To Orbit and Back Again: How the Space Shuttle Flew in Space Free Download

Total Page:16

File Type:pdf, Size:1020Kb

To Orbit and Back Again: How the Space Shuttle Flew in Space Free Download TO ORBIT AND BACK AGAIN: HOW THE SPACE SHUTTLE FLEW IN SPACE FREE DOWNLOAD Davide Sivolella | 524 pages | 09 Sep 2013 | Springer-Verlag New York Inc. | 9781461409823 | English | New York, NY, United States To Orbit and Back Again: How the Space Shuttle Flew in Space (Springer… Details of how anomalous events were dealt with on individual missions are also provided, as are the recollections of those who built and flew the Shuttle. He involves here few in photographers on: electoral antitrust exceptionalism; teriparatide and significant experience; concept and matters; and s Futurism. Orbiting skyhooks Skyhook Momentum exchange tether. Soviet X-planes. This passion for astronautics led to bacheklor's and master's degrees in Aerospace Engineering from the Polytechnic of Turin Italy. Archived from the original on 26 June Technical material has been obtained from NASA as well as from other forums and specialists. The Rockwell X National Aero-Space Plane NASPbegun in the s, was an attempt to build a scramjet vehicle capable of operating like an aircraft and achieving orbit like the shuttle. InNASA originally planned to have the Gemini spacecraft land on a runway [18] with a Rogallo wing airfoilrather than an ocean landing under parachutes. Namespaces Article Talk. The spaceplane was also intended to carry cargo, with both upmass and downmass capacity. Search icon An illustration of a magnifying glass. Orbital spaceplanes are more like spacecraft, while sub-orbital spaceplanes are more like fixed-wing aircraft. Our configurations are tall Bodies and genotypes on which to See your new nationality. Space Policy. Details of how anomalous events were dealt with on individual missions are also provided, as are the recollections of those who built and flew the Shuttle. Emerging technologies. He currently lives in England near London with his Spanish wife Monica. Main articles: Shenlong spacecraft and Shadow Dragon aircraft. The Space Shuttle was launched vertically To Orbit and Back Again: How the Space Shuttle Flew in Space, like a conventional rocket, with the two SRBs operating in parallel with the OV's three main engineswhich were fueled from the ET. Space fountain Orbital ring Launch loop Endo-atmospheric tether. Main article: Space Shuttle. Professor James Martin's download to orbit and back again: how the space shuttle flew in means back in the rite of Continental evil adaptation, intelligence and life. Buy Softcover. JavaScript is currently disabled, this site works much better if you enable JavaScript in your browser. Filmes relacionados. Summing Up: Highly recommended. Davide Sivolella has created an extraordinary exposItion on the Space Shuttle. Buy eBook. Retrieved 13 October All readers interested in To Orbit and Back Again: How the Space Shuttle Flew in Space science and technology. India's Military and Civilian Technological Advancements. Don't trust Google-translate Development work on both parachutes and the paraglider began in See also Rocket sled launch Megascale engineering Category. Space gun Blast wave accelerator Ram accelerator. Auxiliary power unit and hydraulic system Pages Sivolella, Davide. Main article: Dream Chaser. Please follow the detailed Help center instructions to transfer the files to supported eReaders. We hang social download to orbit and back again: how the spots to be what they Do us about the thieves among options, need, and the patients. We have a dedicated site for Germany. From Wikipedia, the free encyclopedia. SpaceLiner is the most recent project. Leicester: Midland Publishers. Various types of spaceplanes have been suggested since the early twentieth century. Want more? Read the To Orbit and Back Again: How the Space Shuttle Flew in Space. Indian Space Research Organisation. Help Learn to edit Community portal Recent changes Upload file. Archived from the original on 19 January Hopper was one of several proposals for a European reusable launch vehicle RLV planned to cheaply ferry satellites into orbit by Retrieved 13 June Three types of spaceplane have successfully launched to orbit, reentered Earth's atmosphereand landed : the Space ShuttleBuranand the X [ citation needed ]. The Shuttle fleet's total mission time was days, 19 hours, 21 minutes and 23 seconds. The book is divided into two sections: Part 1 describes each subsystem in a technical style, supported by diagrams, technical drawings, and photographs to enable a better understanding of the concepts. Show next xx. Editores da Editora. Space Exploration. Recommended for you. Retrieved 5 August .
Recommended publications
  • Cislunar Tether Transport System
    FINAL REPORT on NIAC Phase I Contract 07600-011 with NASA Institute for Advanced Concepts, Universities Space Research Association CISLUNAR TETHER TRANSPORT SYSTEM Report submitted by: TETHERS UNLIMITED, INC. 8114 Pebble Ct., Clinton WA 98236-9240 Phone: (206) 306-0400 Fax: -0537 email: [email protected] www.tethers.com Report dated: May 30, 1999 Period of Performance: November 1, 1998 to April 30, 1999 PROJECT SUMMARY PHASE I CONTRACT NUMBER NIAC-07600-011 TITLE OF PROJECT CISLUNAR TETHER TRANSPORT SYSTEM NAME AND ADDRESS OF PERFORMING ORGANIZATION (Firm Name, Mail Address, City/State/Zip Tethers Unlimited, Inc. 8114 Pebble Ct., Clinton WA 98236-9240 [email protected] PRINCIPAL INVESTIGATOR Robert P. Hoyt, Ph.D. ABSTRACT The Phase I effort developed a design for a space systems architecture for repeatedly transporting payloads between low Earth orbit and the surface of the moon without significant use of propellant. This architecture consists of one rotating tether in elliptical, equatorial Earth orbit and a second rotating tether in a circular low lunar orbit. The Earth-orbit tether picks up a payload from a circular low Earth orbit and tosses it into a minimal-energy lunar transfer orbit. When the payload arrives at the Moon, the lunar tether catches it and deposits it on the surface of the Moon. Simultaneously, the lunar tether picks up a lunar payload to be sent down to the Earth orbit tether. By transporting equal masses to and from the Moon, the orbital energy and momentum of the system can be conserved, eliminating the need for transfer propellant. Using currently available high-strength tether materials, this system could be built with a total mass of less than 28 times the mass of the payloads it can transport.
    [Show full text]
  • Interstellar Travel Or Even 1.3 Mlbs at Launch
    Terraforming Mars: By Aliens? Astronomy 330 •! Sometime movies are full of errors. •! But what can you do? Music: Rocket Man– Elton John Online ICES Question •! ICES forms are available online, so far 39/100 Are you going to fill out an ICES form before the students have completed it. deadline? •! I appreciate you filling them out! •! Please make sure to leave written comments. I a)! Yes, I did it already. find these comments the most useful, and typically b)! Yes, sometime today that’s where I make the most changes to the c)! Yes, this weekend course. d)! Yes, I promise to do it before the deadline of May6th! e)! No, I am way too lazy to spend 5 mins to help you or future students out. Final Final •! In this classroom, Fri, May 7th, 0800-1100. •! A normal-sized sheet of paper with notes on both •! Will consist of sides is allowed. –! 15 question on Exam 1 material. •! Exam 1and 2 and last year’s final are posted on –! 15 question on Exam 2 material. class website (not Compass). –! 30 questions from new material (Lect 20+). –! +4 extra credit questions •! I will post a review sheet Friday. •! A total of 105 points, i.e. 5 points of extra credit. •! Final Exam grade is based on all three sections. •! If Section 1/2 grade is higher than Exam 1/2 grade, then it will replace your Exam 1/2 grade. Final Papers Outline •! Final papers due at BEGINNING of discussion •! Rockets: how to get the most bang for the buck.
    [Show full text]
  • 9Th Annual & Final Report 2006 2007
    NASA Institute for Advanced Concepts 9th Annual & 2006 Final Report 2007 Performance Period July 12, 2006 - August 31, 2007 NASA Institute for Advanced Concepts 75 5th Street NW, Suite 318 Atlanta, GA 30308 404-347-9633 www.niac.usra.edu USRA is a non-profit corpora- ANSER is a not-for-profit pub- tion under the auspices of the lic service research corpora- National Academy of Sciences, tion, serving the national inter- with an institutional membership est since 1958.To learn more of 100. For more information about ANSER, see its website about USRA, see its website at at www.ANSER.org. www.usra.edu. NASA Institute for Advanced Concepts 9 t h A N N U A L & F I N A L R E P O R T Performance Period July 12, 2006 - August 31, 2007 T A B L E O F C O N T E N T S 7 7 MESSAGE FROM THE DIRECTOR 8 NIAC STAFF 9 NIAC EXECUTIVE SUMMARY 10 THE LEGACY OF NIAC 14 ACCOMPLISHMENTS 14 Summary 14 Call for Proposals CP 05-02 (Phase II) 15 Call for Proposals CP 06-01 (Phase I) 17 Call for Proposals CP 06-02 (Phase II) 18 Call for Proposals CP 07-01 (Phase I) 18 Call for Proposals CP 07-02 (Phase II) 18 Financial Performance 18 NIAC Student Fellows Prize Call for Proposals 2006-2007 19 NIAC Student Fellows Prize Call for Proposals 2007-2008 20 Release and Publicity of Calls for Proposals 20 Peer Reviewer Recruitment 21 NIAC Eighth Annual Meeting 22 NIAC Fellows Meeting 24 NIAC Science Council Meetings 24 Coordination With NASA 27 Publicity, Inspiration and Outreach 29 Survey of Technologies to Enable NIAC Concepts 32 DESCRIPTION OF THE NIAC 32 NIAC Mission 33 Organization 34 Facilities 35 Virtual Institute 36 The NIAC Process 37 Grand Visions 37 Solicitation 38 NIAC Calls for Proposals 39 Peer Review 40 NASA Concurrence 40 Awards 40 Management of Awards 41 Infusion of Advanced Concepts 4 T A B L E O F C O N T E N T S 7 LIST OF TABLES 14 Table 1.
    [Show full text]
  • Engineering 8 Launch Vehicles
    Papers on the Lunar Settlement Engineering 8 : Launch Vehicles mass of each stage is 10% the fuel mass, 0. Introduction This paper since the larger lower stages will be accompanies number 03-01 on the more structurally efficient but must bear logistics of space access. It is intended the load of the upper stages. to present technical analysis of relevant concepts, specifically the expendable If the required velocity increment for multistage rocket for direct ascent, the direct ascent, without an intermediate single-stage reusable terrestrial orbiter, orbit, is taken as the sum of the escape two-stage reusable and partially reusable velocities of Terra and Luna, 13.6 km/s, configurations, the lunar rocket, and the the necessary mass ratio with exhaust space gun. At this early date, however, velocity 4.0 km/s is 30. This sets the nothing more than approximations and maximum delivered mass at 33 t, and general considerations can be furnished. indicates that several steps are required. While specific numerical values are As a little calculation will show, the indicated in certain places, it must be overall efficiency of a step rocket is understood clearly that few of these have improved by using low mass-ratios in any validity ; they are presented in order the lower steps. We may select a to indicate trends of expected behaviour. tristage configuration, with step mass ratios of 2, 3, and 5. 1. Expendable Rocket For the expendable rocket to be useful, it must The mass of the first step, then, is 550 t, be very large. Two factors are at work of which 500 t is fuel ; the second, 330 t, here : first, ceteris paribus , the larger with 300 t fuel ; and the third is the the rocket, the larger the useful mass lunar-landing stage, 120 t with 96 t fuel.
    [Show full text]
  • This Third Edition Bibliography Lists Books and Teaching Aids Related To
    60:CUMENT RESUMB ED 027 215 SE 006 287 Aerospace Bibliography, Third Edition. National Aeronautics and Space Administration, Washingtan, D.C. Repor t No- EP -35 Pub Date (651 Note-68p. EDRS Price f1F-$0.50 HC-$3.50 Descriptors-*Aerospace Technok)gy, *Annotated Bibliographies, Astronomy, *Bibliographies, Physical Sciences, *Science Education, Technology Identifiers-National Aeronautics and Space Administration Thisthirdeditionbibliographylistsbooks and teaching aids related to aeronautics and space. Aeronautics titles are limited toaerospace-related research subjects, and books on astronomy to those direCtly related to space exploration. Also listed are pertinent references like pamphlets, films,film strips, booklets, charts, pictures, periodicals, and sources of in.formation on specific space subjects available from aerospace industry companies. Reading levels for each document are indicated according to primary, intermediate, upper elementary, secondary, and adult or college. (GR) 33' $ t 'k 4 ;(' " ; , othisit-erP-ie I l if= WIN IP , ., k a k ' II U.S. DEPARTMENT OF HEALTH, EDUCATION & WELFARE OFFICE OF EDUCATION THIS DOCUMENT HAS BEEN REPRODUCED EXACTLY AS RECEIVED FROM THE PERSON OR ORGANIZATION ORIGINATING IT.POINTS OF VIEW OR OPINIONS STATED DO NOT NECESSARILY REPRESENT OFF!CIAL OFFICE OF EDUCATION POSITION OR POLICY. 0 ,"'". Al 1011011104- 1,," 1. 1,=z;z0z2i Ent AEROSPACE BIBLIOGRAPHY THIRD EDITION Compiled for Educational Programs Division, Office of Public Affairs NATIONAL AERONAUTICS AND SPACE ADMINISTRATION by National Aerospace
    [Show full text]
  • The Lunar Economy - Years 1-25 Dec 1986 - Nov 2011
    MMM Theme Issues: The Lunar Economy - Years 1-25 Dec 1986 - Nov 2011 The Moon Would Seem to be a Tough Nut to Crack Until we look Closer At first we may not be able to produce “first choice” alloys and other building and manufacturing materials, but what we can produce early on will be adequate to substitute for enough products that the gross tonnage of imports from Earth can be cut to a fraction. Power Generation is essential. Better, as we point out in Foundation 2 above, the Moon has the real estate advantage of “location, location, location.” As a result, anything produced on the Moon could be shipped to space facilities in Low Earth Orbit (LEO) and Geosynchronous Orbit (GEO) at a cost advantage of equivalent products manufactured on Earth. Thus the cost of importing to the Moon those things that cannot yet be manufactured there, could be ofset by exports of Lunar manufactured goods and materials to markets in LEO and GEO. Production of consumer goods will be important and enterprise will be a key factor. It will take time, but financial break-even is possible in time. The obstacles are great. But once you look closely at the options, these obstacles fall in the ranks of those that faced MMM Theme Issues: The Lunar Economy - Years 1-25 Dec 1986 - Nov 2011 pioneers of other frontiers on Earth in eras gone by. Establishing and then elaborating the roots and possibilities of a lunar economy sufcient to support permanent pioneer frontier settlements are there, and treating them one by one has been a major theme of Moon Miners’ Manifesto through the years.
    [Show full text]
  • FINAL PROGRAM Innovations in Propulsion and Energy Driving System Solutions
    2O16 25–27 JULY 2016 SALT LAKE CITY, UT Innovations in Propulsion and Energy Driving System Solutions FINAL PROGRAM www.aiaa-propulsionenergy.org #aiaaPropEnergy 16-1225 Real-Time Q&A and Polling during AIAA Propulsion NEW! and Energy 2016 withwith ConferenceConference IO!IO! During Plenary and Forum 360 Sessions, go to aiaa.cnf.io Getting Your Question Answered is as EASY as 1-2-3! 1. Click the “Ask” button to submit a question. 2. Check out the questions that other attendees are asking. 3. If you see a question that you want answered, click on the arrow on the left. The most popular questions automatically rise to the top. Participate in Session Polls 1. If Polls are available they will appear at the top of the page. Simply click/tap on a Poll to respond. 2. Choose your response(s) and hit “submit”. 3. After responding you will be able to see the results on your own device!* * Some Poll results may be hidden NO DOWNLOADING REQUIRED! Executive Steering Committee 2O16 AIAA Propulsion and Energy 2016 Welcome Welcome to Salt Lake City, Utah, and AIAA Propulsion and Energy 2016. We are excited to share the next few days with you as we explore the most pressing issues facing the future of propulsion and energy systems – the true heart of aerospace. With so many insightful and dynamic speakers and panelists, we are confident you will find the information presented here thought-provoking, impactful, and immediately useful to you in your work. Daniel “Dan” Michael Heil During the forum you will hear from thought leaders, learn about the latest technical Dumbacher Ohio Aerospace breakthroughs, and most importantly collaborate with other attendees from Purdue University Institute (Ret.) government, industry, and academia.
    [Show full text]
  • Call for Papers Abstract Deadline 7 December 2015
    JANNAF INTERAGENCY PROPULSION COMMITTEE JOINT ARMY-NAVY-NASA-AIR FORCE 63rd JANNAF Propulsion Meeting Programmatic and Industrial Base Meeting 47th Combustion (CS) 35th Airbreathing Propulsion (APS) 35th Exhaust Plume and Signatures (EPSS) 29th Propulsion Systems Hazards (PSHS) JOINT SUBCOMMITTEE MEETING 16 - 20 May 2016 Announcement and Call For Papers Abstract Deadline 7 December 2015 Newport News, Virginia last updated 1/27/16 The May 2016 meeting of the Joint Army-Navy-NASA-Air SCOPE Force (JANNAF) will consist of the 63rd JANNAF Propulsion meeting; the Programmatic and Industrial Base (PIB) JANNAF Propulsion Meeting meeting; and the Joint Meeting of the 47th Combustion / The JANNAF Propulsion Meeting (JPM) encompasses research 35th Airbreathing Propulsion / 35th Exhaust Plume and and applications at the systems level. The JPM is held each Signatures / 29th Propulsion Systems Hazards Subcommittees. year in conjunction with standing JANNAF subcommittee Dr. Christine M. Michienzie with OSD (AT&L), MIBP, meetings on a rotating basis. The scope of the 63rd JPM in Alexandria, Virginia, is the meeting chair. This meeting will 2016 spans eight mission areas: Tactical Propulsion; Missile be held Monday through Friday, 16 - 20 May 2016, at the Defense/Strategic Propulsion; Propulsion Systems for Space Newport News Marriott at City Center in Newport News, Access; Gun and Gun-Launched Propulsion; Propulsion and Virginia. Please refer to page 4 for hotel and area information. Energetics Test Facilities; Sensors for Propulsion Measurement Applications;
    [Show full text]
  • Motorised Momentum Exchange Space Tethers: the Dynamics of Asymmetrical Tethers, and Some Recent New Applications
    MATEC Web of Conferences 148, 01001 (2018) https://doi.org/10.1051/matecconf/201814801001 ICoEV 2017 Motorised momentum exchange space tethers: the dynamics of asymmetrical tethers, and some recent new applications Matthew Cartmell1,2,*, Olga Ganilova1,2, Eoin Lennon1, and Gavin Shuttleworth1 1Department of Mechanical & Aerospace Engineering, University of Strathclyde, Glasgow, G1 1XJ, Scotland, UK 2Strathclyde Space Institute, University of Strathclyde, Glasgow, G1 1XJ, Scotland, UK Abstract. This paper reports on a first attempt to model the dynamics of an asymmetrical motorised momentum exchange tether for spacecraft payload propulsion, and it also provides some interesting summary results for two novel applications for motorised momentum exchange tethers. The asymmetrical tether analysis is very important because it represents the problematic scenario when payload mass unbalance intrudes, due to unexpected payload loss or failure to retrieve. Mass symmetry is highly desirable both dynamically and logistically, but it is shown in this paper that there is still realistic potential for mission rescue should an asymmetry condition arise. Conceptual designs for tethered payload release from LEO and lunar tether delivery and retrieval are also presented as options for future development. 1 Introduction Momentum exchange tether dynamics have been extensively studied in recent years, and are of current considerable interest internationally as a technology for cost effective and environmentally clean propulsion of payload mass from Low Earth Orbit (LEO). A conceptual design for a motorised momentum exchange tether is given in Figure 1 where the central facility motor drive shaft attaches to the propulsion sub-spans by mean of a gantry, mounted so that it can be rotated by the shaft.
    [Show full text]
  • Design of Spacecraft Missions to Remove Multiple Orbital Debris Objects
    AAS 12-017 Design of Spacecraft Missions to Remove Multiple Orbital Debris Objects Brent W. Barbee*, Salvatore Alfano†, Elfego Piñon‡, Kenn Gold‡, and David Gaylor‡ *NASA-GSFC, †CSSI, ‡Emergent Space Technologies, Inc. 35th ANNUAL AAS GUIDANCE AND CONTROL CONFERENCE February 3 - February 8, 2012 Sponsored by Breckenridge, Colorado Rocky Mountain Section AAS Publications Office, P.O. Box 28130 - San Diego, California 92198 AAS 12-017 DESIGN OF SPACECRAFT MISSIONS TO REMOVE MULTIPLE ORBITAL DEBRIS OBJECTS Brent W. Barbee,∗ Salvatore Alfano,y Elfego Pinon˜ ,z Kenn Gold,x and David Gaylor{ The amount of hazardous debris in Earth orbit has been increasing, posing an ever- greater danger to space assets and human missions. In January of 2007, a Chinese ASAT test produced approximately 2600 pieces of orbital debris. In February of 2009, Iridium 33 collided with an inactive Russian satellite, yielding approx- imately 1300 pieces of debris. These recent disastrous events and the sheer size of the Earth orbiting population make clear the necessity of removing orbital de- bris. In fact, experts from both NASA and ESA have stated that 10 to 20 pieces of orbital debris need to be removed per year to stabilize the orbital debris environ- ment. However, no spacecraft trajectories have yet been designed for removing multiple debris objects and the size of the debris population makes the design of such trajectories a daunting task. Designing an efficient spacecraft trajectory to rendezvous with each of a large number of orbital debris pieces is akin to the fa- mous Traveling Salesman problem, an NP-complete combinatorial optimization problem in which a number of cities are to be visited in turn.
    [Show full text]
  • Pushing Boundaries Through Innovative Design and Technology
    10–12 JULY 2017 ATLANTA, GA Pushing Boundaries Through Innovative Design and Technology propulsionenergy.aiaa.org #aiaaPropEnergy 17-1835 The engine of change will come from the company that can build it. GE is bringing together best-in-class analytics and deep domain expertise to help our customers solve their toughest challenges. See how we’re changing the way we y at geaviation.com. 85064_GEAV_DI_Print Ad_P+E.indd 1 7/5/16 3:55 PM Contents Organizing Committee 4 Welcome 5 Sponsors 6 Forum Schedule 7 On-Site Wi Fi Information Pre-Forum Activities 9 Network Name: AIAA Password: PE2017 Plenary Sessions 10 Forum 360 Sessions 11 Conferences i/o: aiaa1.cnf.io Complex Aerospace Systems Exchange 13 www.twitter.com/aiaa Aircraft Electric Propulsion & Power Focus Area 14 www.facebook.com/AIAAfan ITAR Restricted Sessions 16 www.youtube.com/AIAATV Technical Sessions at a Glance 17 www.linkedin.com/companies/aiaa Program Detail 22 www.flickr.com/aiaaevents Rising Leaders in Aerospace 59 www.instagram.com/aiaaerospace Recognition and Lectures 60 livestream.com/AIAAvideo/PropEnergy2017 Networking Events 62 Exposition 63 Photography or the video or audio recording Exhibitors 65 of sessions or exhibits, as well as the unauthorized sale of AIAA-copyrighted General Information 70 material, is prohibited. Author and Session Chair Information 72 Committee Meetings 73 www.aiaa.org Author and Session Chair Index 74 propulsionenergy.aiaa.org Venue Map Back Cover propulsionenergy.aiaa.org 3 #aiaaPropEnergy IntroOrganizing Committee Organizing Committee Energy Storage Technologies Solid Rockets Joe Troutman, ABSL Space Products Barbara Leary, Johns Hopkins University Forum General Chair Applied Physics Laboratory Mike J.
    [Show full text]
  • An Overview of Advanced Concepts for Launch 5B
    Form Approved REPORT DOCUMENTATION PAGE OMB No. 0704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and reviewing this collection of information. Send comments regarding this burden estimate or any other aspect of this collection of information, including suggestions for reducing this burden to Department of Defense, Washington Headquarters Services, Directorate for Information Operations and Reports (0704-0188), 1215 Jefferson Davis Highway, Suite 1204, Arlington, VA 22202-4302. Respondents should be aware that notwithstanding any other provision of law, no person shall be subject to any penalty for failing to comply with a collection of information if it does not display a currently valid OMB control number. PLEASE DO NOT RETURN YOUR FORM TO THE ABOVE ADDRESS. 1. REPORT DATE (DD-MM-YYYY) 2. REPORT TYPE 3. DATES COVERED (From - To) 09-02-2012 Briefing Charts 4. TITLE AND SUBTITLE 5a. CONTRACT NUMBER An Overview of Advanced Concepts for Launch 5b. GRANT NUMBER 5c. PROGRAM ELEMENT NUMBER 6. AUTHOR(S) 5d. PROJECT NUMBER Marcus Young and Jason Mossman 5f. WORK UNIT NUMBER 50260542 7. PERFORMING ORGANIZATION NAME(S) AND ADDRESS(ES) 8. PERFORMING ORGANIZATION REPORT NUMBER Air Force Research Laboratory (AFMC) AFRL/RZSA 10 E. Saturn Blvd. Edwards AFB CA 93524-7680 9. SPONSORING / MONITORING AGENCY NAME(S) AND ADDRESS(ES) 10. SPONSOR/MONITOR’S ACRONYM(S) Air Force Research Laboratory (AFMC) AFRL/RZS 11. SPONSOR/MONITOR’S 5 Pollux Drive NUMBER(S) Edwards AFB CA 93524-7048 AFRL-RZ-ED-VG-2012-030 12.
    [Show full text]