DOCSLIB.ORG

Beyond Shipbuilding 1-3 Space Ventures 4 Innovative Spirit 5 Quick Hits 6 2Nd Quarter Briefs 7

Total Page：16

File Type：pdf, Size：1020Kb

Download full-text PDF Read full-text
Beyond Shipbuilding 1-3 Space Ventures 4 Innovative Spirit 5 Quick Hits 6 2Nd Quarter Briefs 7 MISSISSIPPI GULF COAST ALLIANCE FOR ECONOMIC DEVELOPMENT July 2011 - Volume V Issue II aerospace ∙ advanced materials ∙ shipbuilding ∙ geospatial ∙ marine science Inside this Issue: Beyond Shipbuilding 1-3 Space Ventures 4 Innovative Spirit 5 Quick Hits 6 2nd Quarter Briefs 7 The Alliance is an independent partnership serving the six Mississippi counties nearest the Gulf of Mexico. Beyond Shipbuilding Hancock Development Composite deckhouse for the DDG 1000 Zumwalt class ship. Photo courtesy of Ingall's Shipbuilding Commission they do it. And it is impressive. Harrison County Technology has changed the way ships are built, and one They build huge composite structures for Development Commission Navy ships, including components for the facility eyeing the future is next generation DDG 1000 Zumwalt-class Jackson County Ingalls’ Gulfport operation… destroyer. And one thing that will really get Economic Development Jenkins talking is a discussion about new Foundation Jay Jenkins is quite enthusiastic when ventures the company is eyeing. he takes a visitor around the facilities How about wind blade construction and Mississippi Power Company at Ingalls Shipbuilding’s Gulfport repair, or bridges and roadway sections? Operations. The site director of the None of that is too far afield. And, as if to company’s Composites Center of drive home the point, not long ago the team Excellence takes pleasure showing what in Gulfport built an emergency escape they do in Gulfport, and explaining how composite fairing for the crew capsule (Beyond Shipbuilding continued, page 2) Copyright 2010-2011, Alliance Insight Beyond Shipbuilding (continued from page 1) of the now-defunct Constellation Program. But that is shipbuilding - of the spaceship variety. “I’m very excited about the future, because of the capabilities and the folks that we have working here. This is a world-class facility. We’re the only ones that can build marine carbon fiber composites in the size that we build them. Nobody else in the world can do that.” The Gulfport operation has been building composite parts for ships for a long time, but Jenkins sees a lot of new fields on the horizon. “Looking to the future, I see the possibilities as endless in terms of what we can do in support of marine composites, in support of civil infrastructure - bridges, roadways, those types of things - in terms of alternative energy capabilities. I think that Gulfport and the composite center of excellence at Gulfport has nearly unlimited world-class capability for future work here.” Jenkins being comfortable with change isn’t that surprising. Change has been the norm for the company since the start of the year. The Company Ingalls Shipbuilding Gulfport Operations is part of Ingalls Shipbuilding, which in turn is a part of the 38,000 employee Huntington Ingalls Industries of Newport News, Va. The company, with operations in Mississippi, Virginia, Louisiana and California, was spun off from Northrop Grumman in March 2011, in part because the shipbuilding portion of Northrop Grumman did The composite mast being built for one of the company’s amphibious ships. Gulfport has not mesh with the focus areas of that company. been building them since 2001. Photo courtesy of Ingall's Shipbuilding Northrop acquired the shipyard when it bought Litton Industries. the DDG 51 destroyer program beyond the first two vessels. Ingalls Shipbuilding has three sites across the Gulf The company could also see more Coast Guard cutter activity, Coast with nearly 11,000 employees: Mississippi’s and will begin building the Hamilton this summer, according Gulfport and Pascagoula operations, as well as the to the Mississippi Press. Avondale, La., shipyard. In 2013, the Avondale will be But among U.S. shipbuilders, Ingalls has the only composite shut down. Earlier, the Tallulah, La., facility was closed. center of excellence. Other companies, even shipbuilders, All of Avondale’s work will be consolidated in Pascagoula also craft vessels out of composites. But none is involved Ingalls is building 28 of the 62 ship DDG 51 class of in programs on the scale and scope of the work done at the Aegis guided missile destroyers for the Navy. It’s also the composite shop. builder of record for the LPD, LHD and LHA classes of amphibious assault ships, and builder of the U.S. Coast Composites Center Guard’s National Security Cutter. The Gulfport operation is a multi-building facility that Right now the Ingalls shipyard in Pascagoula has an occupies a 120-acre site in Bernard Bayou Industrial District. $18 billion backlog that will carry it into 2018. In April It has done composite structures ranging from small combatant it was awarded a $1.5 billion contract to build LPD 26, craft of less than 200 feet to lightweight aerospace structures. its 10th amphibious transport dock ship. This year and It has a workforce of 500, according to the company’s website. next there could be one more amphibious transport dock contract to come on line, as well as a continuation of (Beyond Shipbuilding continued, page 3) Alliance Insight • Volume V Issue II • Page 2 Beyond Shipbuilding (continued from page 2) Gulfport has been building composite masts for the LPD 17 program since 2001. The mast is a detachable, octagon-shaped structure 93 feet high and 35 feet in diameter constructed of a multilayer, frequency selective material designed to allow passage of specific radio frequencies while reflecting others. As strong as steel, composites are resistant to corrosion, lightweight, stealthy and have reduced maintenance costs. One key benefit is electronics can be integrated into the structure, a key reason for composite masts. But composites are more costly. Gulfport’s experience goes back to the hand layup fabrication technology used in the MHC 51 Osprey 4 class mine hunters. Today they use very different techniques, including vacuum assisted resin transfer molding (VARTM). In addition to masts for LPD 17, the Gulfport operation has also built a mast for the carrier USS George H.W. Bush (CVN 77) to replace a steel mast, and other topside structures for the CVN 78 Ford class of carrier. But it’s the work on the DDG 1000 class of ship that is particularly striking for the size of Huge bolts are used to attach composite structures to metal portions of the ship. the structures alone. The Zumwalt class is being This is from the DDG 1000 deckhouse being built by Ingalls. built by General Dynamics’ Bath Iron Works Photo courtesy of Ingall's Shipbuilding in Maine, but Ingalls is a major contractor. It’s building the ship’s integrated composite deckhouses and helicopter hangars, as well as parts Looking to the Future of the ships’ peripheral vertical launch systems. Ingalls is looking at four areas of opportunity: major Ingalls had to build a new set of manufacturing composite structures, topside components and radomes, small buildings to handle work on the Zumwalt, whose composite structures and commercial products. deckhouse is nearly double the width and five times While shipbuilding will continue to be the primary activity the length of the Antonio-class ship masts, according for the Gulfport operation, the company understands there are to Aviation Week. opportunities that go beyond the shipbuilding field. And that’s “I can do multiple composite processes, and I can where Jenkins wants to go. do different types of processes at the same time because “Pick an industry or pick a type of construction,” said I have a plant that’s large enough and a work force that’s Jenkins. “It would include everything from wind blade repair diverse enough and skilled enough to be able to do those, and construction to potentially roadbeds to offshore oil regardless of where the project is and how big it is,” platforms, where we could build composite structures that Jenkins told Alliance Insight. don’t corrode and are lightweight so it gives the structure The biggest panels can take more than 24 hours to further capability to do what they need to do. infuse with resin and cure. The company has adapted And aerospace? some composite-industry processes and developed some “I think we can do small parts, covers, and those kinds of of its own to infuse and cure the resin and then check each things, shields, cowlings, things that don’t require autoclaves, piece with special ultrasonic inspection equipment. we can use an out of autoclave process for manufacturing That’s a major investment for a ship class that has been if we can get the engineering and the tooling we can do the cut from about two dozen ships down to its current three. process.” But the Navy likes composites for topside structures, and For Ingalls’ Gulfport operation, it’s all a matter of trying the investment Ingalls has made may be worth it. to see what’s over the horizon. – David Tortorano Alliance Insight • Volume V Issue II • Page 3 ——————————— advanced materials/shipbuilding ———————————— Shipbuilding Center Ventures into Space Ingalls Shipbuilding Gulfport Operations is known for its work building composite structures for the Navy’s fleet. But less known is that it also ventured into aerospace when it built a composite fairing for NASA’s now-aborted Constellation Program. While the Gulfport Composites Center of Excellence was still part of defense giant Northrop Grumman, workers at the Gulfport operation built the nose piece, called a fairing, for the Max Launch Abort System (MLAS). The MLAS was designed to provide a quick escape from a launch vehicle, the Ares I, in case of emergency on the launch pad or in the initial stages of launch. The MLAS concept for an operational vehicle would have four or more solid rocket motors attached inside the bullet-shaped composite fairing.
Load more

Recommended publications
  • Nasa Engineering & Safety Center
    National Aeronautics and Space Administration NASA ENGINEERING & SAFETY CENTER 2008 TECHNICAL UPDATE www.nasa.gov 1 It gives me a lot of pleasure to recognize the 5th anniversary of the establishment of the NASA Engineering and Safety Center. It also offers, for me, a valuable reminder that it is important always to be open to new ideas and new approaches to solving problems. When the NESC was established, I was more than a bit pessimistic that it could work, that it could provide value for the Agency over and above that offered by our various center engineering directorates. I was wrong. The synergy that has been achieved by the NESC and its cross-agency approach to solving difficult technical problems has been truly impressive. It is, in my mind, a useful model for future endeavors and a great example that it is actually possible for us to “be NASA”, to rise above some of the parochial geographic concerns which have plagued NASA for five decades. These days, when someone tells me that the NESC is looking at a particular issue, I am reassured, because I know that if a solution can be found, this group will find it. – Dr. Michael D. Griffin, NASA Administrator 2 Table of Contents Stakeholder Messages ........................................................................................ 2 NESC Leadership ................................................................................................ 3 Overview: How the NESC Works .......................................................................... 4 NESC Academy: Learning from the Past ............................................................... 8 Technical Highlights Collecting Flight Force Measurements to Improve Coupled Loads Analysis ... 11 Analysis of Constellation Program Mass Properties ....................................... 11 Prediction and Reduction of Ares SRB Thrust Oscillation ............................... 12 Review of the Launch Abort System Motor Qualification Plan .......................
    [Show full text]
  • THE MAX LAUNCH ABORT SYSTEM – CONCEPT, FLIGHT TEST, and EVOLUTION Michael G
    THE MAX LAUNCH ABORT SYSTEM – CONCEPT, FLIGHT TEST, AND EVOLUTION Michael G. Gilbert(1), PhD (1) Principal Engineer, NASA Engineering and Safety Center 11 Langley Blvd., MS 116,Hampton VA 23681 USA Email:[email protected] Abstract escape system Maxime Faget [1]. The effort was intended to provide The NASA Engineering and Safety Center programmatic risk-reduction for the (NESC) is an independent engineering Constellation Program (CxP) Orion Crew analysis and test organization providing Exploration Vehicle (CEV) project. support across the range of NASA programs. In 2007 NASA was developing The CEV project baseline Launch Abort the launch escape system for the Orion System (LAS) development is an evolution spacecraft that was evolved from the of the Apollo towered-rocket design, Fig. traditional tower-configuration escape 2. Unlike the Apollo LAS, the CEV LAS systems used for the historic Mercury and incorporated an attitude control motor to Apollo spacecraft. The NESC was tasked, ensure stable flight following the escape as a programmatic risk-reduction effort to motor burn. At the time the MLAS project develop and flight test an alternative to the was initiated, the CEV LAS was Orion baseline escape system concept. experiencing development delays related This project became known as the Max to the LAS attitude control motor. Launch Abort System (MLAS), named in Therefore, the MLAS project was to honor of Maxime Faget, the developer of consider escape system concepts that the original Mercury escape system. Over would not require active attitude control or the course of approximately two years the stabilization following escape motor NESC performed conceptual and tradeoff burnout.
    [Show full text]
  • Testing Strategies and Methodologies for the Max Launch Abort System Dawn M
    Testing Strategies and Methodologies for the Max Launch Abort System Dawn M. Schaible Daniel E. Yuchnovicz NASA Engineering and Safety Center Hampton, Virginia ABSTRACT The National Aeronautics and Space Administration (NASA) Engineering and Safety Center (NESC) was tasked to develop an alternate, tower-less launch abort system (LAS) as risk mitigation for the Orion Project. The successful pad abort flight demonstration test in July 2009 of the “Max” launch abort system (MLAS) provided data critical to the design of future LASs, while demonstrating the Agency’s ability to rapidly design, build and fly full-scale hardware at minimal cost in a “virtual” work environment. Limited funding and an aggressive schedule presented a challenge for testing of the complex MLAS system. The successful pad abort flight demonstration test was attributed to the project’s systems engineering and integration process, which included: a concise definition of, and an adherence to, flight test objectives; a solid operational concept; well defined performance requirements, and a test program tailored to reducing the highest flight test risks. The testing ranged from wind tunnel validation of computational fluid dynamic simulations to component ground tests of the highest risk subsystems. This paper provides an overview of the testing/risk management approach and methodologies used to understand and reduce the areas of highest risk — resulting in a successful flight demonstration test. KEY WORDS: Testing, risk management, flight test, launch abort systems MLAS PROJECT OVERVIEW NASA’s next generation crewed spacecraft, named Orion, is a part of the overall Constellation Program. The baseline Orion design includes a launch abort system (LAS) with tower, derived from the Apollo design.
    [Show full text]
  • Inside Wallops National Aeronautics and Space Administration Goddard Space Flight Center Wallops Flight Facility, Wallops Island, Va
    Inside Wallops National Aeronautics and Space Administration Goddard Space Flight Center Wallops Flight Facility, Wallops Island, Va. Volume XX-08 Number 10 March 24, 2008 Max Launch Abort System Development Early last year, the Wallops Flight Facility enough and with enough distance Representatives from the Sounding embarked on a challenging effort to downrange to permit the CM to execute a Rockets Program Office and NASA support NASA Engineering and Safety nominal landing. Sounding Rocket Operations Contract, Center (NESC) with the development of (NSROC), have provided technical a composite crew module for the In addition to a wealth of solid rocket motor support associated with the solid rocket Exploration Orion spacecraft. knowledge and experience at Wallops, the motor systems. NSROC will play a major NESC found an engineering staff well- role in vehicle hardware and mechanical The NESC will design, develop, and test suited to rapid-response system GSE fabrication. an alternate concept launch abort system development. Personnel from many (LAS) for the Orion crew module (CM) Wallops organizations have joined the Team members from the Facilities as a risk mitigation for the Orion Project’s MLAS team. LAS development. Management Branch are responsible for procurement and construction of a custom Having an effective means for the crew The Wallops’ Guidance, Navigation & launch pad shelter and for infrastructure to escape in an emergency during launch Control and Mission Systems Engineering improvements related to transportation of is critical in establishing launch system Branch, have supported design and flight the MLAS demonstrator from the Wallops reliability and crew safety for the dynamics analysis.
    [Show full text]
  • Changing the Shape of Launch Abort Systems
    featured knowledge Changing the Shape of Launch Abort Systems n December 2014, NASA’s Orion Starting in December 2006, IMulti-Purpose Crew Vehicle they performed aerodynamic, (MPCV) Program successfully structural and controls analyses, conducted Experimental Flight as well as a number of wind tunnel Test-1 (EFT-1), the first orbital flight experiments, to obtain the data test of the Orion spacecraft. Close required to validate the concept. observers may have noted that the “We found that adding a fairing spacecraft had an updated shape improved the aerodynamic shape from the concepts included on the significantly,” said Schuster. “It previous Ares I-X and Orion Pad reduced drag during ascent, as well Abort 1 flight tests. In reality, the as weight by providing a separate Orion crew module (CM) shape has load path around the crew module.” not changed substantially since In addition to better quantifying these flights, but the Orion Launch the aerodynamic, performance, Abort System (LAS) has changed. and structural improvements, Reducing structural loads a major new focus investigated using the ALAS MBPC to reduce In September 2006, during a peer aeroacoustic loads on the Orion review of the NESC Composite CM. “Current predictions of Orion Crew Module (CCM) Assessment, acoustic loads far exceeded what an Alternate Launch Abort System was assumed in the design of the (ALAS) was conceived to reduce Orion subsystems,” said Scotti. structural loads carried by the “And the project hoped that the CCM during a flight abort. To ALAS approach would help solve further investigate the feasibility that problem and eliminate the of the ALAS concept, Dr.
    [Show full text]
  • Toward a History of the Space Shuttle an Annotated Bibliography
    Toward a History of the Space Shuttle An Annotated Bibliography Part 2, 1992–2011 Monographs in Aerospace History, Number 49 TOWARD A HISTORY OF THE SPACE SHUTTLE AN ANNOTATED BIBLIOGRAPHY, PART 2 (1992–2011) Compiled by Malinda K. Goodrich Alice R. Buchalter Patrick M. Miller of the Federal Research Division, Library of Congress NASA History Program Office Office of Communications NASA Headquarters Washington, DC Monographs in Aerospace History Number 49 August 2012 NASA SP-2012-4549 Library of Congress – Federal Research Division Space Shuttle Annotated Bibliography PREFACE This annotated bibliography is a continuation of Toward a History of the Space Shuttle: An Annotated Bibliography, compiled by Roger D. Launius and Aaron K. Gillette, and published by NASA as Monographs in Aerospace History, Number 1 in December 1992 (available online at http://history.nasa.gov/Shuttlebib/contents.html). The Launius/Gillette volume contains those works published between the early days of the United States’ manned spaceflight program in the 1970s through 1991. The articles included in the first volume were judged to be most essential for researchers writing on the Space Shuttle’s history. The current (second) volume is intended as a follow-on to the first volume. It includes key articles, books, hearings, and U.S. government publications published on the Shuttle between 1992 and the end of the Shuttle program in 2011. The material is arranged according to theme, including: general works, precursors to the Shuttle, the decision to build the Space Shuttle, its design and development, operations, and management of the Space Shuttle program. Other topics covered include: the Challenger and Columbia accidents, as well as the use of the Space Shuttle in building and servicing the Hubble Space Telescope and the International Space Station; science on the Space Shuttle; commercial and military uses of the Space Shuttle; and the Space Shuttle’s role in international relations, including its use in connection with the Soviet Mir space station.
    [Show full text]
  • Launch Abort System Evolution
    featured knowledge Launch Abort System Evolution critical component of crewed spacecraft, the launch Aabort system (LAS), allows for rescue of the crew in the event of a catastrophic malfunction while the spacecraft is sitting on the launch pad or on its way into orbit. For a successful rescue, however, the LAS must perform several critical maneuvers in rapid-fire succession. First, the launch abort motors must be powerful enough to fly the fairing and crew module (CM) to a safe distance away from the launch vehicle. Next, it must reorient and fly in a carefully controlled heat shield-forward attitude. Finally, it must release the CM, enabling the CM’s parachute landing system to deploy for a safe return of the crew. LAS begins with Project Mercury Since the time of Project Mercury and the Apollo Program, the LAS has maintained its traditional tower configuration. But as spacecraft design has evolved, so has the need for a new LAS. The Orion Multi-Purpose Propulsively stabilized MLAS concept. Crew Vehicle launched on December 4, 2014, featured a new Alternative Launch Abort System (ALAS) shape and structure that enhanced the aerodynamic and aeroacoustic performance of the spacecraft. But while the NESC was spearheading efforts on the ALAS design, it was also developing the Max Launch Abort System (MLAS), a follow-on to the ALAS design that incorporated the ALAS shape while fundamentally changing the LAS from a tower to a towerless design. Named in honor of Maxime Faget, developer of the original Mercury launch escape system, MLAS was a 2-year effort Left: Successful launch abort test of the passively stabilized that culminated in a full-scale flight demonstration.
    [Show full text]
  • Lunar Outpost the Challenges of Establishing a Human Settlement on the Moon Erik Seedhouse Lunar Outpost the Challenges of Establishing a Human Settlement on the Moon
    Lunar Outpost The Challenges of Establishing a Human Settlement on the Moon Erik Seedhouse Lunar Outpost The Challenges of Establishing a Human Settlement on the Moon Published in association with Praxis Publishing Chichester, UK Dr Erik Seedhouse, F.B.I.S., As.M.A. Milton Ontario Canada SPRINGER±PRAXIS BOOKS IN SPACE EXPLORATION SUBJECT ADVISORY EDITOR: John Mason, M.Sc., B.Sc., Ph.D. ISBN 978-0-387-09746-6 Springer Berlin Heidelberg New York Springer is part of Springer-Science + Business Media (springer.com) Library of Congress Control Number: 2008934751 Apart from any fair dealing for the purposes of research or private study, or criticism or review, as permitted under the Copyright, Designs and Patents Act 1988, this publication may only be reproduced, stored or transmitted, in any form or by any means, with the prior permission in writing of the publishers, or in the case of reprographic reproduction in accordance with the terms of licences issued by the Copyright Licensing Agency. Enquiries concerning reproduction outside those terms should be sent to the publishers. # Praxis Publishing Ltd, Chichester, UK, 2009 Printed in Germany The use of general descriptive names, registered names, trademarks, etc. in this publication does not imply, even in the absence of a speci®c statement, that such names are exempt from the relevant protective laws and regulations and therefore free for general use. Cover design: Jim Wilkie Project management: Originator Publishing Services, Gt Yarmouth, Norfolk, UK Printed on acid-free paper Contents Preface ............................................. xiii Acknowledgments ...................................... xvii About the author....................................... xix List of ®gures ........................................ xxi List of tables ........................................
    [Show full text]
  • Space Applications for Wireless Sensors W
    Space Applications for Wireless Sensors W. C. Wilson*, G. M. Atkinson** *NASA Langley Research Center, Hampton, VA, USA, [email protected] **Virginia Commonwealth University, Richmond, VA, USA, [email protected] ABSTRACT consuming to route, identify and validate cabling required for the hundreds of sensors on the CCM. If the cables are From ground tests to operations on orbit and on the eliminated through the use of wireless sensors, then the Moon, many space applications could benefit from small, time for cable setup would be eliminated and the overall passive, wireless sensors. Eliminating wires in spacecraft costs would be reduced. could reduce launch costs through the reduction of mass and lead to reduced fabrication costs. Development of 2 SPACE APPLICATIONS wireless Vehicle Health Monitoring Systems (VHMS) will enable more sensors and increase safety. It is for these The Space Shuttle would benefit from wireless sensors reasons that NASA is investigating the use of wireless that can: track fatigue life, detect impacts, verify the technology for a variety of spacecraft applications. This environment, and maintain insight into the space shuttle as paper will present a survey of opportunities for universities, a system [5]. Passive RFID sensor tags are being industry, and other governmental agencies to partner in investigated for monitoring over temperature conditions on developing new wireless sensors to address the future the space shuttle thermal protection tiles [6]. Although the sensing needs. shuttle program is ending, the X-37B Orbital Test Vehicle was launched by the Airforce on April 22, 2010 (Fig. 1). Keywords: wireless sensors, spacecraft, sensors networks.
    [Show full text]
  • 2009 Technical Update
    National Aeronautics and Space Administration NASA ENGINEERING & SAFETY CENTER NESC 2009 TECHNICAL UPDATE www.nasa.gov CONTENTS Stakeholder Messages ................................... 2 Leadership Message ...................................... 3 NESC Overview .............................................. 4 Technical Highlights ........................................ 9 Exploration ................................................... 10 General ........................................................ 21 Space Operations ........................................ 31 Science ....................................................... 36 Center Focus ................................................. 38 Honor Awards ................................................ 50 Biographies .................................................... 52 Alumni ............................................................ 56 Publications .................................................... 57 (Left) Ares I-X in the Vehicle Assembly Building during stacking. On the cover: Launch of the Max Launch Abort System Flight Test Vehicle from Wallops Flight Facility. Inset photos: top, Shell Buckling Test Facility at MSFC; middle, Composite Crew Module at ATK facilities in Iuka, Missis- sippi; bottom, Finite Element Models of Anthropomorphic Test Devices. Back cover: MLAS crew module descends under fully deployed main para- chutes. Photo by Ryan Henriksen/The Virginian-Pilot. All photos in this publication are credited to NASA except where indicated. STAKEHOLDER MESSAGES t is
    [Show full text]
  • 2010 US Commercial Space Transportation
    Federal Aviation Administration 2010 U.S. Commercial Space Transportation Developments and Concepts: Vehicles, Technologies, and Spaceports January 2010 HQ-101068.INDD 2010 U.S. Commercial Space Transportation Developments & 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 encourage, 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://www.faa.gov/about/office_org/headquarters_offices/ast/. 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. • i • Federal Aviation Administration / Commercial Space Transportation • ii • 2010 U.S. Commercial Space Transportation Developments & Concepts • Contents Table of Contents Introduction . .1 Space competitionS . 1 expendable launch Vehicle induStry . 2 reuSable launch Vehicle induStry . 2 reentry VehicleS and in-Space technology . 3 enabling technologieS . 3 commercial human Spaceflight training . 4 SpaceportS . 4 regulatory and legiSlatiVe deVelopmentS . 4 Significant 2009 Events.
    [Show full text]
  • Space Transportation Technology Roadmap
    WWW.NASAWATCH.COM Space Transportation Technology Roadmap A Collaboration by Government and Industry To Address U.S. Government and Commercial Space Transportation Needs Release 1.0 21 October 2010 WWW.NASAWATCH.COM WWW.NASAWATCH.COM Please direct any suggestions on this roadmap to: Paul E. Damphousse LtCol, USMC Chief of Advanced Concepts National Security Space Office Pentagon, Washington DC / Fairfax, VA W (571) 432-1411 C (571) 405-0749 [email protected] - 1 - WWW.NASAWATCH.COM WWW.NASAWATCH.COM Table of Contents EXECUTIVE SUMMARY....................................................................................................... …6 1 ROADMAP OBJECTIVES.................................................................................................... ....8 2 ROADMAP BACKGROUND............................................................................................... ..10 3 ROADMAP METHODOLOGY............................................................................................ ..18 3.1 MODELS AND REFERENCES EMPLOYED FOR THE ROADMAP…………..… ..18 3.1.1 FUNDAMENTALS OF TECHNOLOGY ROADMAPPING…………………. ..18 3.1.2 DOD RECHNOLOGY READINESS ASSESSMENTS DESKBOOK……….....18 3.1.3 SPACE-BASED SOLAR POWER STUDY…………………………………… ..19 4 PHASE 1: PRELIMINARY FOUNDATION PHASE.......................................................... ..20 4.1 SATISFYING THREE (3) ESSENTIAL CONDITIONS............................................. ..20 4.1.1 THE THREE CONDITIONS DEFINED………………………………………. ..20 4.1.2 ASSUMING THE 1ST CONDITION IS MET………………………………….
    [Show full text]