Launcherone Success Opens New Space Access Gateway Guy Norris January 22, 2021
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2008 Estes-Cox Corp. All Rights Reserved
Estes-Cox Corp. 1295 H Street, P.O. BOX 227 Patent Pending Penrose, CO 81240-0227 ©2008 Estes-Cox Corp. All rights reserved. (9-08) PN 2927-8 TABLE OF CONTENTS HOW DO I START MY OWN ESTES ROCKET FLEET? The best way to begin model rocketry is with an Estes flying model rocket Starter Set or Launch Set. You can ® Index . .2 Skill Level 2 Rocket Kits . .30 either start with a Ready To Fly Starter Set or Launch Set that has a fully constructed model rocket or an E2X How To Start . .3 Skill Level 3 Rocket Kits . .34 Starter Set or Launch Set with a rocket that requires assembly prior to launching. Both types of sets come What to Know . .4 ‘E’ Engine Powered Kits . .36 complete with an electrical launch controller, adjustable launch pad and an information booklet to get you out Model Rocket Safety Code . .5 Blurzz™ Rocket Racers . .36 and flying in no time. Starter Sets include engines, Launch Sets let you choose your own engines (not includ- Ready To Fly Starter Sets . .6 How Model Rocket Engines Work . .38 ed). You’ll need four ‘AA’ alkaline batteries and perhaps glue, depending on which set you select. E2X® Starter Sets . .8 Model Rocket Engine Chart . .39 Ready to Fly Launch Sets . .10 Engine Time/Thrust Curves . .40 Launch Sets . .12 Model Rocket Accessories . .41 HOW EASY AND HOW MUCH TIME DOES IT TAKE TO BUILD MY ROCKETS? Ready To Fly Rockets . .14 Estes R/C Airplanes . .42 ® E2X Rocket Kits . .16 Estes Educator™ Products . -
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. -
IT's a Little Chile up Here
IT’s A Little chile up here Press Kit | NET 29 July 2021 LAUNCH INFORMATION LAUNCH WINDOW ORBIT 12-day launch window opening from 29 July 2021 600km DAILY LAUNCH OPPORTUNITY The launch timing for this mission is the same for each day of the launch window. SATELLITES Time Zone Window Open Window Close NZT 18:00 20:00 UTC 06:00 08:00 1 EDT 02:00 04:00 PDT 23:00 01:00 The launch window extends for 12 days. INCLINATION 37 Degrees LAUNCH SITE Launch Complex 1, Mahia, New Zealand CUSTOMER LIVE STREAM Watch the live launch webcast: USSF rocketlabusa.com/live-stream Dedicated mission for U.S. Space Force 2 | Rocket Lab | Press Kit: It’s A Little Chile Up Here Mission OVERVIEW About ‘It’s a Little Chile Up Here’ Electron will launch a research and development satellite to low Earth orbit from Launch Complex 1 in New Zealand for the United States Space Force COMPLEX 1 LAUNCH MAHIA, NEW ZEALAND Electron will deploy an Air Force Research Laboratory- sponsored demonstration satellite called Monolith. ‘It’s a Little Chile Up Here’ The satellite will explore and demonstrate the use of a deployable sensor, where the sensor’s mass is a will be Rocket Lab’s: substantial fraction of the total mass of the spacecraft, changing the spacecraft’s dynamic properties and testing ability to maintain spacecraft attitude control. Analysis from the use of a deployable sensor aims to th st enable the use of smaller satellite buses when building 4 21 future deployable sensors such as weather satellites, launch for Electron launch thereby reducing the cost, complexity, and development timelines. -
Press Release
Rocket Lab, an End-to-End Space Company and Global Leader in Launch, to Become Publicly Traded Through Merger with Vector Acquisition Corporation End-to-end space company with an established track record, uniquely positioned to extend its lead across a launch, space systems and space applications market forecast to grow to $1.4 trillion by 2030 One of only two U.S. commercial companies delivering regular access to orbit: 97 satellites deployed for governments and private companies across 16 missions Second most frequently launched U.S. orbital rocket, with proven Photon spacecraft platform already operating on orbit and missions booked to the Moon, Mars and Venus Transaction will provide capital to fund development of reusable Neutron launch vehicle with an 8-ton payload lift capacity tailored for mega constellations, deep space missions and human spaceflight Proceeds also expected to fund organic and inorganic growth in the space systems market and support expansion into space applications enabling Rocket Lab to deliver data and services from space Business combination values Rocket Lab at an implied pro forma enterprise value of $4.1 billion. Pro forma cash balance of the combined company of approximately $750 million at close Rocket Lab forecasts that it will generate positive adjusted EBITDA in 2023, positive cash flows in 2024 and more than $1 billion in revenue in 2026 Group of top-tier institutional investors have committed to participate in the transaction through a significantly oversubscribed PIPE of approximately $470 million, with 39 total investors including Vector Capital, BlackRock and Neuberger Berman Transaction is expected to close in Q2 2021, upon which Rocket Lab will be publicly listed on the Nasdaq under the ticker RKLB Current Rocket Lab shareholders will own 82% of the pro forma equity of combined company Long Beach, California – 1 March 2021 – Rocket Lab USA, Inc. -
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. -
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