Sale Price Drives Potential Effects on DOD and Commercial Launch Providers
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Launch and Deployment Analysis for a Small, MEO, Technology Demonstration Satellite
46th AIAA Aerospace Sciences Meeting and Exhibit AIAA 2008-1131 7 – 10 January 20006, Reno, Nevada Launch and Deployment Analysis for a Small, MEO, Technology Demonstration Satellite Stephen A. Whitmore* and Tyson K. Smith† Utah State University, Logan, UT, 84322-4130 A trade study investigating the economics, mass budget, and concept of operations for delivery of a small technology-demonstration satellite to a medium-altitude earth orbit is presented. The mission requires payload deployment at a 19,000 km orbit altitude and an inclination of 55o. Because the payload is a technology demonstrator and not part of an operational mission, launch and deployment costs are a paramount consideration. The payload includes classified technologies; consequently a USA licensed launch system is mandated. A preliminary trade analysis is performed where all available options for FAA-licensed US launch systems are considered. The preliminary trade study selects the Orbital Sciences Minotaur V launch vehicle, derived from the decommissioned Peacekeeper missile system, as the most favorable option for payload delivery. To meet mission objectives the Minotaur V configuration is modified, replacing the baseline 5th stage ATK-37FM motor with the significantly smaller ATK Star 27. The proposed design change enables payload delivery to the required orbit without using a 6th stage kick motor. End-to-end mass budgets are calculated, and a concept of operations is presented. Monte-Carlo simulations are used to characterize the expected accuracy of the final orbit. -
Cape Canaveral Air Force Station Support to Commercial Space Launch
The Space Congress® Proceedings 2019 (46th) Light the Fire Jun 4th, 3:30 PM Cape Canaveral Air Force Station Support to Commercial Space Launch Thomas Ste. Marie Vice Commander, 45th Space Wing Follow this and additional works at: https://commons.erau.edu/space-congress-proceedings Scholarly Commons Citation Ste. Marie, Thomas, "Cape Canaveral Air Force Station Support to Commercial Space Launch" (2019). The Space Congress® Proceedings. 31. https://commons.erau.edu/space-congress-proceedings/proceedings-2019-46th/presentations/31 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]. Cape Canaveral Air Force Station Support to Commercial Space Launch Colonel Thomas Ste. Marie Vice Commander, 45th Space Wing CCAFS Launch Customers: 2013 Complex 41: ULA Atlas V (CST-100) Complex 40: SpaceX Falcon 9 Complex 37: ULA Delta IV; Delta IV Heavy Complex 46: Space Florida, Navy* Skid Strip: NGIS Pegasus Atlantic Ocean: Navy Trident II* Black text – current programs; Blue text – in work; * – sub-orbital CCAFS Launch Customers: 2013 Complex 39B: NASA SLS Complex 41: ULA Atlas V (CST-100) Complex 40: SpaceX Falcon 9 Complex 37: ULA Delta IV; Delta IV Heavy NASA Space Launch System Launch Complex 39B February 4, 2013 Complex 46: Space Florida, Navy* Skid Strip: NGIS Pegasus Atlantic Ocean: Navy Trident II* Black text – current programs; -
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 . -
Small Space Launch: Origins & Challenges Lt Col Thomas H
Small Space Launch: Origins & Challenges Lt Col Thomas H. Freeman, USAF, [email protected], (505)853-4750 Maj Jose Delarosa, USAF, [email protected], (505)846-4097 Launch Test Squadron, SMC/SDTW Small Space Launch: Origins The United States Space Situational Awareness capability continues to be a key element in obtaining and maintaining the high ground in space. Space Situational Awareness satellites are critical enablers for integrated air, ground and sea operations, and play an essential role in fighting and winning conflicts. The United States leads the world space community in spacecraft payload systems from the component level into spacecraft, and in the development of constellations of spacecraft. The United States’ position is founded upon continued government investment in research and development in space technology [1], which is clearly reflected in the Space Situational Awareness capabilities and the longevity of these missions. In the area of launch systems that support Space Situational Awareness, despite the recent development of small launch vehicles, the United States launch capability is dominated by an old, unresponsive and relatively expensive set of launchers [1] in the Expandable, Expendable Launch Vehicles (EELV) platforms; Delta IV and Atlas V. The EELV systems require an average of six to eight months from positioning on the launch table until liftoff [3]. Access to space requires maintaining a robust space transportation capability, founded on a rigorous industrial and technology base. The downturn of commercial space launch service use has undermined, for the time being, the ability of industry to recoup its significant investment in current launch systems. -
Commercial Space Transportation Developments and Concepts: Vehicles, Technologies and Spaceports
Commercial Space Transportation 2006 Commercial Space Transportation Developments and Concepts: Vehicles, Technologies and Spaceports January 2006 HQ003606.INDD 2006 U.S. Commercial Space Transportation Developments and Concepts About FAA/AST About the Office of Commercial Space Transportation The Federal Aviation Administration’s Office of Commercial Space Transportation (FAA/AST) licenses and regulates U.S. commercial space launch and reentry activity, as well as the operation of non-federal launch and reentry sites, as authorized by Executive Order 12465 and Title 49 United States Code, Subtitle IX, Chapter 701 (formerly the Commercial Space Launch Act). FAA/AST’s mission is to ensure public health and safety and the safety of property while protecting the national security and foreign policy interests of the United States during commercial launch and reentry operations. In addition, FAA/AST is directed to encour- age, facilitate, and promote commercial space launches and reentries. Additional information concerning commercial space transportation can be found on FAA/AST’s web site at http://ast.faa.gov. Federal Aviation Administration Office of Commercial Space Transportation i About FAA/AST 2006 U.S. Commercial Space Transportation Developments and Concepts NOTICE Use of trade names or names of manufacturers in this document does not constitute an official endorsement of such products or manufacturers, either expressed or implied, by the Federal Aviation Administration. ii Federal Aviation Administration Office of Commercial Space Transportation 2006 U.S. Commercial Space Transportation Developments and Concepts Contents Table of Contents Introduction . .1 Significant 2005 Events . .4 Space Competitions . .6 Expendable Launch Vehicles . .9 Current Expendable Launch Vehicle Systems . .9 Atlas 5 - Lockheed Martin Corporation . -
Review of Nasa's Acquisition of Commercial Launch Services
FEBRUARY 17, 2011 AUDIT REPORT OFFICE OF AUDITS REVIEW OF NASA’S ACQUISITION OF COMMERCIAL LAUNCH SERVICES OFFICE OF INSPECTOR GENERAL National Aeronautics and Space Administration REPORT NO. IG-11-012 (ASSIGNMENT NO. A-09-011-00) Final report released by: Paul K. Martin Inspector General Acronyms COTS Commercial Orbital Transportation Services CRS Commercial Resupply Services DOD Department of Defense EELV Evolved Expendable Launch Vehicle ELV Expendable Launch Vehicle ESMD Exploration Systems Mission Directorate GAO Government Accountability Office GLAST Gamma-ray Large Area Space Telescope IBEX Interstellar Boundary Explorer ICBM Intercontinental Ballistic Missile ICESat-II Ice, Cloud, and Land Elevation Satellite IDIQ Indefinite-Delivery, Indefinite-Quantity ISS International Space Station LADEE Lunar Atmosphere and Dust Environment Explorer LCROSS Lunar Crater Observation and Sensing Satellite LRO Lunar Reconnaissance Orbiter LSP Launch Services Program NLS NASA Launch Services OCO Orbiting Carbon Observatory OIG Office of Inspector General PPBE Planning, Programming, Budgeting, and Execution SMAP Soil Moisture Active Passive SMD Science Mission Directorate SOMD Space Operations Mission Directorate ULA United Launch Alliance REPORT NO. IG-11-012 FEBRUARY 17, 2011 OVERVIEW REVIEW OF NASA’S ACQUISITION OF COMMERCIAL LAUNCH SERVICES The Issue Commercial U.S. launch services providers compete domestically and internationally for contracts to carry satellites and other payloads into orbit using unmanned, single-use vehicles known as expendable launch vehicles (ELVs). However, since the late 1990s the global commercial launch market has generally declined following the downturn in the telecommunications services industry, which was the primary customer of the commercial space industry. Given this trend, U.S. launch services providers struggling to remain economically viable have been bolstered by the Commercial Space Act of 1998 (Public Law 105-303), which requires NASA and other Federal agencies to plan missions and procure space transportation services from U.S. -
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. -
Minotaur I User's Guide
This page left intentionally blank. Minotaur I User’s Guide Revision Summary TM-14025, Rev. D REVISION SUMMARY VERSION DOCUMENT DATE CHANGE PAGE 1.0 TM-14025 Mar 2002 Initial Release All 2.0 TM-14025A Oct 2004 Changes throughout. Major updates include All · Performance plots · Environments · Payload accommodations · Added 61 inch fairing option 3.0 TM-14025B Mar 2014 Extensively Revised All 3.1 TM-14025C Sep 2015 Updated to current Orbital ATK naming. All 3.2 TM-14025D Sep 2018 Branding update to Northrop Grumman. All 3.3 TM-14025D Sep 2020 Branding update. All Updated contact information. Release 3.3 September 2020 i Minotaur I User’s Guide Revision Summary TM-14025, Rev. D This page left intentionally blank. Release 3.3 September 2020 ii Minotaur I User’s Guide Preface TM-14025, Rev. D PREFACE This Minotaur I User's Guide is intended to familiarize potential space launch vehicle users with the Mino- taur I launch system, its capabilities and its associated services. All data provided herein is for reference purposes only and should not be used for mission specific analyses. Detailed analyses will be performed based on the requirements and characteristics of each specific mission. The launch services described herein are available for US Government sponsored missions via the United States Air Force (USAF) Space and Missile Systems Center (SMC), Advanced Systems and Development Directorate (SMC/AD), Rocket Systems Launch Program (SMC/ADSL). For technical information and additional copies of this User’s Guide, contact: Northrop Grumman -
Small Launch Vehicles a 2015 State of the Industry Survey Carlos Niederstrasser
Small Launch Vehicles A 2015 State of the Industry Survey Carlos Niederstrasser An update to this survey will be presented at the 2016 Internaonal Astronau9cal Congress 1 Agenda Overview of Small Launch Vehicles Launch Method/Locations Launch Performance Projected Launch Costs Individual Rocket Details Copyright © 2015 by Orbital ATK, Inc. 2 Listing Criteria Have a maximum capability to LEO of 1000 kg (definition of LEO left to the LV provider). The effort must be for the development of an entire launch vehicle system (with the exception of carrier aircraft for air launch vehicles). Mentioned through a web site update, social media, traditional media, conference paper, press release, etc. sometime after 2010. Have a stated goal of completing a fully operational space launch (orbital) vehicle. Funded concept or feasibility studies by government agencies, patents for new launch methods, etc., do not qualify. Expect to be widely available commercially or to the U.S. Government No specific indication that the effort has been cancelled, closed, or otherwise disbanded. Correc&ons, addi&ons, and comments are welcomed and encouraged! Copyright © 2015 by Orbital ATK, Inc. 3 We did not … … Talk to the individual companies … Rely on any proprietary/confidential information … Verify accuracy of data found in public resources Ø Primarily relied on companies’ web sites Funding sources, when listed, are not implied to be the vehicles sole or even majority funding source. We do not make any value judgements on technical or financial credibility -
Igor AFANASYEV, Dmitry VORONTSOV Cosmonautics | Event
cosmonautics | event Andrey Morgunov Igor AFANASYEV, Dmitry VORONTSOV AANGARA’SNGARA’S FFIRSTIRST BBLASTOFFLASTOFF At 16.04 hrs Moscow time on 9 July 2014, the Plesetsk space launch centre saw the launching facility in February 2014 to the first launch of the Angara-1.2PP launch vehicle of the advanced space rocket practice its fuelling and the nose fairing was family being developed by the Khrunichev state space research and production fitted on the rocket in March. The successful ground tests were followed by the prelaunch centre. The maiden blastoff conducted as part of the Angara flight test programme preparations. was aimed at testing the solutions embodied in the design of the URM-1 and URM-2 The date of the launch was put off for versatile rocket modules and the Angara’s launch and technical facilities as well. 27 June 2014 due to extra checks required. In this connection, orbiting an actual spacecraft had not been considered, with On 9 June, Khrunichev hosted a session of an inseparable full-scale mock-up used as payload. The flight was suborbital to the Chief Designers Council, dedicated to prevent cluttering near-Earth orbit with space junk. the preparation of the Angara to its flight tests. The session pronounced the rocket fit To say the Angara’s first launch had been In spite of the hurdles, the developer, for the trials. anticipated for a long time would be an nevertheless, got in the stretch with the Angara The LV had been taken out of the assembly understatement: it was slated for 2005 under programme. -
Launcherone Success Opens New Space Access Gateway Guy Norris January 22, 2021
1/22/21 7:05 1/6 LauncherOne Success Opens New Space Access Gateway Guy Norris January 22, 2021 With San Nicolas Island far below, LauncherOne headed for polar orbit. Credit: Virgin Orbit Virgin Orbit had barely tweeted news of the successful Jan. 17 space debut of its LauncherOne vehicle on social media when new launch contracts began arriving in the company’s email inbox. A testament to the pent-up market demand for small-satellite launch capability, the speedy reaction to the long-awaited demonstration of the new space-access vehicle paves the way for multiple follow-on Virgin Orbit missions by year-end and a potential doubling of the rate in 2022. First successful privately developed air-launched, liquid-fueled rocket Payloads deployed for NASA’s Venture Class Launch Services program The glitch-free !ight of LauncherOne on its second demonstration test was a critical and much-welcomed milestone for the Long Beach, California-based company. Coming almost nine years a"er the air-launch concept was #rst unveiled by Virgin founder Richard Branson, and six years a"er the start of full-scale development, the !ight followed last May’s #rst demonstration mission, which ended abruptly when the rocket motor shut o$ a"er just 4 sec. 1/22/21 7:05 2/6 A"er an exhaustive analysis and modi#cations to beef up the oxidizer feed line at the heart of the #rst !ight failure, the path to the Launch Demo 2 test was then delayed until January 2021 by the COVID-19 pandemic. With the LauncherOne system now proven, design changes veri#ed and the #rst 10 small satellites placed in orbit, Virgin Orbit is already focusing on the next steps to ramp up its production and launch-cadence capabilities. -
The European Launchers Between Commerce and Geopolitics
The European Launchers between Commerce and Geopolitics Report 56 March 2016 Marco Aliberti Matteo Tugnoli Short title: ESPI Report 56 ISSN: 2218-0931 (print), 2076-6688 (online) Published in March 2016 Editor and publisher: European Space Policy Institute, ESPI Schwarzenbergplatz 6 • 1030 Vienna • Austria http://www.espi.or.at Tel. +43 1 7181118-0; Fax -99 Rights reserved – No part of this report may be reproduced or transmitted in any form or for any purpose with- out permission from ESPI. Citations and extracts to be published by other means are subject to mentioning “Source: ESPI Report 56; March 2016. 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, inciden- tal or consequential, resulting from the information contained in this publication. Design: Panthera.cc ESPI Report 56 2 March 2016 The European Launchers between Commerce and Geopolitics Table of Contents Executive Summary 5 1. Introduction 10 1.1 Access to Space at the Nexus of Commerce and Geopolitics 10 1.2 Objectives of the Report 12 1.3 Methodology and Structure 12 2. Access to Space in Europe 14 2.1 European Launchers: from Political Autonomy to Market Dominance 14 2.1.1 The Quest for European Independent Access to Space 14 2.1.3 European Launchers: the Current Family 16 2.1.3 The Working System: Launcher Strategy, Development and Exploitation 19 2.2 Preparing for the Future: the 2014 ESA Ministerial Council 22 2.2.1 The Path to the Ministerial 22 2.2.2 A Look at Europe’s Future Launchers and Infrastructure 26 2.2.3 A Revolution in Governance 30 3.