Reducing Launch Operation Costs: New Technologies and Practices
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Space Reporter's Handbook Mission Supplement
CBS News Space Reporter's Handbook - Mission Supplement Page 1 The CBS News Space Reporter's Handbook Mission Supplement Shuttle Mission STS-125: Hubble Space Telescope Servicing Mission 4 Written and Produced By William G. Harwood CBS News Space Analyst [email protected] CBS News 5/10/09 Page 2 CBS News Space Reporter's Handbook - Mission Supplement Revision History Editor's Note Mission-specific sections of the Space Reporter's Handbook are posted as flight data becomes available. Readers should check the CBS News "Space Place" web site in the weeks before a launch to download the latest edition: http://www.cbsnews.com/network/news/space/current.html DATE RELEASE NOTES 08/03/08 Initial STS-125 release 04/11/09 Updating to reflect may 12 launch; revised flight plan 04/15/09 Adding EVA breakdown; walkthrough 04/23/09 Updating for 5/11 launch target date 04/30/09 Adding STS-400 details from FRR briefing 05/04/09 Adding trajectory data; abort boundaries; STS-400 launch windows Introduction This document is an outgrowth of my original UPI Space Reporter's Handbook, prepared prior to STS-26 for United Press International and updated for several flights thereafter due to popular demand. The current version is prepared for CBS News. As with the original, the goal here is to provide useful information on U.S. and Russian space flights so reporters and producers will not be forced to rely on government or industry public affairs officers at times when it might be difficult to get timely responses. All of these data are available elsewhere, of course, but not necessarily in one place. -
Trade Studies Towards an Australian Indigenous Space Launch System
TRADE STUDIES TOWARDS AN AUSTRALIAN INDIGENOUS SPACE LAUNCH SYSTEM A thesis submitted for the degree of Master of Engineering by Gordon P. Briggs B.Sc. (Hons), M.Sc. (Astron) School of Engineering and Information Technology, University College, University of New South Wales, Australian Defence Force Academy January 2010 Abstract During the project Apollo moon landings of the mid 1970s the United States of America was the pre-eminent space faring nation followed closely by only the USSR. Since that time many other nations have realised the potential of spaceflight not only for immediate financial gain in areas such as communications and earth observation but also in the strategic areas of scientific discovery, industrial development and national prestige. Australia on the other hand has resolutely refused to participate by instituting its own space program. Successive Australian governments have preferred to obtain any required space hardware or services by purchasing off-the-shelf from foreign suppliers. This policy or attitude is a matter of frustration to those sections of the Australian technical community who believe that the nation should be participating in space technology. In particular the provision of an indigenous launch vehicle that would guarantee the nation independent access to the space frontier. It would therefore appear that any launch vehicle development in Australia will be left to non- government organisations to at least define the requirements for such a vehicle and to initiate development of long-lead items for such a project. It is therefore the aim of this thesis to attempt to define some of the requirements for a nascent Australian indigenous launch vehicle system. -
Corporate Profile
2013 : Epsilon Launch Vehicle 2009 : International Space Station 1997 : M-V Launch Vehicle 1955 : The First Launched Pencil Rocket Corporate Profile Looking Ahead to Future Progress IHI Aerospace (IA) is carrying out the development, manufacture, and sales of rocket projectiles, and has been contributing in a big way to the indigenous space development in Japan. We started research on rocket projectiles in 1953. Now we have become a leading comprehensive manufacturer carrying out development and manufacture of rocket projectiles in Japan, and are active in a large number of fields such as rockets for scientific observation, rockets for launching practical satellites, and defense-related systems, etc. In the space science field, we cooperate with the Japan Aerospace Exploration Agency (JAXA) to develop and manufacture various types of observational rockets named K (Kappa), L (Lambda), and S (Sounding), and the M (Mu) rockets. With the M rockets, we have contributed to the launch of many scientific satellites. In 2013, efforts resulted in the successful launch of an Epsilon Rocket prototype, a next-generation solid rocket which inherited the 2 technologies of all the aforementioned rockets. In the practical satellite booster rocket field, We cooperates with the JAXA and has responsibilities in the solid propellant field including rocket boosters, upper-stage motors in development of the N, H-I, H-II, and H-IIA H-IIB rockets. We have also achieved excellent results in development of rockets for material experiments and recovery systems, as well as the development of equipment for use in a space environment or experimentation. In the defense field, we have developed and manufactured a variety of rocket systems and rocket motors for guided missiles, playing an important role in Japanese defense. -
Launch Options for the Future: a Buyer's Guide (Part 7 Of
— Chapter 3 Enhanced Baseline CONTENTS , Page Improving the Shuttle . 27 Advanced Solid Rocket Motors (ASRMs) . 27 Liquid Rocket Boosters (LRBs) . 28 Lighter Tanks . 29 Improving Shuttle Ground Operations . 29 Improving Existing ELVs . 29 Delta . 30 Atlas-Centaur . ● ● . .* . 30 Titan . ● . ✎ ✎ . 30 Capability . ✎ . ✎ ✎ . ● ✎ ✎ . 30 Table 3-1. Theoretical Lift Capability of Enhanced U.S. Launch Systems. 31 Chapter 3 Enhanced Baseline The ENHANCED BASELINE option is the U.S. Government’s “Best Buy” if . it desires a space program with current or slightly greater levels of activity. By making in- cremental improvements to existing launch vehicles, production and launch facilities, the U.S. could increase its launch capacity to about 1.4 million pounds per year to LEO. The investment required would be low compared to building new vehicles; however, the ade- quacy of the resulting fleet resiliency and dependability is uncertain. This option would not provide the low launch costs (e.g. 10 percent of current costs) sought for SDI deploy- ment or an aggressive civilian space initiative, like a piloted mission to Mars, IMPROVING THE SHUTTLE The Shuttle, though a remarkable tech- . reducing the number of factory joints and nological achievement, never achieved its in- the number of parts, tended payload capacity and recent safety . designing the ASRMs so that the Space modifications have further degraded its per- Shuttle Main Engines no longer need to formance by approximately 4,800 pounds. be throttled during the region of maxi- Advanced Solid Rocket Motors (ASRMs) or mum dynamic pressure, Liquid Rocket Boosters (LRBs) have the potential to restore some of this perfor- ● replacing asbestos-bearing materials, mance; studies on both are underway. -
Jacques Tiziou Space Collection
Jacques Tiziou Space Collection Isaac Middleton and Melissa A. N. Keiser 2019 National Air and Space Museum Archives 14390 Air & Space Museum Parkway Chantilly, VA 20151 [email protected] https://airandspace.si.edu/archives Table of Contents Collection Overview ........................................................................................................ 1 Administrative Information .............................................................................................. 1 Biographical / Historical.................................................................................................... 1 Scope and Contents........................................................................................................ 2 Arrangement..................................................................................................................... 2 Names and Subjects ...................................................................................................... 2 Container Listing ............................................................................................................. 4 Series : Files, (bulk 1960-2011)............................................................................... 4 Series : Photography, (bulk 1960-2011)................................................................. 25 Jacques Tiziou Space Collection NASM.2018.0078 Collection Overview Repository: National Air and Space Museum Archives Title: Jacques Tiziou Space Collection Identifier: NASM.2018.0078 Date: (bulk 1960s through -
5.0 Launch Vehicle Performance
Final Design Report on Converting the Minuteman Missile into a Small Satellite Launch System Submitted to Dr. George W. Botbyl USRA Design Professor Department of Aerospace Engineering The University of Texas at Austin by The Minotaur Design Team Rodrick McHaty - Team Leader Rodolfo Gonzalez - Chief Engineer Vu Pham - Chief Administrative Officer Engineers: Gordon MacKay Greg Humble Bill Alexander November 24, 1993 EXECUTIVE SUMMARY m Introduction Due to the Strategic Arms Reduction Talks (START) treaty between the United States and Ex-Soviet Union, 450 Stage III Minuteman II (MMII) missiles were -q recently taken out of service. Minotaur Designs Incorporated (MDI) intends to StagelI convert the MMII ballistic missile from a "" nuclear" warhead carrier into a small- "] L__________ satellite launcher. MDI will perform this conversion by acquiring the Minuteman Stage I stages, purchasing currently available control wafers, and designing a new ] shroud and interfaces for the satellite. Figure 1. MDI missile MDI is also responsible for properly integrating all systems. The new MDI system still System Description incorporates the original range-safety raceway and attitude-control actuators. MDI plans to purchase the 52 inch Figure 1 shows a representation of diameter avionics, range-safety, and the MDI missile. The stages that MDI attitude-control wafers from Martin will acquire from the Air Force are the Marietta's Multi-Service Launch System MMII stage I and II, and the MMIII stage (MSLS), "D" configuration missile, III. These stages define the propulsion which is currently under development. system of the MDI missile, and an MDI has designed a mechanical analysis of attainable orbits is performed. -
Historian's Corner
Historian’s Corner Ray Ziehm (POC) ([email protected] ) We are making some minor changes to the Historian’s writings for each addition of the STAR. Ray Ziehm has volunteered to take the lead in coordinating our quarterly write ups. He will be the only one listed under the officers for Historians. The individual contributors are well appreciated and are needed every year. We have in the past missed some Historian write ups, so having a lead coordinator should eliminate that. The individual writers will continue to be identified with their writings. Those of you that would like to write an article in the STAR for an item of historical interest should contact Ray at 303-784- 1413. Thanks, Bob Snodgress Ed Bock ([email protected] ) Atlas/Centaur Sale and Transition to Martin Marietta This Atlas Program history was originally presented at the Centaur 50th Anniversary celebration in San Diego by Ed Bock. It has been expanded with input from Tony Christensen to include the Centaur for Titan Program Transition. To appreciate this sale and transition, it’s necessary to understand the environment at General Dynamics Space Systems (GDSS) Division in the early 1990’s. The Commercial Atlas Program was inaugurated with the launch of AC-69, the first Atlas I, in July 1990. Atlas II was in development, and its first launch occurred in December 1991. GDSS was in the process of evaluating a Russian rocket engine (the RD-180) for its evolved Atlas. From mid 1990 to late 1993 there were 14 Atlas/Centaur launches, including three Atlas I failures. -
Small Satellite Access to ESPA Standard Service
SSC10-IX-1 Small Satellite Access to ESPA Standard Service Mr. Ted Marrujo DoD Space Test Program (STP), Mission Design 3548 Aberdeen Ave. SE, Kirtland AFB NM 87117; (505) 853-3338 Ted. [email protected] Lt Jake Mathis Space and Missile Systems Center, Launch and Range Systems Wing, Engineering 483 N. Aviation Blvd, Los Angeles AFB, CA; (310) 653-3392 [email protected] Mr. Caleb C. Weiss United Launch Alliance, Mission Integration 12257 S. Wadsworth Blvd, TSB-B7140, Littleton, CO 80125; (303) 977-0843 [email protected] ABSTRACT The DoD Space Test Program (STP), the Air Force Launch and Range Systems Wing (LRSW), and United Launch Alliance (ULA) are teaming up to provide a rideshare service to small satellites (<400lb) using an Evolved Expendable Launch Vehicle (EELV) Secondary Payload Adapter (ESPA). This rideshare service is an opportunity on EELV missions with margin to carry auxiliary payloads (APLs). This paper will define the ESPA, the standard rideshare service provided to APLs, and how APLs can access this service. We will discuss the roles and responsibilities the different government organizations, ULA, and the small satellite provider have in accessing and implementing ESPA Standard Service. In brief, ULA builds the EELV and performs the launch service, LRSW is responsible for developing and acquiring EELVs from ULA, and STP is responsible for identifying and manifesting APLs that meet ESPA Standard Service requirements. We will further define the processes and procedures required to implement ESPA Standard Service to include: how a particular EELV mission is selected to host ESPA Standard Service, the selection process for auxiliary satellites to utilize the capability, the requirements and timelines small satellites must meet to qualify, and the scope of services provided by ULA as part of Standard Service. -
Building KSC's Launch Complex 39
National Aeronautics and Space Administration Building KSC’s Launch Complex 39 n the beginning, there was sand and adjacent to the VAB would house the Apollo I palmettos and water. Yet out of this idyllic spacecraft and the Launch Control Center. setting would grow the most unique structures -- The launcher-transporter would incorporate engineering milestones -- that would set the stage three major facilities: a pedestal for the space for the future in space. vehicle, an umbilical tower to service the upper The Kennedy Space Center of the 21st reaches of the space vehicle, and a rail transport- century began life in the early 1960s when new er. An arming tower would stand about midway Facts facilities were needed to launch the moon-bound between the assembly building and the pads. Saturn V rockets. The Apollo Saturn would carry a number of Initial plans called for a launch complex hazardous explosives: the launch escape system comprising a Vertical Assembly Building (VAB), (the tower on top of the vehicle that lifted the a launcher-transporter, an arming area and a spacecraft away from the launch vehicle in case launch pad. The VAB would consist of assembly of an emergency), retrorockets to separate the bay areas for each of the stages, with a high-bay stages, ullage rockets to force fuel to the bottom unit approximately 110 meters in height for final of tanks, and the launch vehicle’s destruct system. assembly and checkout of the vehicle. Buildings These plans would be modified during NASA NASA Launch Pad 39A is under construction (foreground) with the imposing Vertical Assembly Building rising from the sand in the background. -
MIT Japan Program Working Paper 01.10 the GLOBAL COMMERCIAL
MIT Japan Program Working Paper 01.10 THE GLOBAL COMMERCIAL SPACE LAUNCH INDUSTRY: JAPAN IN COMPARATIVE PERSPECTIVE Saadia M. Pekkanen Assistant Professor Department of Political Science Middlebury College Middlebury, VT 05753 [email protected] I am grateful to Marco Caceres, Senior Analyst and Director of Space Studies, Teal Group Corporation; Mark Coleman, Chemical Propulsion Information Agency (CPIA), Johns Hopkins University; and Takashi Ishii, General Manager, Space Division, The Society of Japanese Aerospace Companies (SJAC), Tokyo, for providing basic information concerning launch vehicles. I also thank Richard Samuels and Robert Pekkanen for their encouragement and comments. Finally, I thank Kartik Raj for his excellent research assistance. Financial suppport for the Japan portion of this project was provided graciously through a Postdoctoral Fellowship at the Harvard Academy of International and Area Studies. MIT Japan Program Working Paper Series 01.10 Center for International Studies Massachusetts Institute of Technology Room E38-7th Floor Cambridge, MA 02139 Phone: 617-252-1483 Fax: 617-258-7432 Date of Publication: July 16, 2001 © MIT Japan Program Introduction Japan has been seriously attempting to break into the commercial space launch vehicles industry since at least the mid 1970s. Yet very little is known about this story, and about the politics and perceptions that are continuing to drive Japanese efforts despite many outright failures in the indigenization of the industry. This story, therefore, is important not just because of the widespread economic and technological merits of the space launch vehicles sector which are considerable. It is also important because it speaks directly to the ongoing debates about the Japanese developmental state and, contrary to the new wisdom in light of Japan's recession, the continuation of its high technology policy as a whole. -
+ STS-123 Press
CONTENTS Section Page STS-123 MISSION OVERVIEW................................................................................................ 1 TIMELINE OVERVIEW.............................................................................................................. 11 MISSION PROFILE................................................................................................................... 15 MISSION PRIORITIES............................................................................................................. 17 MISSION PERSONNEL............................................................................................................. 19 STS-123 ENDEAVOUR CREW .................................................................................................. 21 PAYLOAD OVERVIEW .............................................................................................................. 31 KIBO OVERVIEW.................................................................................................................................. 31 KIBO MISSION CONTROL CENTER ....................................................................................................... 39 TSUKUBA SPACE CENTER.................................................................................................................... 43 SPACE STATION INTEGRATION AND PROMOTION CENTER .................................................................. 47 JAXA’S EXPERIMENTS DURING THE 1J/A STAGE................................................................................. -
N AS a Facts
National Aeronautics and Space Administration NASA’s Launch Services Program he Launch Services Program (LSP) manufacturing, launch operations and rockets for launching Earth-orbit and Twas established at Kennedy Space countdown management, and providing interplanetary missions. Center for NASA’s acquisition and added quality and mission assurance in In September 2010, NASA’s Launch program management of expendable lieu of the requirement for the launch Services (NLS) contract was extended launch vehicle (ELV) missions. A skillful service provider to obtain a commercial by the agency for 10 years, through NASA/contractor team is in place to launch license. 2020, with the award of four indefinite meet the mission of the Launch Ser- Primary launch sites are Cape Canav- delivery/indefinite quantity contracts. The vices Program, which exists to provide eral Air Force Station (CCAFS) in Florida, expendable launch vehicles that NASA leadership, expertise and cost-effective and Vandenberg Air Force Base (VAFB) has available for its science, Earth-orbit services in the commercial arena to in California. and interplanetary missions are United satisfy agencywide space transporta- Other launch locations are NASA’s Launch Alliance’s (ULA) Atlas V and tion requirements and maximize the Wallops Flight Facility in Virginia, the Delta II, Space X’s Falcon 1 and 9, opportunity for mission success. Kwajalein Atoll in the South Pacific’s Orbital Sciences Corp.’s Pegasus and facts The principal objectives of the LSP Republic of the Marshall Islands, and Taurus XL, and Lockheed Martin Space are to provide safe, reliable, cost-effec- Kodiak Island in Alaska. Systems Co.’s Athena I and II.