Spacex CRS-4 National Aeronautics and Fourth Commercial Resupply Services Flight Space Administration
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Spacex Launch Manifest - a List of Upcoming Missions 25 Spacex Facilities 27 Dragon Overview 29 Falcon 9 Overview 31 45Th Space Wing Fact Sheet
COTS 2 Mission Press Kit SpaceX/NASA Launch and Mission to Space Station CONTENTS 3 Mission Highlights 4 Mission Overview 6 Dragon Recovery Operations 7 Mission Objectives 9 Mission Timeline 11 Dragon Cargo Manifest 13 NASA Slides – Mission Profile, Rendezvous, Maneuvers, Re-Entry and Recovery 15 Overview of the International Space Station 17 Overview of NASA’s COTS Program 19 SpaceX Company Overview 21 SpaceX Leadership – Musk & Shotwell Bios 23 SpaceX Launch Manifest - A list of upcoming missions 25 SpaceX Facilities 27 Dragon Overview 29 Falcon 9 Overview 31 45th Space Wing Fact Sheet HIGH-RESOLUTION PHOTOS AND VIDEO SpaceX will post photos and video throughout the mission. High-Resolution photographs can be downloaded from: http://spacexlaunch.zenfolio.com Broadcast quality video can be downloaded from: https://vimeo.com/spacexlaunch/videos MORE RESOURCES ON THE WEB Mission updates will be posted to: For NASA coverage, visit: www.SpaceX.com http://www.nasa.gov/spacex www.twitter.com/elonmusk http://www.nasa.gov/nasatv www.twitter.com/spacex http://www.nasa.gov/station www.facebook.com/spacex www.youtube.com/spacex 1 WEBCAST INFORMATION The launch will be webcast live, with commentary from SpaceX corporate headquarters in Hawthorne, CA, at www.spacex.com. The webcast will begin approximately 40 minutes before launch. SpaceX hosts will provide information specific to the flight, an overview of the Falcon 9 rocket and Dragon spacecraft, and commentary on the launch and flight sequences. It will end when the Dragon spacecraft separates -
Nanoracks External Platform (NREP) Interface Definition Document (IDD)
NanoRacks External Platform (NREP) Interface Definition Document (IDD) Doc No: NR-NREP-S0001 Revision: B © Copyright NanoRacks, LLC 2016. All Rights Reserved. NanoRacks External Platform IDD NREP Doc No: NR-NREP-S0001 Rev: B NanoRacks External Platform (NREP) IDD NREP Prepared by Steven Stenzel; Systems Engineer; Date Reviewed by Mark Rowley; Mechanical Design; Date Reviewed by Keith Tran; Operations Manager; Date Reviewed by Troy Guy; Avionics Manager; Date Reviewed by Bob Alexander; Safety; Date Reviewed by Susan Lufkin; Systems Engineer; Date Reviewed by Kirk Woellert; Payload Coordinator; Date Approved by Mike Lewis; Chief Technology Officer; Date NanoRacks External Platform IDD NREP Doc No: NR-NREP-S0001 Rev: B List of Revisions Revision Revision Date Revised By Revision Description - 3/16/2016 Steve Stenzel Initial Release A 4/20/2016 Steve Stenzel Update logo on cover page B 11/14/2016 C. Cummins Replace Proprietary Statement with a Copyright statement. NanoRacks External Platform IDD NREP Doc No: NR-NREP-S0001 Rev: B Table of Contents 1 Introduction 1 1.1 Purpose 1 1.2 Scope 1 1.3 Use 1 1.4 Exceptions 1 2 Acronyms, Definitions and Applicable Documents 2 3 NanoRacks NREP Overview 4 3.1 NREP Physical Descriptions 4 3.1.1 NREP-P Baseplate 4 3.1.2 NanoRacks External Plate - Payload 5 3.1.3 NREP Coordinate System 5 3.1.4 NREP General Dimensions 6 3.1.5 NREP Payload Configurations 6 3.1.6 NREP Baseplate Location Numbering System 7 3.2 NREP Operations Overview 10 3.2.1 Schedule 10 3.2.2 Ground Operations 11 3.2.2.1 Delivery to NanoRacks -
Exploration of the Moon
Exploration of the Moon The physical exploration of the Moon began when Luna 2, a space probe launched by the Soviet Union, made an impact on the surface of the Moon on September 14, 1959. Prior to that the only available means of exploration had been observation from Earth. The invention of the optical telescope brought about the first leap in the quality of lunar observations. Galileo Galilei is generally credited as the first person to use a telescope for astronomical purposes; having made his own telescope in 1609, the mountains and craters on the lunar surface were among his first observations using it. NASA's Apollo program was the first, and to date only, mission to successfully land humans on the Moon, which it did six times. The first landing took place in 1969, when astronauts placed scientific instruments and returnedlunar samples to Earth. Apollo 12 Lunar Module Intrepid prepares to descend towards the surface of the Moon. NASA photo. Contents Early history Space race Recent exploration Plans Past and future lunar missions See also References External links Early history The ancient Greek philosopher Anaxagoras (d. 428 BC) reasoned that the Sun and Moon were both giant spherical rocks, and that the latter reflected the light of the former. His non-religious view of the heavens was one cause for his imprisonment and eventual exile.[1] In his little book On the Face in the Moon's Orb, Plutarch suggested that the Moon had deep recesses in which the light of the Sun did not reach and that the spots are nothing but the shadows of rivers or deep chasms. -
NUCLEAR SAFETY LAUNCH APPROVAL: MULTI-MISSION LESSONS LEARNED Yale Chang the Johns Hopkins University Applied Physics Laboratory
ANS NETS 2018 – Nuclear and Emerging Technologies for Space Las Vegas, NV, February 26 – March 1, 2018, on CD-ROM, American Nuclear Society, LaGrange Park, IL (2018) NUCLEAR SAFETY LAUNCH APPROVAL: MULTI-MISSION LESSONS LEARNED Yale Chang The Johns Hopkins University Applied Physics Laboratory, 11100 Johns Hopkins Rd, Laurel, MD 20723 240-228-5724; [email protected] Launching a NASA radioisotope power system (RPS) trajectory to Saturn used a Venus-Venus-Earth-Jupiter mission requires compliance with two Federal mandates: Gravity Assist (VVEJGA) maneuver, where the Earth the National Environmental Policy Act of 1969 (NEPA) Gravity Assist (EGA) flyby was the primary nuclear safety and launch approval (LA), as directed by Presidential focus of NASA, the U.S. Department of Energy (DOE), the Directive/National Security Council Memorandum 25. Cassini Interagency Nuclear Safety Review Panel Nuclear safety launch approval lessons learned from (INSRP), and the public alike. A solid propellant fire test multiple NASA RPS missions, one Russian RPS mission, campaign addressed the MPF finding and led in part to two non-RPS launch accidents, and several solid the retrofit solid propellant breakup systems (BUSs) propellant fire test campaigns since 1996 are shown to designed and carried by MER-A and MER-B spacecraft have contributed to an ever-growing body of knowledge. and the deployment of plutonium detectors in the launch The launch accidents can be viewed as “unplanned area for PNH. The PNH mission decreased the calendar experiments” that provided real-world data. Lessons length of the NEPA/LA processes to less than 4 years by learned from the nuclear safety launch approval effort of incorporating lessons learned from previous missions and each mission or launch accident, and how they were tests in its spacecraft and mission designs and their applied to improve the NEPA/LA processes and nuclear NEPA/LA processes. -
Mission Overview
CRS Orb-1 Mission Mission Overview Overview Under the Commercial Resupply Services (CRS) contract with NASA, Orbital will provide approximately 20 metric tons of cargo to the International Space Station over the course of eight missions. Orb-1 is the first of those missions. The Orb-1 mission builds on the successful Commercial Orbital Transportation Services (COTS) demonstration mission conducted from September 18 to October 23, 2013. The Orb-1 flight will carry substantially more cargo (1465 kg vs. 700 kg) than the COTS mission, including several time-sensitive payloads and Cygnus’ first powered payload, the Commercial Generic Bioprocessing Apparatus (CGBA) from Bioserve. Mission Overview, Cont. Antares® The configuration of the Antares launch vehicle for the Orb-1 Mission is much the same as the two previous Antares flights with a CASTOR 30B second stage motor instead of the CASTOR 30 used previously. The first stage includes a core that contains the tanks for the liquid oxygen and kerosene, the first stage avionics, and two AJ26 rocket engines. The second stage consists of the CASTOR® 30B solid rocket motor, an avionics section containing the flight computer and guidance/ navigation/control functions, an interstage that connects the solid rocket motor to the first stage, the Cygnus spacecraft, and a fairing that encloses and protects the Cygnus spacecraft during ascent. Continued on Next Page Mission Overview, Cont. Cygnus™ The Cygnus spacecraft is composed of two elements, the Service Module (SM) and the Pressurized Cargo Module (PCM). The SM provides the propulsion, power, guidance, navigation and control, and other “housekeeping” services for the duration of the mission. -
Sentinel-1A Launch
SENTINEL-1A LAUNCH Arianespace’s seventh Soyuz launch from the Guiana Space Center will orbit Sentinel-1A, the first satellite in Europe’s Earth observation program, Copernicus. The European Space Agency (ESA) chose Thales Alenia Space to design, develop and build the satellite, as well as perform related tests. Copernicus is the new name for the European program previously known as GMES (Global Monitoring for Environment and Security), and is the European Commission’s second major space program, following Galileo. Copernicus is designed to give Europe continuous, independent and reliable access to Earth observation data. With the Soyuz, Ariane 5 and Vega launchers at the Guiana Space Center (CSG), Arianespace is the only launch services provider in the world capable of launching all types of payloads into all orbits, from the smallest to the largest geostationary satellites, from satellite clusters for constellations to cargo missions for the International Space Station (ISS). Arianespace sets the launch services standard for all operators, whether commercial or governmental, and guarantees access to space for scientific missions. Sentinel-1A is the 50th satellite with an Earth observation payload to be launched by Arianespace. Arianespace has seven more Earth observation missions in its order book, including four commercial missions (signed in 2013 and 2014). The Copernicus program is designed to give Europe complete independence in the acquisition and management of environmental data concerning our planet. ESA’s Sentinel programs comprise five satellite families: Sentinel-1, to provide continuity for radar data from ERS and Envisat. Sentinel-2 and Sentinel-3, dedicated to the observation of the Earth and its oceans. -
NANORACKS, LLC 555 Forge River Rd., Suite 120 Webster, TX 77598 4369 Phone: 832-632-7754 Fax: 832-575-4767
NANORACKS, LLC 555 Forge River Rd., Suite 120 Webster, TX 77598 4369 Phone: 832-632-7754 Fax: 832-575-4767 www.nanoracks.com Contract Administrator: Christopher Cummins Email Address: [email protected] Business Size: Small For more information on ordering from Federal Supply Schedules click on the FSS Schedules button at fss.gsa.gov. TABLE OF CONTENTS COMPANY OVERVIEW ...............................................................................................................3 CUSTOMER INFORMATION .......................................................................................................5 GSA PRICELIST .............................................................................................................................8 SERVICE DESCRIPTIONS ..........................................................................................................13 NanoRacks, LLC 47QRAA18D004R 2 About NanoRacks NanoRacks was founded on the vision of building a business ecosystem in space. Our company has been integrating customer payloads for the International Space Station since our first launch in 2010. As of February 2018, we have integrated and operated over 600 payloads on 32 launches to the Space Station, including Shuttle, Antares/Cygnus, Atlas V/Cygnus, Falcon/Dragon, HTV, ATV, and Soyuz. To date, we have also deployed over 200 satellites into low-Earth orbit. NanoRacks comes with a team that has real hands on experience with payloads ranging from professional grade research to DOD to high school experiments. NanoRacks -
Nanoracks Completes First Mission on India's Polar Satellite Launch
NanoRacks Completes First Mission on India’s Polar Satellite Launch Vehicle, Launches Spire’s 100th Satellite NanoRacks, the world’s leading commercial space station company, completed its first CubeSat deployment mission on India Space Research Organization’s (ISROs) Polar Satellite Launch Vehicle (PSLV). This mission was brokered on behalf of Spire, which now has four more of their LEMUR 3U CubeSats in orbit. Notably, this mission included the launch of Spire’s 100th Lemur satellite. “Congratulations to Spire on this incredible achievement,” says NanoRacks Payloads Director, Conor Brown. “Spire has been with us from the beginning, not just as a customer but as a partner, working alongside us to pioneer new capabilities across platforms on the Space Station, Cygnus, and now finally on the PSLV. Spire’s diversified launch approach and willingness to embrace new technologies continues to foster the marketplace and we couldn’t be more excited to have deployed the 100th satellite!” NanoRacks announced sun synchronous polar orbit launch opportunities after receiving significant customer demand and strong feedback for the customer support that the Company offers. Polar orbit offerings come in addition to NanoRacks’ proven success in small satellite deployments, having deployed over 230 satellites to date. Spire’s CubeSats offer data and analytics for parts of the world where collecting data is notoriously difficult, tracking ships, planes, and weather in remote regions which often go unmonitored. To date, of the 100 satellites Spire has launched, 37 were on NanoRacks missions from the Space Station, the Cygnus Spacecraft, and now PSLV. “Spire is excited to share this milestone with NanoRacks,” says Jenny Barna, Spire’s Director of Launch. -
Cubesat-Services.Pdf
Space• Space Station Station Cubesat CubesatDeployment Services Deployment Services NanoRacks Cubesat Deployer (NRCSD) • 51.6 degree inclination, 385-400 KM • Orbit lifetime 8-12 months • Deployment typically 1-3 months after berthing • Soft stowage internal ride several times per year Photo credit: NASA NRCSD • Each NRCSD can deploy up to 6U of CubeSats • 8 NRCSD’s per airlock cycle, for a total of 48U deployment capability • ~2 Air Lock cycles per mission Photo Credit: NanoRacks LLC Photo credit: NASA 2. Launched by ISS visiting vehicle 3. NRCSDs installed by ISS Crew 5. Grapple by JRMS 4. JEM Air Lock depress & slide 6. NRCSDs positioned by JRMS table extension 1. NRCSDs transported in CTBs 7. Deploy 8. JRMS return NRCSD-MPEP stack to slide table; 9. ISS Crew un-install first 8 NRCSDs; repeat Slide table retracts and pressurizes JEM air lock install/deploy for second set of NRCSDs NanoRacks Cubesat Mission (NR-CM 3 ) • Orbital Sciences CRS-1 (Launched Jan. 9, 2014) • Planet Labs Flock1A, 28 Doves • Lithuanian Space Assoc., LitSat-1 • Vilnius University & NPO IEP, LituanicaSat-1 • Nanosatisfi, ArduSat-2 • Southern Stars, SkyCube • University of Peru, UAPSat-1 Photo credit: NASA Mission Highlights Most CubeSats launched Two countries attain in a single mission space-faring status World’s largest remote Kickstarter funding sensing constellation • NR-CM3 • Orbital Science CRS-1, Launch Jan 9, 2014 • Air Lock Cycle 1, Feb 11-15, 2014 Dove CubeSats • Deployers 1-8 (all Planet Labs Doves) Photo credit: NASA • NR-CM3 • Orbital Science CRS-1, -
ISS Launch Schedule
ISS Launch Schedule February 17, 2015 March 27, 2015 April 8, 2015 April 8, 2015 June 13, 2015 August 6, 2015 Progress 58 Soyuz 42 SpaceX CRS-6 Progress 59 SpaceX CRS-7 Progress 60 October 22, 2015 September 1, 2015 December 5, 2015 August 17, 2015 September 1, 2015 September 2, 2015 October 15, 2015 Progress 61 Soyuz 45 SpaceX CRS-9 HTV-5, ISS Resupply Soyuz 44 SpaceX CRS-8 Orb-4, ISS Resupply Manifesting and Scheduling- External • Major Challenges • Demand for upmass exceeds current availability • All manifest requests subject to ISS Program Prioritization • Difficultly planning future missions when short-term allocation is unknown • Orbital ATK returning to flight will provide relief • Increased demand of JEM Airlock • Will take increased coordination between NanoRacks, JAXA, and NASA to maximize utilization • Various hardware requires different slide-table adaptors; up to 1 month to reconfigure airlock • Safety Requirements • Some requirements outdated/not clearly defined • Vibration testing Manifesting and Scheduling- CubeSats Lessons Learned • Some COTS CubeSat components need to be altered to comply with ISS flight safety standards • 3 deployment switches • Battery Protection Circuits • Early Coordination • PSRP needs significant time to review, particularly if hazards of payload are non-standard • Custom timelines for payloads with unique hazards (i.e., propulsion, biologicals, etc.) Manifesting and Scheduling- Internal • Major Challenges • Crew time • Availability of astronaut time to support experiments on orbit • Varying levels of technical capabilities • Helping all types of customers to get experiments to the ISS • Changing launch schedules • As well as predicting in advance who will be ready for what flight Manifesting and Scheduling- Internal Lessons Learned • Early support for new customers • Safety and ops involvement earlier in the timeline • Understanding of crew time needs and use of streamlining strategies . -
Securing Japan an Assessment of Japan´S Strategy for Space
Full Report Securing Japan An assessment of Japan´s strategy for space Report: Title: “ESPI Report 74 - Securing Japan - Full Report” Published: July 2020 ISSN: 2218-0931 (print) • 2076-6688 (online) Editor and publisher: European Space Policy Institute (ESPI) Schwarzenbergplatz 6 • 1030 Vienna • Austria Phone: +43 1 718 11 18 -0 E-Mail: [email protected] Website: www.espi.or.at Rights reserved - No part of this report may be reproduced or transmitted in any form or for any purpose without permission from ESPI. Citations and extracts to be published by other means are subject to mentioning “ESPI Report 74 - Securing Japan - Full Report, July 2020. All rights reserved” and sample transmission to ESPI before publishing. ESPI is not responsible for any losses, injury or damage caused to any person or property (including under contract, by negligence, product liability or otherwise) whether they may be direct or indirect, special, incidental or consequential, resulting from the information contained in this publication. Design: copylot.at Cover page picture credit: European Space Agency (ESA) TABLE OF CONTENT 1 INTRODUCTION ............................................................................................................................. 1 1.1 Background and rationales ............................................................................................................. 1 1.2 Objectives of the Study ................................................................................................................... 2 1.3 Methodology -
NRCSD) Interface Definition Document (IDD
NanoRacks CubeSat Deployer (NRCSD) Interface Definition Document (IDD) NRCSD Doc No: NR-NRCSD-S0003 Revision: - NANORACKS PROPRIETARY RIGHTS ARE INCLUDED HEREIN. RECIPIENT AGREES THAT NEITHER THIS DOCUMENT NOR THE INFORMATION DISCUSSED HEREIN NOR ANY PART THEREOF SHALL BE REPRODUCED OR DISCLOSED TO OTHERS. NanoRacks CubeSat Deployer IDD NRCSD Doc No: NR-NRCSD-S0003 Rev: - NanoRacks CubeSat Deployer (NRCSD) Interface Definition Document (IDD) NRCSD Prepared by Tristan Prejean; Mission Manager; Date Reviewed by Henry Martin; Senior Mission Manager; Date Reviewed by Conor Brown; External Payloads Manager; Date Reviewed by Troy Guy; Electrical Engineer; Date Reviewed by Teresa Freund; Safety Engineer; Date Approved by Mike Lewis; Chief Technology Officer; Date NanoRacks CubeSat Deployer IDD NRCSD Doc No: NR-NRCSD-S0003 Rev: - List of Revisions Revision Revision Date Revised By Revision Description - 5/29/2018 Tristan Prejean Initial Release NanoRacks CubeSat Deployer IDD NRCSD Doc No: NR-NRCSD-S0003 Rev: - Table of Contents 1 Introduction 6 1.1 Purpose 6 1.2 Scope 6 1.3 Usage 6 1.4 Exceptions 6 2 Acronyms, Definitions, and Applicable Documents 7 3 NanoRacks CubeSat Deployer System Overview 10 3.1 NRCSD Overview and Payload Capacity 10 3.2 NRCSD Coordinate System 10 3.3 NRCSD Design Features 11 3.4 NRCSD Operations Overview 12 3.4.1 Schedule 12 3.4.2 Ground Operations 13 3.4.3 On-Orbit Environments, Interfaces, and Operations 15 4 Payload Interface Requirements 21 4.1 Structural and Mechanical Systems Interface Requirements 21 4.1.1 CubeSat