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Serena M. Aunon-Chancellor (M.D.) NASA Astronaut
National Aeronautics and Space Administration Lyndon B. Johnson Space Center Houston, Texas 77058 October 2019 Serena M. Aunon-Chancellor (M.D.) NASA Astronaut Summary: Dr. Serena M. Aunon was selected by NASA in 2009. Board certified in Internal and Aerospace Medicine, she recently served as Flight Engineer on the International Space Station for Expeditions 56 and 57. During her time on orbit, the crews contributed to hundreds of experiments in biology, biotechnology, physical science and Earth science aboard the International Space Station. Investigations were led into new cancer treatment methods and algae growth in space. The crew also installed a new Life Sciences Glovebox, a sealed work area for life science and technology investigations that can accommodate two astronauts. Serena’s first flight, she logged in 197 days in space. She currently covers medical issues and on-orbit support in the Astronaut Office. Personal Data: Born April 9, 1976 in Indianapolis, Indiana. Considers Fort Collins, CO, to be her home town. Married to Jeff Chancellor and she has a stepdaughter, Serafina Chancellor. Personal and recreational interests include mountain hiking and providing medical care to the underserved. Education: Graduated from Poudre High School, Fort Collins, Colorado in 1993. Received a Bachelor of Science in Electrical Engineering from The George Washington University, Washington, D.C., in 1997 and a Doctorate of Medicine from The University of Texas - Health Science Center at Houston in 2001. Completed a three-year residency in internal medicine at The University of Texas Medical Branch (UTMB) in Galveston, Texas, in 2004, and then completed an additional year as Chief Resident in the Internal Medicine Department in 2005. -
120611MS.Pdf
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -ミルスペース 120611- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - [What’s New in Virtual Library?] McGrawHill AW&ST AVIATION WEEK 1205AeroAme_Cover-ss.jpg 120528AWST_Contents.pdf, Cover.jpg 1204AeroAme_Cover-s.jpg Milbank Space Business Review SJAC 1205_Space Business Review.pdf SJAC1203_Jisedai-Uchu-Project-ni-kansuru-Chosa_Contents.pd NASA KSC SpaceportNews f, Cover.jpg 120601nasa_KSC_SpaceportNews_8pages.pdf, Cover.jpg SJAC1203_CD_Sekai-No-Uchu-Infra-Databook_Cover.jpg NASA MSFC MarshallStar CNES CnesMag 120530MarshallStar_Cover.jpg 1204cnesmag_No.53_Contents.pdf, Cover.jpg 120523MarshallStar_Cover.jpg ISAS ISAS News AIAA Aerospace America 1205ISAS_News_374_14pages.pdf, Cover.jpg 1206AeroAme_Cover-ss.jpg [What’s New in Real Library?] 重力とは何か、アインシュタインから超弦理論へ、宇宙の謎に迫る、 大栗博司 (幻冬舎新書, 12.05) 収蔵。 - - - - - - - - - - - - - - - - - - - Futron 12.06- - - - - - - - - - - - - - - - - - - - - - - - 2012 Orbital Launches by Launch Vehicle Family 2012 Orbital Commercial Launches 1 Manufacturer Market Share of Satellites Launched Through May 31, 2012 Selected Satellites with Regulatory Activity During May 2012 Satellite Location Activity NSS-7 20WL THE FCC granted SES‘s request to modify its license in terms of its access to the U.S. market within the FCC's Permitted Space Station List by relocating the C- and Ku-band operations for NSS-7 from 22 WL to 20 WL. DIRECTV 14 99WL DIRECTV applied to launch and operate a Ka-band satellite, DIRECTV 14, to be located at 99 WL. Intelsat 19 194WL The FCC granted Intelsat's request to launch and operate a C-/Ku-band satellite, Intelsat 19, to be located at 194 WL (166 EL). AMC 2 340.8WL SES applied to reassign AMC-2 from 355.02 WL (4.98 EL) to 340.8 WL (19.2 EL) where it will operate pursuant to Luxembourg ITU filings and will be flown in an inverted mode to provide Ku-band coverage in Southern Africa. -
Preparation of Papers for AIAA Journals
ASCEND 10.2514/6.2020-4000 November 16-18, 2020, Virtual Event ASCEND 2020 Cryogenic Fluid Management Technologies Enabling for the Artemis Program and Beyond Hans C. Hansen* and Wesley L. Johnson† NASA Glenn Research Center, Cleveland, Ohio, 44135, USA Michael L. Meyer‡ NASA Engineering Safety Center, Cleveland, Ohio, 44135, USA Arthur H. Werkheiser§ and Jonathan R. Stephens¶ NASA Marshall Space Flight Center, Huntsville, Alabama, 35808, USA NASA is endeavoring on an ambitious return to the Moon and eventually on to Mars through the Artemis Program leveraging innovative technologies to establish sustainable exploration architectures collaborating with US commercial and international partners [1]. Future NASA architectures have baselined cryogenic propulsion systems to support lunar missions and ultimately future missions to Mars. NASA has been investing in maturing CFM active and passive storage, transfer, and gauging technologies over the last decade plus primarily focused on ground development with a few small- scale microgravity fluid experiments. Recently, NASA created a Cryogenic Fluid Management (CFM) Technology Roadmap identifying the critical gaps requiring further development to reach a technology readiness level (TRL) of 6 prior to infusion to flight applications. To address the technology gaps the Space Technology Mission Directorate (STMD) strategically plans to invest in a diversified CFM portfolio approach through ground and flight demonstrations, collaborating with international partners, and leveraging Public Private Partnerships (PPPs) opportunities with US industry through Downloaded by Michele Dominiak on December 23, 2020 | http://arc.aiaa.org DOI: 10.2514/6.2020-4000 the Tipping Point and Announcement of Collaborative Opportunities (ACO) solicitations. Once proven, these system capabilities will enable the high performing cryogenic propellant systems needed for the Artemis Program and beyond. -
ORION ORION a to Z APOGEE to Break the Frangible Joints and Separate the Fairings, Three Parachutes
National Aeronautics and Space Administration ORION www.nasa.gov ORION A to Z APOGEE to break the frangible joints and separate the fairings, three parachutes. The next two parachutes will then VAN ALLEN RADIATION BELTS The term apogee refers to the point in an elliptical exposing the spacecraft to space. LAS - LAUNCH ABORT SYSTEM deploy and open. Once the spacecraft slows to around The Van Allen Belts are belts of plasma trapped by orbit when a spacecraft is farthest from the Earth. Orion’s Launch Abort System (LAS) is designed to 100 mph, the three main parachutes will then deploy the Earth’s magnetic field that shield the surface of During Exploration Flight Test-1, Orion’s flight path will GUPPY propel the crew module away from an emergency on using three pilot parachutes and slow the spacecraft the Earth from much of the radiation in space. During take it to an apogee of 3,600 miles. Just how high is The Super Guppy is a special airplane capable of the launch pad or during initial takeoff, moving the to around 20 mph for splashdown in the Pacific Ocean. Exploration Flight Test-1, Orion will pass within the Van that? A commercial airliner flies about 8 miles above transporting up to 26 tons in its cargo compartment crew away from danger. Orion’s LAS has three new When fully deployed, the canopies of three main Allen Radiation Belts and will spend more time in the the Earth’s surface, so Orion’s flight is 450 times farther measuring 25 feet tall, 25 feet wide, and 111 feet long. -
The Orbital-Hub: Low Cost Platform for Human Spaceflight After ISS
67th International Astronautical Congress (IAC), Guadalajara, Mexico, 26-30 September 2016. Copyright ©2016 by the International Astronautical Federation (IAF). All rights reserved. IAC-16, B3,1,9,x32622 The Orbital-Hub: Low Cost Platform for Human Spaceflight after ISS O. Romberga, D. Quantiusa, C. Philpota, S. Jahnkea, W. Seboldta, H. Dittusb, S. Baerwaldeb, H. Schlegelc, M. Goldd, G. Zamkad, R. da Costae, I. Retate, R. Wohlgemuthe, M. Langee a German Aerospace Center (DLR), Institute of Space Systems, Bremen, Germany, [email protected] b German Aerospace Center (DLR), Executive Board, Space Research and Technology, Cologne, Germany, c European Space Agency (ESA) Contractor, Johnson Space Center, Houston, USA, d Bigelow Aerospace, Las Vegas / Washington, USA, e Airbus DS, Bremen, Germany Abstract The International Space Station ISS demonstrates long-term international cooperation between many partner governments as well as significant engineering and programmatic achievement mostly as a compromise of budget, politics, administration and technological feasibility. A paradigm shift to use the ISS more as an Earth observation platform and to more innovation and risk acceptance can be observed in the development of new markets by shifting responsibilities to private entities and broadening research disciplines, demanding faster access by users and including new launcher and experiment facilitator companies. A review of worldwide activities shows that all spacefaring nations are developing their individual programmes for the time after ISS. All partners are basically still interested in LEO and human spaceflight as discussed by the ISECG. ISS follow-on activities should comprise clear scientific and technological objectives combined with the long term view on space exploration. -
International Docking System Standard (IDSS) Interface Definition Document (IDD)
IDSS IDD Revision E October 2016 International Docking System Standard (IDSS) Interface Definition Document (IDD) Revision E October 2016 IDSS IDD Revision E October 2016 This page intentionally left blank. IDSS IDD Revision E October 2016 REVISION AND HISTORY REV. DESCRIPTION PUB. DATE - Initial Release 09-21-10 A Revised, rearranged, and added text to nearly all sections of 05-13-11 document. Revised & renumbered figures. Added requirements on mechanical soft capture, soft capture sensors, HCS seals, hook stiffness, separation system, electrical bonding, environments, and materials. Added Docking Performance section, and Appendix A. B Document Hard Capture System parameter values, figure updates, 11-15-12 separation system force addition, editorial correction and updates. C Document the narrow ring Soft Capture System (SCS) geometric 11-20-13 parameters and update applicable figures. Added Appendix B on Magnetic Soft Capture. D Revision D is the first version of the document under NASA 08-04-15 configuration control and released by NASA ERU. Revision D includes the following DCNs: DCN 001 DCN 002 DCN 003 DCN 004C DCN 005 DCN 006 DCN 007 DCN 008A DCN 009B DCN 010 DCN 011 DCN 012 DCN 013 E Revision E includes the following DCNs: XX-XX-XX DCN 014 DCN 015A DCN 017 DCN 018 DCN 020 DCN 021 IDSS IDD Revision E October 2016 REVISION AND HISTORY REV. DESCRIPTION PUB. DATE DCN 022 DCN 023 DCN 024 DCN 025 DCN 027A DCN 029 DCN 032 DCN 033 DCN 037 DCN 038 DCN 039 IDSS IDD Revision E October 2016 This page intentionally left blank. -
The SKYLON Spaceplane
The SKYLON Spaceplane Borg K.⇤ and Matula E.⇤ University of Colorado, Boulder, CO, 80309, USA This report outlines the major technical aspects of the SKYLON spaceplane as a final project for the ASEN 5053 class. The SKYLON spaceplane is designed as a single stage to orbit vehicle capable of lifting 15 mT to LEO from a 5.5 km runway and returning to land at the same location. It is powered by a unique engine design that combines an air- breathing and rocket mode into a single engine. This is achieved through the use of a novel lightweight heat exchanger that has been demonstrated on a reduced scale. The program has received funding from the UK government and ESA to build a full scale prototype of the engine as it’s next step. The project is technically feasible but will need to overcome some manufacturing issues and high start-up costs. This report is not intended for publication or commercial use. Nomenclature SSTO Single Stage To Orbit REL Reaction Engines Ltd UK United Kingdom LEO Low Earth Orbit SABRE Synergetic Air-Breathing Rocket Engine SOMA SKYLON Orbital Maneuvering Assembly HOTOL Horizontal Take-O↵and Landing NASP National Aerospace Program GT OW Gross Take-O↵Weight MECO Main Engine Cut-O↵ LACE Liquid Air Cooled Engine RCS Reaction Control System MLI Multi-Layer Insulation mT Tonne I. Introduction The SKYLON spaceplane is a single stage to orbit concept vehicle being developed by Reaction Engines Ltd in the United Kingdom. It is designed to take o↵and land on a runway delivering 15 mT of payload into LEO, in the current D-1 configuration. -
A Researcher's Guide to Earth Observations
National Aeronautics and Space Administration A Researcher’s Guide to: Earth Observations This International Space Station (ISS) Researcher’s Guide is published by the NASA ISS Program Science Office. Authors: William L. Stefanov, Ph.D. Lindsey A. Jones Atalanda K. Cameron Lisa A. Vanderbloemen, Ph.D Cynthia A. Evans, Ph.D. Executive Editor: Bryan Dansberry Technical Editor: Carrie Gilder Designer: Cory Duke Published: June 11, 2013 Revision: January 2020 Cover and back cover: a. Photograph of the Japanese Experiment Module Exposed Facility (JEM-EF). This photo was taken using External High Definition Camera (EHDC) 1 during Expedition 56 on June 4, 2018. b. Photograph of the Momotombo Volcano taken on July 10, 2018. This active stratovolcano is located in western Nicaragua and was described as “the smoking terror” in 1902. The geothermal field that surrounds this volcano creates ideal conditions to produce thermal renewable energy. c. Photograph of the Betsiboka River Delta in Madagascar taken on June 29, 2018. This river is comprised of interwoven channels carrying sediment from the mountains into Bombetoka Bay and the Mozambique Channel. The heavy islands of built-up sediment were formed as a result of heavy deforestation on Madagascar since the 1950s. 2 The Lab is Open Orbiting the Earth at almost 5 miles per second, a structure exists that is nearly the size of a football field and weighs almost a million pounds. The International Space Station (ISS) is a testament to international cooperation and significant achievements in engineering. Beyond all of this, the ISS is a truly unique research platform. The possibilities of what can be discovered by conducting research on the ISS are endless and have the potential to contribute to the greater good of life on Earth and inspire generations of researchers to come. -
Why NASA's Planet-Hunting Astrophysics Telescope Is an Easy Budget Target, and What Defeat Would Mean PAGE 24
Q & A 12 ASTRONAUT’S VIEW 20 SPACE LAUNCH 34 Neil deGrasse Tyson A realistic moon plan SLS versus commercial SPECIAL REPORT SPACE DARK ENERGY DILEMMA Why NASA’s planet-hunting astrophysics telescope is an easy budget target, and what defeat would mean PAGE 24 APRIL 2018 | A publication of the American Institute of Aeronautics andd Astronautics | aeroaerospaceamerica.aiaa.orgerospaceamerica.aiaa.org 9–11 JULY 2018 CINCINNATI, OH ANNOUNCING EXPANDED TECHNICAL CONTENT FOR 2018! You already know about our extensive technical paper presentations, but did you know that we are now offering an expanded educational program as part of the AIAA Propulsion and Energy Forum and Exposition? In addition to our pre-forum short courses and workshops, we’ve enhanced the technical panels and added focused technical tutorials, high level discussion groups, exciting keynotes and more. LEARN MORE AND REGISTER TODAY! For complete program details please visit: propulsionenergy.aiaa.org FEATURES | April 2018 MORE AT aerospaceamerica.aiaa.org 20 34 40 24 Returning to Launching the Laying down the What next the moon Europa Clipper rules for space Senior research scientist NASA, Congress and We asked experts in for WFIRST? and former astronaut the White House are space policy to comment Tom Jones writes about debating which rocket on proposed United NASA’s three upcoming space what it would take to should send the probe Nations guidelines deliver the funds and into orbit close to this for countries and telescopes are meant to piece together political support for the Jovian moon. companies sending some heady puzzles, but the White Lunar Orbital Outpost- satellites and other craft House’s 2019 budget proposal would Gateway. -
Atlas Launch System Mission Planner's Guide, Atlas V Addendum
ATLAS Atlas Launch System Mission Planner’s Guide, Atlas V Addendum FOREWORD This Atlas V Addendum supplements the current version of the Atlas Launch System Mission Plan- ner’s Guide (AMPG) and presents the initial vehicle capabilities for the newly available Atlas V launch system. Atlas V’s multiple vehicle configurations and performance levels can provide the optimum match for a range of customer requirements at the lowest cost. The performance data are presented in sufficient detail for preliminary assessment of the Atlas V vehicle family for your missions. This guide, in combination with the AMPG, includes essential technical and programmatic data for preliminary mission planning and spacecraft design. Interface data are in sufficient detail to assess a first-order compatibility. This guide contains current information on Lockheed Martin’s plans for Atlas V launch services. It is subject to change as Atlas V development progresses, and will be revised peri- odically. Potential users of Atlas V launch service are encouraged to contact the offices listed below to obtain the latest technical and program status information for the Atlas V development. For technical and business development inquiries, contact: COMMERCIAL BUSINESS U.S. GOVERNMENT INQUIRIES BUSINESS INQUIRIES Telephone: (691) 645-6400 Telephone: (303) 977-5250 Fax: (619) 645-6500 Fax: (303) 971-2472 Postal Address: Postal Address: International Launch Services, Inc. Commercial Launch Services, Inc. P.O. Box 124670 P.O. Box 179 San Diego, CA 92112-4670 Denver, CO 80201 Street Address: Street Address: International Launch Services, Inc. Commercial Launch Services, Inc. 101 West Broadway P.O. Box 179 Suite 2000 MS DC1400 San Diego, CA 92101 12999 Deer Creek Canyon Road Littleton, CO 80127-5146 A current version of this document can be found, in electronic form, on the Internet at: http://www.ilslaunch.com ii ATLAS LAUNCH SYSTEM MISSION PLANNER’S GUIDE ATLAS V ADDENDUM (AVMPG) REVISIONS Revision Date Rev No. -
Get Ready to Launch! with NASA's Commercial Crew
Get ready to LAUNCH! with NASA’s Commercial Crew What is What are they Where are they Commercial Crew? launching? going? Boeing SpaceX CST-100 Starliner Crew Dragon National Aeronautics and Space Administration www.nasa.gov SP-2019-04-575-KSC Boeing Crew Flight Test SpaceX Demo 2 Nicole Aunapu Mann A NEW SPACE AGE Bob Behnken NASA Astronaut NASA’s Commercial Crew Program spacecraft and rockets will carry up to four astronauts NASA Astronaut Marine Corps Air Force Colonel and about 220 pounds of cargo to and from the International Space Station. Commercial Lieutenant Colonel crew will resume human spaceflight launches from the United States and provide the nation Flew aboard space shuttle Endeavour twice as a Mission Selected as an Astronaut in 2013, with two unique spacecraft, two human-rated rockets and the necessary ground support this is Nicole’s first spaceflight. Specialist, first on STS-123 and systems. NASA and our commercial partners, Boeing and SpaceX, are working together to then on STS-130. open access to low-Earth orbit. Chris Ferguson Boeing Astronaut BUILDING A NEW AMERICAN CAPABILITY Doug Hurley Navy Captain (retired) NASA’s Commercial Crew Program has been redefining space system development for NASA Astronaut Marine Corps Colonel Piloted space shuttle Atlantis low-Earth orbit by forming strong public-private partnerships with the aerospace industry to for STS-115, and commanded encourage innovation while maintaining NASA’s high safety standards and leveraging NASA’s (retired) shuttle Endeavour on STS-126 Piloted space shuttle Endeavor and Atlantis on STS-135, the 50 plus years of spaceflight experience. -
Emotional Intelligence
O L O R A D AerospaceO S T E M M A G A Z i N E Orion Lockheed Martin Colorado E.I. Emotional Intelligence Apollopalooza 2019 July \\022v “An Experience for Everyone” Colorado Aerospace STEM Magazine believes that the key to success in seeing higher graduation rates, improved test- Orion Test ing results, student inspiration, creativity, Lockheed Martin excitement and career satisfaction rests in the hands of the teacher. The example and inspiration of individual educators carries tremendous weight on a daily basis, great- ly impacting the quality and effectiveness of the classroom environment. STEM Teaching Career Hill Our mission: Encourage curiosity, Betsy investigation, inspiration, creativity, and innovation; the foundations of every career passion and career in the Colorado workforce. STEM Careers of Tomorrow Laron Walker Wayne Carley Publisher Unlimited distribution is permitted to everyone receiving Colorado Aerospace Emotional Intelligence STEM Magazine. Please feel free to share Pat Kozyra with educators, students, parents and in- terested individuals or organizations. Colorado Aerospace STEM Magazine strives to encourage the educator to better STEM Tools Delights understand the importance of STEM skills, Estes, Boucvalt, their use in every school subject, the need Bryce Cathy and ease of integration into curriculum Steve Curtis, and Bruce Camber and the urgency for students to embrace STEM. To find out more, please send your E-mail request to: Apollopalooza [email protected] Lockheed Martin Orionwww.lockheedmartin.com This month, NASA will test the Orion’s The AA-2 test will last less than three launch abort system (LAS) for the final minutes, but the mock-up module will time, and the team charged with keep- reach up to 31,000 feet at more than 1,000 ing the crew safe from injury during the mph (Mach 1.3) before the LAS fires and most severe phases of space flight will be separates the module from the booster.