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NASA Armstrong X-Press April 2020
National Aeronautics and Space Administration Volume 62 Number 3 April 2020 AFRC2020-0058-032 NASA/Carla Thomas NASA Armstrong engineer Mike Buttigieg works on an oxygen hood system prototype worn by Dr. Daniel Khodabakhsh from the Antelope Valley Hospital. The hood is designed to help coronavirus patients who don’t yet need a ventilator, but who are experiencing breathing troubles. The hood forces oxygen into patients with mild coronavirus symptoms, minimizing the likelihood that the patient will need to use a ventilator. Lending a hand Center assists community COVID-19 response www.nasa.gov/ Return to center plans begin, page 2 X-Press April 2020 Successful partnership By Teresa Whiting next week at TSC’s Faith Facility in NASA Armstrong Public Affairs Mojave. NASA Armstrong has joined “I’ve been inspired by the forces with an Antelope Valley teamwork shown by the Antelope task force to build medical devices Valley task force in response to the to help patients with coronavirus. challenge of COVID-19. Now more Armstrong partnered with than ever, it is crucial that we share Antelope Valley Hospital, knowledge, skills and collaborate,” Lancaster, Virgin Galactic, said Virgin Galactic CEO George The Spaceship Company and Whitesides. “By producing several Antelope Valley College to innovative health solutions for develop innovative ideas to solve regional hospitals over a few possible shortages of critical weeks, we are protecting health medical equipment. care workers on the front lines “NASA is more than scientists, while improving patient care. It is engineers and explorers. We truly showing the best of American are neighbors and members of public-private cooperation.” AFRC2020-0059-024 NASA/Carla Thomas communities across the country,” The device, developed byNASA engineer Mike Buttigieg works on the Aerospace Valley Positive Pres- said NASA Administrator Jim NASA engineer Mike Buttigieg, sure Helmet, a device successfully tested by Antelope Valley Hospital doctors. -
Space Launch System (Sls) Motors
Propulsion Products Catalog SPACE LAUNCH SYSTEM (SLS) MOTORS For NASA’s Space Launch System (SLS), Northrop Grumman manufactures the five-segment SLS heavy- lift boosters, the booster separation motors (BSM), and the Launch Abort System’s (LAS) launch abort motor and attitude control motor. The SLS five-segment booster is the largest solid rocket motor ever built for flight. The SLS booster shares some design heritage with flight-proven four-segment space shuttle reusable solid rocket motors (RSRM), but generates 20 percent greater average thrust and 24 percent greater total impulse. While space shuttle RSRM production has ended, sustained booster production for SLS helps provide cost savings and access to reliable material sources. Designed to push the spent RSRMs safely away from the space shuttle, Northrop Grumman BSMs were rigorously qualified for human space flight and successfully used on the last fifteen space shuttle missions. These same motors are a critical part of NASA’s SLS. Four BSMs are installed in the forward frustum of each five-segment booster and four are installed in the aft skirt, for a total of 16 BSMs per launch. The launch abort motor is an integral part of NASA’s LAS. The LAS is designed to safely pull the Orion crew module away from the SLS launch vehicle in the event of an emergency on the launch pad or during ascent. Northrop Grumman is on contract to Lockheed Martin to build the abort motor and attitude control motor—Lockheed is the prime contractor for building the Orion Multi-Purpose Crew Vehicle designed for use on NASA’s SLS. -
Virgin Galactic Launcherone Service Guide
LauncherOne Service Guide Version 0.2 his is this cover page) SERVICE GUIDE Virgin Galactic, LLC Version 0.2 25 March 2016 1 Cleared for Public Release by the DOD Office of Prepublication and Security Review LauncherOne Service Guide Version 0.2 Revolutionizing Space Access for Small Satellites If the key selling points of small satellites are that they are agile, flexible, and affordable, then these satellites need a launch service with the same qualities. Virgin Galactic has invested in the team, technologies, and facilities required to build just such a customer-focused launch service, LauncherOne. Air-launched from a 747-400 carrier aircraft, LauncherOne is the space access service that will accelerate the small satellite revolution. Overview LauncherOne is a simple, expendable, two stage launch vehicle designed to place small satellites (up to 500 kilograms) into a wide range of Low Earth Orbits (LEO) at an affordable price. LauncherOne System Expanded View 2 Cleared for Public Release by the DOD Office of Prepublication and Security Review LauncherOne Service Guide Version 0.2 Capabilities LauncherOne missions are highly customized to suit each customer’s specific requirements. Operating commercially through the FAA, LauncherOne operates independently of many of the external factors that can delay ground based launches: weather, offline radar tracking assets, boats in the launch pad stay out zone, and traffic jams on the increasingly crowded Eastern and Western ranges. Service Value Payload Payload Capability • Up to 300 kg / 661 lbm to 500 km / 270 nmi Sun Synchronous Orbit (SSO) • Up to 500 kg / 1100 lbm to 200 km / 108 nmi circular 28.5 degree inclination Low Earth Orbit (LEO) • Due to LauncherOne’s high degree of customization, payload capabilities are best calculated for each customer based on their specific requirements. -
Paper Session IA-Shuttle-C Heavy-Lift Vehicle of the 90'S
The Space Congress® Proceedings 1989 (26th) Space - The New Generation Apr 25th, 2:00 PM Paper Session I-A - Shuttle-C Heavy-Lift Vehicle of the 90's Robert G. Eudy Manager, Shuttle-C Task Team, Marshall Space Flight Center Follow this and additional works at: https://commons.erau.edu/space-congress-proceedings Scholarly Commons Citation Eudy, Robert G., "Paper Session I-A - Shuttle-C Heavy-Lift Vehicle of the 90's" (1989). The Space Congress® Proceedings. 5. https://commons.erau.edu/space-congress-proceedings/proceedings-1989-26th/april-25-1989/5 This Event is brought to you for free and open access by the Conferences at Scholarly Commons. It has been accepted for inclusion in The Space Congress® Proceedings by an authorized administrator of Scholarly Commons. For more information, please contact [email protected]. SHUTTLE-C HEAVY-LIFT VEHICLE OF THE 90 ' S Mr. Robert G. Eudy, Manager Shuttle-C Task Team Marshall Space Flight Center ABSTRACT United States current and planned space activities identify the need for increased payload capacity and unmanned flight to complement the existing Shuttle. To meet this challenge the National Aeronautics and Space Administration is defining an unmanned cargo version of the Shuttle that can give the nation early heavy-lift capability. Called Shuttle-C, this unmanned vehicle is a natural, low-cost evolution of the current Space Shuttle that can be flying 100,000 to 170,000 pound payloads by late 1994. At the core of Shuttle-C design philosophy is the principle of evolvement from the United State's Space Transportation System. -
Grey and Gold Grungy Classroom Newsletter
T H E M A R T I A N D E C E M B E R 2 0 1 9 THE MARTIAN M O N T H L Y N E W S L E T T E R MESSAGE FROM THE DIRECTOR Greetings! Back in May 2019, we founded the GD Goenka World School's Astronomy Club, with tremendous support from our Respected Director-Principal Ma'am Dr. Neeta Bali, DHM Ms. Shahnaz Banoo Butt, IBDP Coordinator Dr. Manisha Mehta, all the IB teachers, and the students. Today, all the members of the Astronomy Club proudly speak for all that they have learnt and explored, be it from the wonders of physical Astronomy, to the mysteries of black holes. We started with our very own Solar System - the Sun, Planets, Satellites, Comets, Asteroids and went on as far as the enormous El Gordo. Our classes include lectures, debates, quizzes, interactive games and RIP TO THIS videos, and brainstorming sessions. In the coming months, we aim to learn more about the mysteries of DYNAMIC DUO the universe. We bring to you the maiden edition of our Astronomy For seven years, NASA’s Van Allen Club's Monthly Newsletter, titled 'The Martian'. Probes have studied one of the nastiest We thank our club members Sumer Kaistha, Rehaan radiation environments known to Chibber, Aekum Kamboj, Jeevesh Raj Gupta, Naman humans: the Van Allen radiation belts. Akankshi, Omar Mir, and the Deputy Director Jusjeev They're an extremely important factor Singh for their effort into bringing this magazine to to plan for when it comes to satellite you. -
View / Download
www.arianespace.com www.starsem.com www.avio Arianespace’s eighth launch of 2021 with the fifth Soyuz of the year will place its satellite passengers into low Earth orbit. The launcher will be carrying a total payload of approximately 5 518 kg. The launch will be performed from Baikonur, in Kazakhstan. MISSION DESCRIPTION 2 ONEWEB SATELLITES 3 Liftoff is planned on at exactly: SOYUZ LAUNCHER 4 06:23 p.m. Washington, D.C. time, 10:23 p.m. Universal time (UTC), LAUNCH CAMPAIGN 4 00:23 a.m. Paris time, FLIGHT SEQUENCES 5 01:23 a.m. Moscow time, 03:23 a.m. Baikonur Cosmodrome. STAKEHOLDERS OF A LAUNCH 6 The nominal duration of the mission (from liftoff to separation of the satellites) is: 3 hours and 45 minutes. Satellites: OneWeb satellite #255 to #288 Customer: OneWeb • Altitude at separation: 450 km Cyrielle BOUJU • Inclination: 84.7degrees [email protected] +33 (0)6 32 65 97 48 RUAG Space AB (Linköping, Sweden) is the prime contractor in charge of development and production of the dispenser system used on Flight ST34. It will carry the satellites during their flight to low Earth orbit and then release them into space. The dedicated dispenser is designed to Flight ST34, the 29th commercial mission from the Baikonur Cosmodrome in Kazakhstan performed by accommodate up to 36 spacecraft per launch, allowing Arianespace and its Starsem affiliate, will put 34 of OneWeb’s satellites bringing the total fleet to 288 satellites Arianespace to timely deliver the lion’s share of the initial into a near-polar orbit at an altitude of 450 kilometers. -
Space Industry Bulletin July 2019
VOLUME 2 • ISSUE 7 www.spaceindustrybulletin.com Space Industry Bulletin Market analysis and business intelligence for the space community Commercialising LEO will need destinations beyond the ISS ommercialisation of low investors. And it will depend on and a few private companies Earth orbit will require having destinations beyond just does not make a sustainable in - Cnew models for public- the International Space Station. frastructure. So how do we build private partnership, and it will be For almost two decades, the this community? built on a technology infras- ISS has been the sole hub for Kerry Timmons, LEO com - tructure that will include the commercialisation activities, pro - mercial programme manage - CONTENTS likes of robotics and machine viding unique access to research ment lead at Lockheed Martin learning. and development in a micro- Space, said: “It requires collab - Industry news 2 But commercial success will gravity environment. oration. It needs ‘old space’ and l Virgin Galactic to go public hinge on an infrastructure that Doug Comstock, deputy chief ‘new space’ working in partner - following merger “buys down the risk” for financial officer for integration ship. It needs the commercial l Launch of balloon marks the commercial partners and at NASA, said: “The ISS has 14 market to be energised to bring beginning of a new space era different facilities built by 11 dif - their money and ideas to space.” l Innovation loans offer a share of ferent companies. We don’t want When we talk about commer - £10m funding a gap in capability for human cialising LEO, it’s important to l Galileo outage helps build the access to LEO.” recognise that space is not the case for sovereign UK GNSS Along with destinations, suc - first frontier, and also that Earth l OneWeb takes sustainability into cessful commercialisation of LEO imagery is an industry success orbit and calls on the wider industry will depend on a community, story. -
2019 Nano/Microsatellite Market Forecast, 9Th Edition
2019 NANO/MICROSATELLITE MARKET FORECAST, 9TH EDITION Copyright 2018, SpaceWorks Enterprises, Inc. (SEI) APPROVED FOR PUBLIC RELEASE. SPACEWORKS ENTERPRISES, INC., COPYRIGHT 2018. 1 Since 2008, SpaceWorks has actively monitored companies and economic activity across both the satellite and launch sectors 0 - 50 kg 50 - 250kg 250 - 1000kg 1000 - 2000kg 2000kg+ Custom market assessments are available for all mass classes NANO/MICROSATELLITE DEFINITION Picosatellite Nanosatellite Microsatellite Small/Medium Satellite (0.1 – 0.99 kg) (1 – 10 kg) (10 – 100 kg) (100 – 1000 kg) 0 kg 1 kg 10 kg 100 kg 1000 kg This report bounds the upper range of interest in microsatellites at 50 kg given the relatively large amount of satellite development activity in the 1 – 50 kg range FORECASTING METHODOLOGY SpaceWorks’ proprietary Launch Demand Database (LDDB) Downstream serves as the data source for all satellite market Demand assessments ▪ Planned The LDDB is a catalogue of over 10,000+ historical and Constellations future satellites containing both public and non-public (LDDB) satellite programs Launch Supply SpaceWorks newly updated Probabilistic Forecast Model (PFM) is used to generate future market potential SpaceWorks PFM Model ▪ The PFM considers down-stream demand, announced/planed satellite constellations, and supply-side dynamics, among other relevant factors Expert Analysis The team of expert industry analysts at SpaceWorks SpaceWorks further interprets and refines the PFM results to create Forecast accurate market forecasts Methodology at a Glance 2018 SpaceWorks forecasted 2018 nano/microsatellite launches with unprecedented accuracy – actual satellites launched amounted to just 5% below our analysts’ predictions. In line with SpaceWorks’ expectations, the industry corrected after a record launch year in 2017, sending 20% less nano/microsatellites to orbit than in 2018. -
Update for MVEDA Meeting
Update for MVEDA Meeting Jonathan Firth, Executive Vice President VG Las Cruces, NM – Star Date: April 3rd 2018 Virgin Galactic’s business aim is to transform access to space for the benefit of life on Earth 4 More frequent More responsive More affordable More reliable Most Safe Virgin Galactic’s business aim is to transform access to space for the benefit of life on Earth Virgin aims to transform access to space in two markets Suborbital: Orbital: SpaceShipTwo LauncherOne Personal Spaceflight Small Satellite Research Launch Flights Virgin’s Space Portfolio at a Glance • Virgin Galactic was set up in 2004 to be world’s first commercial spaceline • Three business areas now – separate companies: • Virgin Galactic: Suborbital spaceflight for people & research • Virgin Orbit: Orbital satellite launch (SSO / LEO) • The Spaceship Company: Vehicle manufacture and flight test Virgin’s Space Portfolio at a Glance • Virgin Galactic was set up in 2004 to be world’s first commercial spaceline • Three business areas now – separate companies: • Virgin Galactic: Suborbital spaceflight for people & research • Virgin Orbit: Orbital satellite launch (SSO / LEO) • The Spaceship Company: Vehicle manufacture and test • Each company carries out its own: design, engineering, manufacturing, testing and flight operations Aims: frequent flights, responsive, lower cost, high safety/reliability Virgin Galactic will operate from the ‘Gateway to Space’ facility at Spaceport America in New Mexico VG’s Economic Impact in New Mexico to date 33 + 85 + local hires / 5 years 10 VG’s Economic Impact in New Mexico to date VG now has 33 full time employees permanently based at its Las Cruces, NM office, with various other employees cycling through from our Mojave, CA facility on a regular basis, and a plan to transition at least 85 employees permanently from Mojave to New Mexico before the start of operations. -
For Personal Use Only Use Personal for Galactic for Four Dedicated Missions on the Launcherone System from 2018
Sky and Space Global Ltd ABN 73 117 770 475 Level 7 1008 Hay Street PERTH WA 6000 P: +61 8 9389 2000 F: +61 8 9389 2099 W: skyandspace.global 5 October 2016 ASX Code: SAS Virgin Galactic Sign MOU - Evaluation of SAS Network for LauncherOne Highlights • Sky and Space Global has signed a non-binding Memorandum of Understanding (MOU) with Virgin Galactic • The MOU is to evaluate the technical and commercial potential of the Company’s nano- satellite communications network to provide connectivity to its LauncherOne carrier aircraft, Cosmic Girl • Parties will work together to determine whether Virgin Galactic’s modified 747-400 carrier aircraft can be made compatible with SAS’s space-based communication network • The joint objective is to evaluate the potential use of the SAS nano-satellite communications network as the platform to transmit the LauncherOne telemetry data from the launch vehicle during orbit, back to Virgin Galactic’s data control centre • SAS has previously contracted with Virgin Galactic for four dedicated missions on the LauncherOne system Sky and Space Global Ltd (ASX: SAS, “Sky and Space Global” or the “Company”) is pleased to advise that it has signed a non-binding Memorandum of Understanding (MOU) with Virgin Galactic regarding the potential use of the Company’s network to provide connectivity to Virgin Galactic’s 747 carrier aircraft for transmission of its telemetry data to its control centre. Under the terms of the MOU, the parties are to work together to evaluate the technical and commercial parameters to determine whether Virgin Galactic’s modified 747-400 carrier aircraft, Cosmic Girl can be made compatible with SAS’s space-based nano-satellite communications network. -
Atlas V Cutaway Poster
ATLAS V Since 2002, Atlas V rockets have delivered vital national security, science and exploration, and commercial missions for customers across the globe including the U.S. Air Force, the National Reconnaissance Oice and NASA. 225 ft The spacecraft is encapsulated in either a 5-m (17.8-ft) or a 4-m (13.8-ft) diameter payload fairing (PLF). The 4-m-diameter PLF is a bisector (two-piece shell) fairing consisting of aluminum skin/stringer construction with vertical split-line longerons. The Atlas V 400 series oers three payload fairing options: the large (LPF, shown at left), the extended (EPF) and the extra extended (XPF). The 5-m PLF is a sandwich composite structure made with a vented aluminum-honeycomb core and graphite-epoxy face sheets. The bisector (two-piece shell) PLF encapsulates both the Centaur upper stage and the spacecraft, which separates using a debris-free pyrotechnic actuating 200 ft system. Payload clearance and vehicle structural stability are enhanced by the all-aluminum forward load reactor (FLR), which centers the PLF around the Centaur upper stage and shares payload shear loading. The Atlas V 500 series oers 1 three payload fairing options: the short (shown at left), medium 18 and long. 1 1 The Centaur upper stage is 3.1 m (10 ft) in diameter and 12.7 m (41.6 ft) long. Its propellant tanks are constructed of pressure-stabilized, corrosion-resistant stainless steel. Centaur is a liquid hydrogen/liquid oxygen-fueled vehicle. It uses a single RL10 engine producing 99.2 kN (22,300 lbf) of thrust. -
Phase Change: Titan’S Disappearing Lakes
Phase Change: Titan’s Disappearing Lakes Investigation Notebook NYC Edition © 2018 by The Regents of the University of California. All rights reserved. No part of this publication may be reproduced or transmitted in any form or by any means, electronic or mechanical, including photocopy, recording, or any information storage or retrieval system, without permission in writing from the publisher. Teachers purchasing this Investigation Notebook as part of a kit may reproduce the book herein in sufficient quantities for classroom use only and not for resale. These materials are based upon work partially supported by the National Science Foundation under grant numbers DRL-1119584, DRL-1417939, ESI-0242733, ESI-0628272, and ESI-0822119. The Federal Government has certain rights in this material. Any opinions, findings, and conclusions or recommendations expressed in this material are those of the author(s) and do not necessarily reflect the views of the National Science Foundation. These materials are based upon work partially supported by the Institute of Education Sciences, U.S. Department of Education, through Grant R305A130610 to The Regents of the University of California. The opinions expressed are those of the authors and do not represent views of the Institute or the U.S. Department of Education. Developed by the Learning Design Group at the University of California, Berkeley’s Lawrence Hall of Science. Amplify. 55 Washington Street, Suite 800 Brooklyn, NY 11201 1-800-823-1969 www.amplify.com Phase Change: Titan’s Disappearing Lakes