NASA's New Direct Electric Docking System Supporting ISS and Future
Total Page:16
File Type:pdf, Size:1020Kb
Load more
Recommended publications
-
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. -
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 International Space Station
The International Space Station Aeronautics and Space Engineering Board April 2015 Sam Scimemi Director, International Space Station NASA Headquarters NASA’s and America’s goals onboard the Station Enable long duration human spaceflight beyond LEO Enable a commercial market in LEO Advance benefits to humanity through research Basis for international HSF exploration partnerships 2 Where we are Today In January 2014 the Administration extended the life of ISS at least to 2024 Each International Partner is working within their own policy framework to determine ISS future beyond 2020 Begun 1 year crew expedition and associated long duration human performance research Together with CASIS, NASA is expanding the commercial demand for micro-gravity research and LEO access ISS has become an important space and earth science platform expanding our knowledge of our home planet and the universe Commercial transportation development and operations for ISS is having a significant influence on the aerospace industry; considering the next commercial activity in LEO 3 3 4/ 4 4 The Future of Human Space Exploration NASA’s Building Blocks to Mars Expanding capabilities at an asteroid redirected to lunar orbit Exploring Mars and other deep U.S. companies space provide destinations affordable access to low Earth orbit Learning the fundamentals aboard the Traveling beyond low Earth International orbit with the Space Launch Space Station System rocket and Orion crew capsule Missions: 6 to 12 months Missions: 1 month up to 12 months Missions: 2 to 3 years Return: -
The Messenger Spacecraft Power System Design and Early Mission Performance
THE MESSENGER SPACECRAFT POWER SYSTEM DESIGN AND EARLY MISSION PERFORMANCE G. Dakermanji, C. Person, J. Jenkins, L. Kennedy, D. Temkin Johns Hopkins University Applied Physics Laboratory, 11100 Johns Hopkins Rd., Laurel, Maryland, 20723-6099, USA Email: [email protected] ABSTRACT The MESSENGER (MErcury Surface, Space ENvironment, GEochemistry, and Ranging) spacecraft was launched on August 3, 2004. The spacecraft will be inserted into Mercury orbit in March 2011 for one year of orbital operation. During the mission, the spacecraft distance to the Sun will vary between approximately 1 and 0.3 Astronomical Units (AU), imposing severe requirements on the spacecraft thermal and power systems design. The spacecraft is maintained behind a sunshade. The two single-axis, gimbaled solar array panels are designed to withstand the expected high temperatures. A peak power tracking system has been selected to allow operation over the widely varying solar array I-V curves. In order to reduce cost and risk while increasing the likelihood of mission success, the approach taken in the power system design, including the solar arrays, was to use conventional design, materials, and fabrication techniques. 1. MISSION DESCRIPTION a. Launch Configuration Sunshade MESSENGER (MErcury Surface, Space ENvironment, GEochemistry, and Ranging), shown in Fig. 1, is a Battery NASA Discovery Program spacecraft designed and built by the Johns Hopkins University Applied Physics Laboratory (APL). It will orbit the planet Mercury for one Earth year of orbital operation. Most of what is known about Mercury comes from the Mariner 10 spacecraft. Using three flybys, Mariner 10 was able to map about 45% of the planet surface during a one-year period between 1974 and 1975. -
Constellation Program Overview
Constellation Program Overview October 2008 hris Culbert anager, Lunar Surface Systems Project Office ASA/Johnson Space Center Constellation Program EarthEarth DepartureDeparture OrionOrion -- StageStage CrewCrew ExplorationExploration VehicleVehicle AresAres VV -- HeavyHeavy LiftLift LaunchLaunch VehicleVehicle AltairAltair LunarLunar LanderLander AresAres II -- CrewCrew LaunchLaunch VehicleVehicle Lunar Capabilities Concept Review EstablishedEstablished Lunar Lunar Transportation Transportation EstablishEstablish Lunar Lunar Surface SurfaceArchitecturesArchitectures ArchitectureArchitecture Point Point of of Departure: Departure: StrategiesStrategies which: which: Satisfy NASA NGO’s to acceptable degree ProvidesProvides crew crew & & cargo cargo delivery delivery to to & & from from the the Satisfy NASA NGO’s to acceptable degree within acceptable schedule moonmoon within acceptable schedule Are consistent with capacity and capabilities ProvidesProvides capacity capacity and and ca capabilitiespabilities consistent consistent Are consistent with capacity and capabilities withwith candidate candidate surface surface architectures architectures ofof the the transportation transportation systems systems ProvidesProvides sufficient sufficient performance performance margins margins IncludeInclude set set of of options options fo for rvarious various prioritizations prioritizations of cost, schedule & risk RemainsRemains within within programmatic programmatic constraints constraints of cost, schedule & risk ResultsResults in in acceptable -
ISS - Enabling Exploration Through Docking Standards
https://ntrs.nasa.gov/search.jsp?R=20110016704 2019-11-17T11:14:50+00:00Z ISS - Enabling Exploration through Docking Standards ISSMars-DC Conference C.A. Hatfield Docking Systems Manager April 2011 International Space Station Program Standards – Enabling Exploration • Connecting spacecraft from different nations has required unique development and expensive integration and test – Apollo-Soyuz Test Project – International Space Station • Expansion of spacefaring nations (and non-governmental entities) will compound this issue in the future – Exploration cooperation could be much easier with internationally accepted interface standards • One of the key elements involved in mating dissimilar spacecraft is docking systems – Enabling dissimilar spacecraft mating for crew and cargo exchange – Enabling spacecraft assembly (e.g., APAS joining USOS and Russian Segments on ISS) Page No. 2 C.A. Hatfield ISSMars Conference April 2011 Enabling a Docking Standard • The ISS partnership has developed an International Docking System Standard (IDSS) – An expanded version is expected to be approved in the second quarter 2011 by the ISS partnership – The latest version of IDSS can be found at http://internationaldockingstandard.com/ • It is expected that several versions of IDSS compatible docking systems will eventual emerge – Both NASA and ESA are currently developing systems • NASA will install an adapter to use this standard on the U.S. segment of ISS beginning in 2015 – The two new adapters will replace existing APAS adapters used by the Space Shuttle Page No. 3 C.A. Hatfield ISSMars Conference April 2011 Docking System Early Design Progression Apollo Probe Cone Apollo Soyuz – the first androgynous system Russian Probe Cone (No scale is implied between figures) Page No. -
Space Communications and Navigation (Scan) Testbed
National Aeronautics and Space Administration Space Communication and Navigation Testbed: Communications Technology for Exploration Richard Reinhart NASA Glenn Research Center July 2013 ISS Research and Development Conference Sponsored by Space Communication and Navigation Program Titan Lunar Neptune Relay Satellite Saturn Uranus Pluto LADEE Charon Jupiter Near Earth Optical Relay Pathfinder Mars NISNNISN MCC MOCs SCaN2023202520182015 Add: Services Provide: ••IntegratedEnhancedDeepIntegratedStandard Space service-basedServicesOptical Network Optical Initial Management Initial and architectureCapability Interfaces Capability (INM) ••SpaceDeepSpaceIntegratedDelay Space internetworking InternetworkingTolerant Service Optical Networking Execution Relay (DTN throughout Pathfinder and (ISE) IP) Solar Venus Deep Space ••InternationalLunarSystemSpaceDeep SpaceRelay Internetworking interoperability Satellite Antenna Initial Array Capability Antenna Optical Relay ••AssuredSignificantOpticalLunar Optical Ground safety Increases and Pathfinder Terminal security in Bandwidth (LADEE) of missions Array Pathfinder ••SignificantRetirementNearTDRS Earth K, L increases Optical of Aging Initial RFin bandwidth Systems Capability Sun Mercury • TDRSIncreased M,N microwave link data rates • Lunar Relay Payload (potential) 2 Microwave Links Optical Links NISN Next Generation Communication and Navigation Technology – Optical Communications – Antenna Arraying Technology – Receive and Transmit – Software Defined Radio – Advanced Antenna Technology – Spacecraft RF -
Master's Thesis
MASTER'S THESIS On-Orbit Servicing Satellite Docking Mechanism Modeling and Simulation Karim Bondoky 2015 Master of Science (120 credits) Space Engineering - Space Master Luleå University of Technology Department of Computer Science, Electrical and Space Engineering On-Orbit Servicing Satellite Docking Mechanism Modeling and Simulation by Karim Bondoky A thesis submitted in partial fulfilment for the degree of Masters of Science in Space Science and Technology Supervisors: Eng. Sebastian Schwarz Airbus Defence and Space Prof. Dr. Sergio Montenegro University of W¨urzburg Dr. Johnny Ejemalm Lule˚aUniversity of Technology October 2014 Declaration of Authorship I, Karim Bondoky, declare that this thesis titled, `On-Orbit Servicing Satellite Docking Mechanism Modeling and Simulation' and the work presented in it are my own. I confirm that: This work was done wholly while in candidature for a research degree at both Universities. Where any part of this thesis has previously been submitted for a degree or any other qualification, this has been clearly stated. Where I have consulted the published work of others, this is always clearly at- tributed. Where I have quoted from the work of others, the source is always given. With the exception of such quotations, this thesis is entirely my own work. I have acknowledged all main sources of help. Signed: Date: 15.10.2014 i Abstract Docking mechanism of two spacecraft is considered as one of the main challenging as- pects of an on-orbit servicing mission. This thesis presents the modeling, analysis and software simulation of one of the docking mechanisms called "probe and drogue". The aim of this thesis is to model the docking mechanism, simulate the docking process and use the results as a reference for the Hardware-In-the-Loop simulation (HIL) of the docking mechanism, in order to verify and validate it. -
Silencing Nasa's Space Shuttle Crawler
SILENCING NASA’S SPACE SHUTTLE CRAWLER TRANSPORTER R. MacDonalda, C. Faszerb, and R. Margasahayamc aNoise Solutions Inc., #310 605 – 1st Street SW, Calgary, Alberta, Canada T2P 3S9 bFaszer Farquharson & Associates, #304 605 – 1st Street SW, Calgary, Alberta, Canada T2P 3S9 cNASA, John F. Kennedy Space Center, Florida, United States of America 32899 [email protected]; [email protected]; [email protected] Abstract. The crawler transporter (CT) is the world’s second largest known tracked vehicle, weighing 6 million pounds with a length of 131 feet and a width of 113 feet. The Kennedy Space Center (KSC) has two CTs that were designed and built for the Apollo program in the 1960’s, maintained and retrofitted for use in the Space Shuttle program. As a key element of the Space Shuttle ground systems, the crawler transports the entire 12-million-pound stack comprising the orbiter, the mobile launch platform (MLP), the external tank (ET), and the solid rocket boosters (SRB) from the Vehicle Assembly Building (VAB) to the launch pad. This rollout, constituting a 3.5 to 5.0 mile journey at a top speed of 0.9 miles-per-hour, requires over 8 hours to reach either Launch Complex 39A or B. This activity is only a prelude to the spectacle of sound and fury of the Space Shuttle launch to orbit in less than 10 minutes and traveling at orbital velocities of Mach 24. This paper summarizes preliminary results from the Crawler Transporter Sound Attenuation Study, encompassing test and engineering analysis of significant sound sources to measure and record full frequency spectrum and intensity of the various noise sources and to analyze the potential for noise mitigation. -
588168 Amendment No. 56 NASA Glenn Research Center, License
NRC FORM 374 PAGE 1 OF 7 PAGES U.S. NUCLEAR REGULATORY COMMISSION Amendment No. 56 MATERIALS LICENSE Pursuant to the Atomic Energy Act of 1954, as amended, the Energy Reorganization Act of 1974 (Public Law 93-438), and Title 10, Code of Federal Regulations, Chapter I, Parts 30, 31, 32, 33, 34, 35, 36, 37, 39, 40, 70 and 71, and in reliance on statements and representations heretofore made by the licensee, a license is hereby issued authorizing the licensee to receive, acquire, possess, and transfer byproduct, source, and special nuclear material designated below; to use such material for the purpose(s) and at the place(s) designated below; to deliver or transfer such material to persons authorized to receive it in accordance with the regulations of the applicable Part(s). This license shall be deemed to contain the conditions specified in Section 183 of the Atomic Energy Act of 1954, as amended, and is subject to all applicable rules, regulations, and orders of the Nuclear Regulatory Commission now or hereafter in effect and to any conditions specified below. Licensee In accordance with letter dated 4. Expiration Date: March 31, 2025 March 28, 201 1. National Aeronautics & Space Administration R John H. Glenn Research Center 5. Docket No.: 030-05626 2. 21000 Brookpark Road Reference No.: Mailstop 6-4 Cleveland, OH 44135 6. Byproduct, source, 9. Authorized use and/or special nuclear material A. Any byproduct material A. Activation ~ucts A. For research and development as between atomic numbers described in 10 CFR 30.4. Possession 3 and 83 incident to the radiological characterization surveys of a shut-down cyclotron. -
10 Things to Know About NASA's Glenn Research Center
National Aeronautics and Space Administration 10 Things to Know About NASA’s Glenn Research Center 1. NASA Glenn’s economic impact in Ohio exceeds $1.4 billion per year. According to an economic impact study by Cleveland State University’s Center for Economic Development, Glenn generates over $700 million annually in economic activity and creates over 7,000 jobs. NASA Glenn also generates nearly $500 million in labor income and approximately $120 million in tax revenue per year. 2. Glenn scientists and engineers are prolific inventors. The research center holds more than 725 patents and has won over 120 R&D 100 Awards, also known as the Oscars of innovation. That’s more than any other NASA center. Glenn strives to increase private sector revenue and contribute to private sector job growth by licensing its inventions. 3. Every U.S. aircraft has NASA Glenn technology on board. NASA is with you when you fly. Today’s commercial airliners are safer, quieter and more fuel efficient because of NASA Glenn technology. Glenn advancements such as ice detection and air traffic control systems have made flying safer. Glenn jet engine combustors have resulted in more efficient aircraft engines, and Glenn developed nozzle chevrons are used to make the Boeing 787 Dreamliner and new 737 MAX quieter. 4. Glenn is transforming aviation by developing revolutionary technologies for aircraft and the national airspace system. Glenn is working to dramatically improve efficiency, reduce costs and noise, and maintain safety in crowded skies. The center leads the agency’s effort to develop hybrid electric propulsion systems for commercial passenger aircraft. -
Complete List of Contents
Complete List of Contents Volume 1 Cape Canaveral and the Kennedy Space Center ......213 Publisher’s Note ......................................................... vii Chandra X-Ray Observatory ....................................223 Introduction ................................................................. ix Clementine Mission to the Moon .............................229 Preface to the Third Edition ..................................... xiii Commercial Crewed vehicles ..................................235 Contributors ............................................................. xvii Compton Gamma Ray Observatory .........................240 List of Abbreviations ................................................. xxi Cooperation in Space: U.S. and Russian .................247 Complete List of Contents .................................... xxxiii Dawn Mission ..........................................................254 Deep Impact .............................................................259 Air Traffic Control Satellites ........................................1 Deep Space Network ................................................264 Amateur Radio Satellites .............................................6 Delta Launch Vehicles .............................................271 Ames Research Center ...............................................12 Dynamics Explorers .................................................279 Ansari X Prize ............................................................19 Early-Warning Satellites ..........................................284