NYK Line Westbound Sailing Schedule 30 June 2021

Total Page:16

File Type:pdf, Size:1020Kb

NYK Line Westbound Sailing Schedule 30 June 2021 Week 26 NYK Line Westbound Sailing Schedule 30 June 2021 Vessel Aquarius Leader Harmony Leader Pleiades Leader Grand Phoenix Leo Leader Triton Leader Antares Leader Garnet Leader Orion Leader Themis Leader Phoenix Leader Delphinus Leader Asteria Leader Vessel Voyage Number 035 070 085 070 088 083 077 101 026 023 032 031 007 Voyage Number Line ECX RTW RTW ECX ECX RTW RTW RTW ECX RTW RTW ECX RTW Line Ramp Capacity (T) 150 150 80 150 150 100 100 150 150 80 80 150 80 Ramp Capacity (T) Max Deck Height (M) 6.30 5.15 5.10 5.00 6.30 5.10 5.10 5.00 6.30 5.10 5.10 6.30 5.10 Max Deck Height (M) Flag Panama Bahamas Japan Panama Panama Panama Panama Bahamas Japan Japan Panama Japan Japan Flag Africa Africa Durban, South Africa 15-Apr --- 18-May --- 18-Jun ---- Durban, South Africa Mediterranean Sea Mediterranean Sea Beirut, Lebanon - 06-May --- 09-Jun - - - 11-Jul - - 20-Jul Beirut, Lebanon Mersin, Turkey ------------- Mersin, Turkey Derince, Turkey -- 18-May --- 17-Jun - - - 15-Jul - 24-Jul Derince, Turkey Piraeus, Greece - 10-May 20-May -- 15-Jun 19-Jun 22-Jun - 14-Jul 17-Jul - - Piraeus, Greece Livorno, Italy - 13-May - - - - - - - - - - 31-Jul Livorno, Italy Barcelona, Spain ------- 28-Jun ----- Barcelona, Spain North Continent North Continent Vigo, Spain 07-May --- 11-Jun - - - 14-Jul - - 06-Aug - Vigo, Spain Bristol, UK -- 28-May - - - - - - - 24-Jul - - Bristol, UK Antwerp, Belgium - - 02-Jun -- - 27-Jun - - - 26-Jul - 08-Aug Antwerp, Belgium Zeebrugge Bastenaken, Belgium 20-May 28-May 05-Jun 12-Jun 28-Jun 25-Jun 28-Jun 06-Jul 24-Jul 22-Jul 27-Jul 16-Aug 09-Aug Zeebrugge Bastenaken, Belgium Malmo, Sweden ------------- Malmo, Sweden Bremerhaven, Germany 18-May 21-May 11-Jun - 23-Jun 29-Jun 05-Jul 09-Jul 20-Jul 25-Jul 29-Jul 13-Aug 12-Aug Bremerhaven, Germany Emden, Germany - 25-May ---- 30-Jun -- 24-Jul --- Emden, Germany Southampton, UK 11-May 29-May 13-Jun - 15-Jun 26-Jun 07-Jul 11-Jul 17-Jul 28-Jul 01-Aug 09-Aug 15-Aug Southampton, UK USEC USEC Charleston, USA - - - - - - - TBC 21-Jul - - - - TBC 26-Aug Charleston, USA Houston, USA - - - - - 19-Jul via T/S - - - 19-Aug via T/S - - - Houston, USA ECCA ECCA Santo Domingo, Dominican Rep. ------------- Santo Domingo, Dominican Rep. Veracruz, Mexico - - - - - 22-Jul via T/S - - - 22-Aug via T/S - - - Veracruz, Mexico Cartagena P.Bahia, Colombia - 10-Jun - - - 12-Jul - - - - 15-Aug - - Cartagena P.Bahia, Colombia San Lorenzo, Honduras ---------- 20-Aug -- San Lorenzo, Honduras Manzanillo, Panama - - - - - 13-Jul - - - 10-Aug - - - Manzanillo, Panama ECSA & WCSA ECSA & WCSA Santos, Brasil --- 26-Jun --------- Santos, Brasil San Antonio, Chile 10-Jul - - 27-Jul 13-Aug - - - 17-Sep - - 30-Sep - San Antonio, Chile Iquique, Chile 13-Jul - - 29-Jul 18-Jul --- 13-Aug -- 06-Sep - Iquique, Chile Callao, Peru 17-Jul - - - 21-Jul --- 18-Aug -- 04-Sep - Callao, Peru USWC & WCCA USWC & WCCA Lazaro Cardenas, Mexico - 17-Jun - - - 19-Jul - - - - 23-Aug - - Lazaro Cardenas, Mexico San Diego, USA - 22-Jun - - - - 30-Jul - - 19-Aug - - - San Diego, USA Long Beach, USA - 24-Jun 07-Jul - - 23-Jul 29-Jul - - - 29-Aug - TBC 08-Sep Long Beach, USA Port Hueneme, USA - 23-Jun 06-Jul - - 24-Jul 28-Jul 05-Aug - 20-Aug 28-Aug - 09-Sep Port Hueneme, USA Far East Far East Tomakomai, Japan - - 21-Jul - - - - - - - 14-Sep - - Tomakomai, Japan Hitachi, Japan - - 23-Jul - - - 17-Aug 21-Aug - - 16-Sep - 24-Sep Hitachi, Japan Yokohama Daikoku, Japan - 10-Jul C3 24-Jul C3 - - 10-Aug C3 - 22-Aug C3 - CANCELLED TBC 17-Sep - - Yokohama Daikoku, Japan Toyohashi Jinno, Japan ------------- Toyohashi Jinno, Japan Schedule and calls are subject to change Call occurred - Unsequenced call NYK Westbound service can also offer to transhipment destinations via Manzanillo , such as but not limited to; Dominican Republic, Costa Rica, Honduras, Guatemala, Brazil, Argentina, Uruguay and Ecuador. For more information on the ports we serve please contact your local booking office. Details can be found below..
Recommended publications
  • Orion First Flight Test
    National Aeronautics and Space Administration orion First Flight Test NASAfacts Orion, NASA’s new spacecraft Exploration Flight Test-1 built to send humans farther During Orion’s flight test, the spacecraft will launch atop a Delta IV Heavy, a rocket built than ever before, is launching and operated by United Launch Alliance. While into space for the first time in this launch vehicle will allow Orion to reach an altitude high enough to meet the objectives for December 2014. this test, a much larger, human-rated rocket An uncrewed test flight called Exploration will be needed for the vast distances of future Flight Test-1 will test Orion systems critical to exploration missions. To meet that need, NASA crew safety, such as heat shield performance, is developing the Space Launch System, which separation events, avionics and software will give Orion the capability to carry astronauts performance, attitude control and guidance, farther into the solar system than ever before. parachute deployment and recovery operations. During the uncrewed flight, Orion will orbit The data gathered during the flight will influence the Earth twice, reaching an altitude of design decisions and validate existing computer approximately 3,600 miles – about 15 times models and innovative new approaches to space farther into space than the International Space systems development, as well as reduce overall Station orbits. Sending Orion to such a high mission risks and costs. altitude will allow the spacecraft to return to Earth at speeds near 20,000 mph. Returning
    [Show full text]
  • Concept Study of a Cislunar Outpost Architecture and Associated Elements That Enable a Path to Mars
    Concept Study of a Cislunar Outpost Architecture and Associated Elements that Enable a Path to Mars Presented by: Timothy Cichan Lockheed Martin Space [email protected] Mike Drever Lockheed Martin Space [email protected] Franco Fenoglio Thales Alenia Space Italy [email protected] Willian D. Pratt Lockheed Martin Space [email protected] Josh Hopkins Lockheed Martin Space [email protected] September 2016 © 2014 Lockheed Martin Corporation Abstract During the course of human space exploration, astronauts have travelled all the way to the Moon on short flights and have logged missions of a year or more of continuous time on board Mir and the International Space Station (ISS), close to Earth. However, if the long term goal of space exploration is to land humans on the surface of Mars, NASA needs precursor missions that combine operating for very long durations and great distances. This will allow astronauts to learn how to work in deep space for months at a time and address many of the risks associated with a Mars mission lasting over 1,000 days in deep space, such as the inability to abort home or resupply in an emergency. A facility placed in an orbit in the vicinity of the Moon, called a Deep Space Transit Habitat (DSTH), is an ideal place to gain experience operating in deep space. This next generation of in-space habitation will be evolvable, flexible, and modular. It will allow astronauts to demonstrate they can operate for months at a time beyond Low Earth Orbit (LEO). The DSTH can also be an international collaboration, with partnering nations contributing elements and major subsystems, based on their expertise.
    [Show full text]
  • Lunar Programs
    LUNAR PROGRAMS NASA is leading a sustainable return to the Moon Aerospace is partnered with NASA to with commercial and international partners to return humans to the Moon in every expand human presence in space and gather phase and journey, including the: new knowledge and opportunities. In 2017, Space › Planning and supporting the Policy Directive-1 called for a renewed emphasis on first lifecycle review of the commercial and international partnerships, return Gateway Initiative of humans to the Moon for long-term exploration and utilization followed by human missions to Mars. › Design, systems engineering and Aerospace is partnered with NASA in this endeavor integration, and operational concepts and is involved in every phase and journey. of the EVA system Artist’s conception of a gateway habitat. Image credit: NASA Humans must return to the moon for long-term › Ground testing of the NEXTStep deep exploration and utilization of deep space, but lunar space habitat module prototypes exploration is more than a stepping stone to Mars missions. The phased plan includes › Design and test of the Orion sending missions to the moon and cislunar space for exploration and study, and the capsule avionics construction of the Deep Space Gateway, a space station intended to orbit the moon. Aerospace provides support to these missions in areas such as systems engineering and integration, program management, and various subsystem expertise. Current Lunar Programs GATEWAY INITIATIVE NASA’s Gateway is conceived to be an exploration and science outpost in orbit around the moon that will enable human crewed missions to both cislunar space and the moon’s surface, meet scientific discovery and exploration objectives, and demonstrate and prove enabling technologies through commercial and international partnerships.
    [Show full text]
  • Orion Capsule Launch Abort System Analysis
    Orion Capsule Launch Abort System Analysis Assignment 2 AE 4802 Spring 2016 – Digital Design and Manufacturing Georgia Institute of Technology Authors: Tyler Scogin Michel Lacerda Jordan Marshall Table of Contents 1. Introduction ......................................................................................................................................... 4 1.1 Mission Profile ............................................................................................................................. 7 1.2 Literature Review ........................................................................................................................ 8 2. Conceptual Design ............................................................................................................................. 13 2.1 Design Process ........................................................................................................................... 13 2.2 Vehicle Performance Characteristics ......................................................................................... 15 2.3 Vehicle/Sub-Component Sizing ................................................................................................. 15 3. Vehicle 3D Model in CATIA ................................................................................................................ 22 3.1 3D Modeling Roles and Responsibilities: .................................................................................. 22 3.2 Design Parameters and Relations:............................................................................................
    [Show full text]
  • Space Sector Brochure
    SPACE SPACE REVOLUTIONIZING THE WAY TO SPACE SPACECRAFT TECHNOLOGIES PROPULSION Moog provides components and subsystems for cold gas, chemical, and electric Moog is a proven leader in components, subsystems, and systems propulsion and designs, develops, and manufactures complete chemical propulsion for spacecraft of all sizes, from smallsats to GEO spacecraft. systems, including tanks, to accelerate the spacecraft for orbit-insertion, station Moog has been successfully providing spacecraft controls, in- keeping, or attitude control. Moog makes thrusters from <1N to 500N to support the space propulsion, and major subsystems for science, military, propulsion requirements for small to large spacecraft. and commercial operations for more than 60 years. AVIONICS Moog is a proven provider of high performance and reliable space-rated avionics hardware and software for command and data handling, power distribution, payload processing, memory, GPS receivers, motor controllers, and onboard computing. POWER SYSTEMS Moog leverages its proven spacecraft avionics and high-power control systems to supply hardware for telemetry, as well as solar array and battery power management and switching. Applications include bus line power to valves, motors, torque rods, and other end effectors. Moog has developed products for Power Management and Distribution (PMAD) Systems, such as high power DC converters, switching, and power stabilization. MECHANISMS Moog has produced spacecraft motion control products for more than 50 years, dating back to the historic Apollo and Pioneer programs. Today, we offer rotary, linear, and specialized mechanisms for spacecraft motion control needs. Moog is a world-class manufacturer of solar array drives, propulsion positioning gimbals, electric propulsion gimbals, antenna positioner mechanisms, docking and release mechanisms, and specialty payload positioners.
    [Show full text]
  • The New Vision for Space Exploration
    Constellation The New Vision for Space Exploration Dale Thomas NASA Constellation Program October 2008 The Constellation Program was born from the Constellation’sNASA Authorization Beginnings Act of 2005 which stated…. The Administrator shall establish a program to develop a sustained human presence on the moon, including a robust precursor program to promote exploration, science, commerce and U.S. preeminence in space, and as a stepping stone to future exploration of Mars and other destinations. CONSTELLATION PROJECTS Initial Capability Lunar Capability Orion Altair Ares I Ares V Mission Operations EVA Ground Operations Lunar Surface EVA EXPLORATION ROADMAP 0506 07 08 09 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 LunarLunar OutpostOutpost BuildupBuildup ExplorationExploration andand ScienceScience LunarLunar RoboticsRobotics MissionsMissions CommercialCommercial OrbitalOrbital Transportation ServicesServices forfor ISSISS AresAres II andand OrionOrion DevelopmentDevelopment AltairAltair Lunar LanderLander Development AresAres VV and EarthEarth DepartureDeparture Stage SurfaceSurface SystemsSystems DevelopmentDevelopment ORION: NEXT GENERATION PILOTED SPACECRAFT Human access to Low Earth Orbit … … to the Moon and Mars ORION PROJECT: CREW EXPLORATION VEHICLE Orion will support both space station and moon missions Launch Abort System Orion will support both space stationDesigned and moonto operate missions for up to 210 days in Earth or lunar Designedorbit to operate for up to 210 days in Earth or lunar orbit Designed for lunar
    [Show full text]
  • The Apollo Moon Landings Were a Water- Shed Moment for Humanity
    Retracing the FOOTPRINTS Downloaded from http://asmedigitalcollection.asme.org/memagazineselect/article-pdf/143/3/49/6690390/me-2021-may4.pdf by guest on 24 September 2021 The Apollo Moon landings were a water- shed moment for humanity. NASA’s new program to return astronauts to the lunar surface could well be a steppingstone to the cosmos. By Michael Abrams he plaque left on the Sea of Tranquility by Neil Armstrong and Buzz Aldrin bore a simple mes- sage: “We came in peace for all Mankind.” But the Moon Race was part of a contest between nations and ideological systems and commanded military-scale budgets from both the United TStates and the Soviet Union. Today, more than 50 years after the Apollo 11 Moon landing (and nearly 30 since the end of the USSR), NASA is engaged in a new program to send astronauts back to the lunar surface. It ought to be a cinch, as our computers, design tools, and materials are radically more advanced than they were for the first trips to the Moon. But the demands of space travel haven’t changed at all—it is still a difficult and dangerous busi- ness—and dictate the shape of space exploration more than our high-tech gadgetry. Some elements of the new program, called Artemis, will seem like carbon copies of the 1960s roadmap to the Moon. The first step—which could happen as early as this November—will be to launch an unmanned crew capsule to lunar orbit, dipping to within 62 miles of the surface before returning to Earth and splashing down in the Pacific.
    [Show full text]
  • The Orion Spacecraft As a Key Element in a Deep Space Gateway
    The Orion Spacecraft as a Key Element in a Deep Space Gateway A Technical Paper Presented by: Timothy Cichan Lockheed Martin Space [email protected] Kerry Timmons Lockheed Martin Space [email protected] Kathleen Coderre Lockheed Martin Space [email protected] Willian D. Pratt Lockheed Martin Space [email protected] July 2017 © 2014 Lockheed Martin Corporation Abstract With the Orion exploration vehicle and Space Launch System (SLS) approaching operational status, NASA and the international community are developing the next generation of habitats to serve as a deep space platform that will be the first of its kind, a cislunar Deep Space Gateway (DSG). The DSG is evolvable, flexible, and modular. It would be positioned in the vicinity of the Moon and allow astronauts to demonstrate they can operate for months at a time well beyond Low Earth Orbit. Orion is the next generation human exploration spacecraft being developed by NASA. It is designed to perform deep space exploration missions, and is capable of carrying a crew of 4 astronauts on independent free-flight missions up to 21 days, limited only by consumables. Because Orion meets the strict requirements for deep space flight environments (reentry conditions, deep-space communications, safety, radiation, and life support for example) it is a key element in a DSG and is more than just a transportation system. Orion has the capability to act as the command deck of any deep space piloted vehicle. To increase affordability and reduce the complexity and number of subsystem functions the early DSG must be responsible for, the DSG can leverage these unique deep space qualifications of Orion.
    [Show full text]
  • Orion MPCV Spacecraft Systems
    National Aeronautics and Space Administration orion Quick Facts Orion is America’s next generation spacecraft that will take astronauts to exciting destinations never explored by humans. It will serve as the exploration vehicle that will carry the crew to distant planetary bodies, provide emergency abort capability, sustain the crew during space travel, and provide safe re-entry from deep space. facts Orion Summary Number of crew ............................................................................. 4 Crewed mission duration ............................................. 21-210 days Total change in velocity ..................................................... 4920 ft/s Gross liftoff weight .......................................................... 69,181 lbs Effective mass to orbit ..................................................... 50,231 lbs Launch Abort System – Emergency Crew Escape System During Launch Mass Properties NASA Dry mass/propellant ........................................................ 10,369 lbs Gross liftoff weight .......................................................... 16,125 lbs Crew Module – Crew and Cargo Transport Pressurized volume (total) .................................................. 690.6 ft3 Habitable volume (net) ........................................................... 316 ft3 Reaction control system (RCS) engine thrust ........... 160 lbf/engine Return payload ..................................................................... 220 lbs Mass Properties Dry mass/propellant .......................................................
    [Show full text]
  • PEANUTS and SPACE FOUNDATION the Beagle Has Landed!
    Reproducible Master PEANUTS and SPACE FOUNDATION The Beagle Has Landed! GRADE K – 5 OBJECTIVES PAGE 1 Students will: ö Read Snoopy, First Beagle on the Moon! and Shoot for the Moon, Snoopy! to give students some background knowledge. ö Work in teams to design a Doghouse Lunar Lander that will keep Snoopy and Woodstock safe on their journey back to the Moon! ö Test the Doghouse Lunar Landers designed by student teams in order to determine their effectiveness. ö Redesign the Doghouse Lunar Landers as necessary based on test results. SUGGESTED GRADE LEVELS K – 5 SUBJECT AREAS Engineering Design, Space Science TIMELINE 60 minutes NEXT GENERATION SCIENCE STANDARDS ö K-2-ETS1-1. Ask questions, make observations, and gather information about a situation people want to change to define a simple problem that can be solved through the development of a new or improved object or tool. ö 3-5-ETS.1-1. Define a simple design problem reflecting a need or a want that includes specified criteria for success and constraints on materials, time, or cost. ö 3-5-ETS.1-3. Plan and carry out fair tests in which variables are controlled and failure points are considered to identify aspects of a model or prototype that can be improved. 21st CENTURY ESSENTIAL SKILLS Critical Thinking/Problem Solving, Collaboration and Teamwork, Communication, Flexibility, Leadership, Initiative, Social Skills, Constructing Explanations, Obtaining/Evaluating/Communicating Ideas GRADE K – 5 ö PAGE 1 Reproducible Master PEANUTS and SPACE FOUNDATION The Beagle Has Landed! GRADE K – 5 BACKGROUND PAGE 2 ö According to NASA.gov, NASA has proudly shared an association with Charles M.
    [Show full text]
  • Orion Crew Exploration Vehicle and Service Module, (Eight Nozzles) Docked to a Conceptual Lunar Landing Craft, Orbit the Moon
    National Aeronautics and Space Administration Constellation Program: America’s Spacecraft for a New Generationf of Explorers a c t s The Orion Crew Exploration Vehicle NASA The Orion crew exploration vehicle and its service module orbit the moon with disc-shaped solar arrays tracking the sun to generate electricity. America will send a new generation of explorers Orion will be capable of carrying crew and cargo to the moon aboard NASA’s Orion crew exploration to the space station. It will be able to rendezvous vehicle. Making its first flights early in the next with a lunar landing module and an Earth departure decade, Orion is part of the Constellation Program stage in low-Earth orbit to carry crews to the moon to send human explorers back to the moon, and and, one day, to Mars-bound vehicles assembled then onward to Mars and other destinations in the in low-Earth orbit. Orion will be the Earth entry solar system. vehicle for lunar and Mars returns. Orion’s design will borrow its shape from the capsules of the past, A component of the Vision for Space Exploration, but takes advantage of 21st century technology Orion’s development is taking place in parallel in computers, electronics, life support, propulsion with missions to complete the International Space and heat protection systems. Station using the space shuttle before the shuttle is retired in 2010. Veteran Shape, State-of-the Art Technology the Orion spacecraft stays in lunar orbit. Once the astronauts’ Orion will be similar in shape to the Apollo spacecraft, lunar mission is complete, they will return to the orbiting but significantly larger.
    [Show full text]
  • Te11 As the Remnant of Nova Ori AD 483
    CELESTIAL OPTICAL TRANSIENTS FROM 532 BCE TO 2015 AD. Brian Warner Astrophysics, Cosmology and Gravity Centre, Department of Astronomy, University of Cape Town Introduction The earliest recorded optical transients occur in oriental records at least as early as 532 BCE (there is Modern identification a possible earlier record of a nova, c.1400 BCE, on Chinese oracle bones (Hsi 1958), but with insufficient detail to be of modern value). Among these are events now recognised as novae and supernovae, the most famous of which is the supernova of AD1054, with the Crab Nebula as Current understanding of the evolution of cataclysmic variable (CV) stars is that they are all close binary stars, with remnant. Within the past few years some of the ancient ordinary novae have been identified from mass transferring from (usually) a main sequence donor onto a white dwarf (Warner 1995). The build-up of their ejected shells or from the nature of the remnant binary star; more can be expected to be found hydrogen-rich material on the surface of the white dwarf leads eventually to a thermonuclear runaway, with with the upcoming all-sky surveys, such as LSST and Pan-STARRS. Here I discuss the current status expulsion of the accreted gas; intervals between such nova eruptions in theory should be ~ 104-5 y. Following the of the observations and the recent the discovery of an eclipsing dwarf nova, with an ejected shell, eruption, the heated white dwarf cools down, reducing irradiation of the donor and hence the mass transfer rate that is probably the remnant of the Chinese nova of AD 483.
    [Show full text]