational Modulation collimator) No direct imaging in hard X-ray band for solar mission 5 FOXSI rocket mission FOXSI experiment (UCB/SSL, NASA, UMN, ISAS/JAXA) Indirect Direct Imaging Spectroscopy with Focusing Optics in Hard X-ray Hard X-ray telescopes + CdTe focal plane detectors FOXSI’s hard X-ray telescope clearly identified a micro-flare with high S/N ratio Direct Telescope Angular resolution : 5 arcsec (FWHM) Focal plane detector 50µm on focal plane Krucker et al. -
Macquarie University Researchonline
Macquarie University ResearchOnline This is the published version of: Anand Sivaramakrishnan ; David Lafrenière ; K. E. Saavik Ford ; Barry McKernan ; Anthony Cheetham ; Alexandra Z. Greenbaum ; Peter G. Tuthill ; James P. Lloyd ; Michael J. Ireland ; René Doyon ; Mathilde Beaulieu ; André Martel ; Anton Koekemoer ; Frantz Martinache ; Peter Teuben " Non- redundant Aperture Masking Interferometry (AMI) and segment phasing with JWST-NIRISS," in Space telescopes and instrumentation 2012 : optical, infared, and millimeter wave 1-6 July 2012 Amsterdam, Netherlands, edited by Mark C. Clampin, Giovanni G. Fazio, Howard A. MacEwen, Jacobus M. Oschmann, Proceedings of SPIE Vol. 8442 (SPIE, Bellingham, WA, 2012) Article CID Number 84422S. Access to the published version: http://dx.doi.org/10.1117/12.925565 Copyright: Copyright 2012 Society of Photo Optical Instrumentation Engineers. One print or electronic copy may be made for personal use only. Systematic reproduction and distribution, duplication of any material in this paper for a fee or for commercial purposes, or modification of the content of the paper are prohibited. Non-Redundant Aperture Masking Interferometry (AMI) and Segment Phasing with JWST-NIRISS Anand Sivaramakrishnana,j, David Lafreni`ereb, K. E. Saavik Fordc,j,k, Barry McKernanc,j,k, Anthony Cheethamd, Alexandra Z. Greenbaume, Peter G. Tuthilld, James P. Lloydf, Michael J. Irelandg, Ren´eDoyonb, Mathilde Beaulieub, Andr´eMartela, Anton Koekemoera, Frantz Martinacheh, Peter Teubeni a Space Telescope Science Institute, 3700 San Martin Drive, Baltimore, MD 21218, United States b D´epartement de Physique, Universit´ede Montr´eal,Montr´eal,Qc, H3C 3J7, Canada c Dept. of Science, Borough of Manhattan Community College, City University of New York, 199 Chambers Street, NY 10007 United States d School of Physics, University of Sydney, NSW 2006, Australia e Johns Hopkins University, Department of Physics & Astronomy, 366 Bloomberg Center, 3400 N. -
List of RN/LPN Required to Complete Fingerprinting by June 30, 2021
List of RN/LPN Required to Complete Fingerprinting by June 30, 2021 RN 74156 ABAD CHARLES U RN 61837 ACASIO KYRA K RN 75958 ADVINCULA ROLAND D J RN 75271 ABAD GLORY GAY M RN 59937 ACCOUSTI NEAL O RN 42910 ADZUARA MARY JANE R RN 76449 ABALOS JUDY S RN 52918 ACEBO RUSSELL J RN 72683 AETO JUSTIN RN 38427 ABALOS TRICIA H M RN 43188 ACEVEDO JUNE D RN 86091 AFONG CLAREN C D RN 70657 ABANES JANE J RN 68208 ACIDERA NORIVIE S RN 72856 AGACID MARIE JOY H RN 46560 ABANIA JONATHAN R RN 59880 ACIO ROSARIO A D RN 78671 AGANOS DAWN Y A V RN 67772 ABARQUEZ BLESSILDA C RN 72528 ACKLIN JUSTIN P RN 85438 AGARAN NOBEMEN O RN 67707 ABATAYO LIEZL P RN 68066 ACOB FERLITA D RN 52928 AGARAN TINA K LPN 7498 ABBEY LORI J RN 35794 ACOBA BETH MARY BARN RN 33999 AGASID GLISERIA D RN 77337 ABE DAVID K RN 73632 ACOBA JULIA R LPN 18148 AGATON KRYSTLE LIAAN RN 57015 ABE JAYSON K RN 53744 ACOPAN MARK N RN 66375 AGBAYANI REYNANTE LPN 6111 ABE LORI R RN 55133 ACOSTA MARISSA R RN 58450 AGCAOILI ANNABEL RN 18300 ABE LYNN Y LPN 18682 ACOSTA MYLEEN G A RN 54002 AGCAOILI FLORENCE A RN 73517 ABE SUN-HWA K RN 69274 ACRE-PICKRELL ALEXAN RN 79169 AGDEPPA MARK J RN 84126 ABE TIFFANY K RN 45793 ACZON-ARMSTRONG MARI RN 41739 AGENA DALE S RN 69525 ABEE JENNIFER E RN 19550 ADAMS CAROLYN L RN 33363 AGLIAM MARILYN A RN 69992 ABEE KEVIN ANDREW RN 73979 ADAMS JENNIFER N RN 46748 AGLIBOT NANCY A RN 69993 ABELLADA MARINEL G RN 39164 ADAMS MARIA V RN 38303 AGLUGUB AURORA A RN 66502 ABELLANIDA STEPHANIE RN 52798 ADAMSKI MAUREEN RN 68068 AGNELLO TAI D RN 83403 ABERILLA JEREMY J RN 84737 ADDUCCI -
Message from the Director General September 2017 Saku Tsuneta Director General
Message from the Director General September 2017 Saku Tsuneta Director General Institute of Space and Astronautical Science Japan Aerospace Exploration Agency On April 28, 2016, the Japan former ISAS project managers, and levels, the satellite was declared to Aerospace Exploration Agency an Action Plan for Reforming ISAS have entered into its scheduled orbit (JAXA) made the difficult decision Based on the Anomaly Experienced in March 2017. The successful start to terminate attempts to restore by Hitomi was developed. In of the ARASE mission is a testament communication with the X-ray addition, “town hall meetings” were to the dedication and skills across Astronomy Satellite ASTRO-H (also held to share the spirit and practice JAXA. known as HITOMI), which was of the action plan with all ISAS ISAS is currently operating six launched on February 17, 2016, due employees. The plan, which was satellites and space probes: ARASE, to the communication anomalies applied to launch preparations of Hayabusa2, HISAKI, AKATSUKI, that occurred on March 26, 2016. the geospace exploration satellite HINODE, and GEOTAIL. Asteroid Since that time, in consultation with ARASE, contributed to the successful Explorer Hayabusa2, which is experts inside as well as outside and stable operation of that satellite, currently on its planned trajectory JAXA, the Institute of Space and and will be applied to other projects towards the 162173 Ryugu asteroid Astronautical Science (ISAS) has such as the Smart Lander for under ion engine power, is equipped been making every possible effort Investigating Moon (SLIM). The plan- with new technologies for solar to determine what went wrong, and do-check-act (PDCA) cycle should system exploration such as long- what can be done to prevent this work to further refine both current distance communication using Ka- from happening again in the future.