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This Boeing Team's Skills at Producing Delta IV Rocket Fairings Helped
t’s usually the tail end of the rocket that gets all the early atten- other work. But they’d jump at the chance to work together again. tion, providing an impressive fiery display as the spacecraft is Their story is one of challenges and solutions. And they attribute hurled into orbit. But mission success also depends on what’s their success to Lean+ practices and good old-fashioned teamwork. Ion top of the rocket: a piece of metal called the payload fairing “The team took it upon themselves to make an excellent that protects the rocket’s cargo during the sometimes brutal ride product,” said program manager Thomas Fung. “We had parts to orbital speed. issues and tool problems, but the guys really stepped up and took “There’s no room for error,” said Tracy Allen, Boeing’s manu- pride and worked through the issues.” facturing production manager for a Huntington Beach, Calif., team The aluminum fairing team went through a major transition that made fairings for the Delta IV. The fairing not only protects the when Boeing merged its Delta Program with Lockheed Martin’s payload from launch to orbit but also must jettison properly for Atlas Program to form United Launch Alliance in 2006. deployment of the satellite or spacecraft. “There were a lot of process changes in the transition phase Allen and his colleagues built the 65-foot-long (20-meter-long) because we were working with a new company,” Fung said. “We aluminum isogrid fairings for the Delta IV heavy-lift launch vehicle. had part shortages because of vendor issues, and that caused The design was based on 41 similar fairings Boeing made for the an impact to the schedule. -
Douglas Missile & Space Systems Division
·, THE THOR HISTORY. MAY 1963 DOUGLAS REPORT SM-41860 APPROVED BY: W.H.. HOOPER CHIEF, THOR SYSTEMS ENGINEERING AEROSPACE SYSTEMS ENGINEERING DOUGLAS MISSILE & SPACE SYSTEMS DIVISION ABSTRACT This history is intended as a quick orientation source and as n ready-reference for review of the Thor and its sys tems. The report briefly states the development of Thor, sur'lli-:arizes and chronicles Thor missile and booster launch inGs, provides illustrations and descriptions of the vehicle systcn1s, relates their genealogy, explains sane of the per fon:iance capabilities of the Thor and Thor-based vehicles used, and focuses attention to the exploration of space by Douelas Aircraf't Company, Inc. (DAC). iii PREFACE The purpose of The Thor History is to survey the launch record of the Thor Weapon, Special Weapon, and Space Systems; give a systematic account of the major events; and review Thor's participation in the military and space programs of this nation. The period covered is from December 27, 1955, the date of the first contract award, through May, 1963. V �LE OF CONTENTS Page Contract'Award . • • • • • • • • • • • • • • • • • • • • • • • • • 1 Background • • • • • • • • • • • • • • • • • • • • • • • • • • • • l Basic Or�anization and Objectives • • • • • • • • • • • • • • • • 1 Basic Developmenta� Philosophy . • • • • • • • • • • • • • • • • • 2 Early Research and Development Launches • • • ·• • • • • • • • • • 4 Transition to ICBM with Space Capabilities--Multi-Stage Vehicles . 6 Initial Lunar and Space Probes ••••••• • • • • • • • -
Space) Barriers for 50 Years: the Past, Present, and Future of the Dod Space Test Program
SSC17-X-02 Breaking (Space) Barriers for 50 Years: The Past, Present, and Future of the DoD Space Test Program Barbara Manganis Braun, Sam Myers Sims, James McLeroy The Aerospace Corporation 2155 Louisiana Blvd NE, Suite 5000, Albuquerque, NM 87110-5425; 505-846-8413 [email protected] Colonel Ben Brining USAF SMC/ADS 3548 Aberdeen Ave SE, Kirtland AFB NM 87117-5776; 505-846-8812 [email protected] ABSTRACT 2017 marks the 50th anniversary of the Department of Defense Space Test Program’s (STP) first launch. STP’s predecessor, the Space Experiments Support Program (SESP), launched its first mission in June of 1967; it used a Thor Burner II to launch an Army and a Navy satellite carrying geodesy and aurora experiments. The SESP was renamed to the Space Test Program in July 1971, and has flown over 568 experiments on over 251 missions to date. Today the STP is managed under the Air Force’s Space and Missile Systems Center (SMC) Advanced Systems and Development Directorate (SMC/AD), and continues to provide access to space for DoD-sponsored research and development missions. It relies heavily on small satellites, small launch vehicles, and innovative approaches to space access to perform its mission. INTRODUCTION Today STP continues to provide access to space for DoD-sponsored research and development missions, Since space first became a viable theater of operations relying heavily on small satellites, small launch for the Department of Defense (DoD), space technologies have developed at a rapid rate. Yet while vehicles, and innovative approaches to space access. -
L AUNCH SYSTEMS Databk7 Collected.Book Page 18 Monday, September 14, 2009 2:53 PM Databk7 Collected.Book Page 19 Monday, September 14, 2009 2:53 PM
databk7_collected.book Page 17 Monday, September 14, 2009 2:53 PM CHAPTER TWO L AUNCH SYSTEMS databk7_collected.book Page 18 Monday, September 14, 2009 2:53 PM databk7_collected.book Page 19 Monday, September 14, 2009 2:53 PM CHAPTER TWO L AUNCH SYSTEMS Introduction Launch systems provide access to space, necessary for the majority of NASA’s activities. During the decade from 1989–1998, NASA used two types of launch systems, one consisting of several families of expendable launch vehicles (ELV) and the second consisting of the world’s only partially reusable launch system—the Space Shuttle. A significant challenge NASA faced during the decade was the development of technologies needed to design and implement a new reusable launch system that would prove less expensive than the Shuttle. Although some attempts seemed promising, none succeeded. This chapter addresses most subjects relating to access to space and space transportation. It discusses and describes ELVs, the Space Shuttle in its launch vehicle function, and NASA’s attempts to develop new launch systems. Tables relating to each launch vehicle’s characteristics are included. The other functions of the Space Shuttle—as a scientific laboratory, staging area for repair missions, and a prime element of the Space Station program—are discussed in the next chapter, Human Spaceflight. This chapter also provides a brief review of launch systems in the past decade, an overview of policy relating to launch systems, a summary of the management of NASA’s launch systems programs, and tables of funding data. The Last Decade Reviewed (1979–1988) From 1979 through 1988, NASA used families of ELVs that had seen service during the previous decade. -
Implementation of a Femto-Satellite and a Mini-Launcher
Implementation of a femto-satellite and a mini-launcher Joshua Tristancho SUPERVISED BY Jordi Guti errez´ Universitat Polit ecnica` de Catalunya Master in Aerospace Science & Technology May 2010 Implementation of a femto-satellite and a mini-launcher BY Joshua Tristancho DIPLOMA THESIS FOR DEGREE Master in Aerospace Science and Technology AT Universitat Polit ecnica` de Catalunya SUPERVISED BY: Jordi Guti errez´ Applied Physics department A Sonia Quiero agradecer a Dios, a mi familia y a mi iglesia de Salou por el apoyo recibido durante estos a nos˜ de trabajo en el proyecto PicoRover y WikiSat. Sin ellos hubiera sido imposible llegar hasta aqu ´ı. Agradecer tambi en´ el incondicional apoyo de los profesores de la UPC: Cristina Barrado Mux ´ı Dagoberto Jos e´ Salazar Hern andez´ Daniel Crespo Artiaga Enric Pastor Llorens Enrique Carg ´ıa-Berro Montilla Francisco Javier Mora Serrano F. Xavier Estop a` Mulet Jordi Guti errez´ Cabello Jos e´ Luis Andr es´ Yebra Juan L opez´ Rubio M. Ang elica´ Reyes Mu noz˜ Marcos Qu ´ılez Figuerola Miguel Valero Garc ´ıa Oscar Casas Piedrafita Pablo Royo Chic Pilar Gil Pons Ricard Gonz alez´ Cinca Santiago Torres Gil Xavier Prats Men endez´ Yuri Koubychine . Carles, mai t’oblidarem. ABSTRACT In this Master Thesis we begin with a short analysis of the current space market, with the aim of searching solutions that allow us to implement femto-satellites (that is, satellites with a mass less than 100 grams) and mini-launchers (in this case less than 100 kilograms). New synergies will be explored in order to reduce drastically the cost of development, construction, operation and disposal of femto-satellites and mini-launchers for operations in LEO (Low Earth Orbits below 300 kilometers of altitude) and short duration, about one week. -
DELTA4000/5000/4D/5D Version / Release 2.1 Manuel Opérateur Multilingue Multilingual Operator’S Manual Ref
6159938010-07 DELTA4000/5000/4D/5D Version / Release 2.1 Manuel opérateur multilingue Multilingual operator’s manual Ref. / N° : 6159938010-07 English ...................................3 Français................................27 Español ................................51 Deutsch ................................75 Italiano................................101 Português...........................127 Nederlands.........................151 Svenska..............................177 Georges Renault S.A.S - 199 route de Clisson - B.P.13627 44236 Saint Sébastien-sur-Loire Cedex France 6159938010-07 6159938010-07 English 3 / 200 DELTA4000/5000/4D/5D Release 2.1 Operator's Manual No. 6159938010-07 © Copyright 2005, GEORGES RENAULT S.A.S, 44230 France All rights reserved. Any unauthorized use or copying of the contents or part thereof is prohibited. This applies in particular to © trademarks, model denominations, part numbers and drawings. Use only authorized parts. Any damage or malfunction caused by the use of unauthorised parts is not covered by Warranty or Product Liability. Georges Renault S.A.S - 199 route de Clisson - B.P.13627 44236 Saint Sébastien-sur-Loire Cedex France 6159938010-07 TABLE OF CONTENTS English 4 / 200 TABLE OF CONTENTS 1 - INTRODUCTION ................................................................................................................................... 5 2 - DESCRIPTION OF THE UNIT .............................................................................................................. 5 2.1 - Front side -
John F. Kennedy Space Center
1 . :- /G .. .. '-1 ,.. 1- & 5 .\"T!-! LJ~,.", - -,-,c JOHN F. KENNEDY ', , .,,. ,- r-/ ;7 7,-,- ;\-, - [J'.?:? ,t:!, ;+$, , , , 1-1-,> .irI,,,,r I ! - ? /;i?(. ,7! ; ., -, -?-I ,:-. ... 8 -, , .. '',:I> !r,5, SPACE CENTER , , .>. r-, - -- Tp:c:,r, ,!- ' :u kc - - &te -- - 12rr!2L,D //I, ,Jp - - -- - - _ Lb:, N(, A St~mmaryof MAJOR NASA LAUNCHINGS Eastern Test Range Western Test Range (ETR) (WTR) October 1, 1958 - Septeniber 30, 1968 Historical and Library Services Branch John F. Kennedy Space Center "ational Aeronautics and Space Administration l<ennecly Space Center, Florida October 1968 GP 381 September 30, 1968 (Rev. January 27, 1969) SATCIEN S.I!STC)RY DCCCIivlENT University uf A!;b:,rno Rr=-?rrh Zn~tituta Histcry of Sciecce & Technc;oGy Group ERR4TA SHEET GP 381, "A Strmmary of Major MSA Zaunchings, Eastern Test Range and Western Test Range,'" dated September 30, 1968, was considered to be accurate ag of the date of publication. Hmever, additianal research has brought to light new informetion on the official mission designations for Project Apollo. Therefore, in the interest of accuracy it was believed necessary ta issue revfsed pages, rather than wait until the next complete revision of the publiatlion to correct the errors. Holders of copies of thia brochure ate requested to remove and destroy the existing pages 81, 82, 83, and 84, and insert the attached revised pages 81, 82, 83, 84, 8U, and 84B in theh place. William A. Lackyer, 3r. PROJECT MOLL0 (FLIGHTS AND TESTS) (continued) Launch NASA Name -Date Vehicle -Code Sitelpad Remarks/Results ORBITAL (lnaMANNED) 5 Jul 66 Uprated SA-203 ETR Unmanned flight to test launch vehicle Saturn 1 3 7B second (S-IVB) stage and instrment (IU) , which reflected Saturn V con- figuration. -
The Delta Launch Vehicle- Past, Present, and Future
The Space Congress® Proceedings 1981 (18th) The Year of the Shuttle Apr 1st, 8:00 AM The Delta Launch Vehicle- Past, Present, and Future J. K. Ganoung Manager Spacecraft Integration, McDonnell Douglas Astronautics Co. H. Eaton Delta Launch Program, McDonnell Douglas Astronautics Co. Follow this and additional works at: https://commons.erau.edu/space-congress-proceedings Scholarly Commons Citation Ganoung, J. K. and Eaton, H., "The Delta Launch Vehicle- Past, Present, and Future" (1981). The Space Congress® Proceedings. 7. https://commons.erau.edu/space-congress-proceedings/proceedings-1981-18th/session-6/7 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]. THE DELTA LAUNCH VEHICLE - PAST, PRESENT AND FUTURE J. K. Ganoung, Manager H. Eaton, Jr., Director Spacecraft Integration Delta Launch Program McDonnell Douglas Astronautics Co. McDonnell Douglas Astronautics Co. INTRODUCTION an "interim space launch vehicle." The THOR was to be modified for use as the first stage, the The Delta launch vehicle is a medium class Vanguard second stage propulsion system, was used expendable booster managed by the NASA Goddard as the Delta second stage and the Vanguard solid Space Flight Center and used by the U.S. rocket motor became Delta's third stage. Government, private industry and foreign coun Following the eighteen month development program tries to launch scientific, meteorological, and failure to launch its first payload into or applications and communications satellites. -
King County Fuel Cell Demonstration Project
Final Report KING COUNTY FUEL CELL DEMONSTRATION PROJECT Prepared for Department of U.S. Environmental Protection Agency Natural Resources and Parks Wastewater Treatment Division April 2009 Prepared by Department of Natural Resources and Parks Wastewater Treatment Division King County Fuel Cell Demonstration Project Prepared for U.S. Environmental Protection Agency April 2009 Prepared by For comments or questions, contact: Bob Bucher King County Wastewater Treatment Division 1400 Utah St. West M.S. WTP-NR-0100 Seattle, WA 98199 [email protected] This information is available in alternative formats on request at 206-684-1280 (voice) or 711 (TTY) King County Fuel Cell Demonstration Project ii Table of Contents Executive Summary...................................................................................................................vii SECTION 1 Introduction..................................................................................................... 1-1 Background........................................................................................................................................... 1-1 Project Timeline.................................................................................................................................... 1-3 Project Teams........................................................................................................................................ 1-3 Report Organization ........................................................................................................................... -
Delta II Dawn Mission Booklet
Delta Launch Vehicle Programs Dawn United Launch Alliance is proud to launch the Dawn mission. Dawn will be launched aboard a Delta II 7925H launch vehicle from Cape Canaveral Air Force Station (CCAFS), Florida. The launch vehicle will deliver the Dawn spacecraft into an Earth- escape trajectory, where it will commence its journey to the solar system’s main asteroid belt to gather comparative data from dwarf planet Ceres and asteroid Vesta. United Launch Alliance provides the Delta II launch service under the NASA Launch Services (NLS) contract with the NASA Kennedy Space Center Expendable Launch Services Program. We are delighted that NASA has chosen the Delta II for this Discovery Mission. I congratulate the entire Delta team for their significant efforts that resulted in achieving this milestone and look forward to continued launches of scientific space missions aboard the Delta launch vehicle. Kristen T. Walsh Director, NASA Programs Delta Launch Vehicles 1 Dawn Mission Overview The Dawn spacecraft will make an eight-year journey to the main asteroid belt between Mars and Jupiter in an effort to significantly increase our understanding of the conditions and processes acting at the solar system’s earliest epoch by examining the geophysical properties of the asteroid Vesta and dwarf planet Ceres. Evidence shows that Vesta and Ceres have distinct characteristics and, therefore, must have followed different evolutionary paths. By observing both, with the same set of instruments, scientists hope to develop an understanding of the transition from the rocky inner regions, of which Vesta is characteristic, to the icy outer regions, of which Ceres is representative. -
January 1972
1- -/- r-FI - M . , 2 1. I ./ r..1 1 ..1 .91"r«Fr 11 'L ' 4 *L :,1 1 1 15'i'&11& ..-t *4-**4,- '+ , 1 ,#146*1\ :1,#F'i- ihlf,1,r. 'flijh/f»--,1~.Ati ·, 4 <A/ 1,11 -. , . NNU -A . * IA- 1 IIi,_ %4'1 r'll,I, , . ...... ........ ..~..1.... - 9, , .t 1, 14., '.,r'. - 4-- . 3 8 . il- . 191 01, t . Ad v - » r'* _ , , I I r V '- 4 \ '111 11 4 1, 14, , 4 7S* . GOLD CARD PRESENTATIONS signifying Honorary Membership in Ope- 4/36, Reg, 231681; C. J. Mahan, Init. 7/27, Reg. 179387: Don E. Malhiot, rating Engineers Local Union No. 3 were made by Business Manager Al Init. 12/32, Reg. 202738; Meryl D. Mayes, Init. 12/36, Reg. 238116; John Clen- a- the Semi-Annual Meeting to Brothers E. J. Blood, Int. 7/17, Reg. F. Regallo, Init. 5/36, Reg. 232718; C. A. Schroff, Init. 4/30, Reg. 195110: 87915· C. C. Clark, Init. 3/30, Reg. 194797; Earl Dooley, Init. 9/35, Reg. Hobart Simpson, Init. 9/32, Reg. 202429; C. W. Stevens, Init. 9/28, Reg. 227545 George Ernst, Init. 4/36, Reg. 230898; Barney Felix, Init. 4/36, 187508: George W. Stevens, Init, 2/31, Reg, 198375 and Earl Stiles, Init. Reg. 23 1675; Ralph L, Foy, Init. 5/36, Reg. 23652; Robert Hall, Init. 9/35, 12/36, Reg. 239392. A standing ovation followed the presentations. Reg. 226889; F, M. Lauritzen, 9/35, Reg. 227,552; Philip Perrin, Init. "Serving the men who move tbe earth.'" ~~ ENGINEERS Cr »~ iNH :W 48 <tlESN>- PUBLISHED TO PROMOTE THE GENERAL WELFARE OF ALL ENGINEERS AND THEIR FAMILIES 1. -
Central Florida Future, Vol. 12 No. 14, November 30, 1979
University of Central Florida STARS Central Florida Future University Archives 11-30-1979 Central Florida Future, Vol. 12 No. 14, November 30, 1979 Part of the Mass Communication Commons, Organizational Communication Commons, Publishing Commons, and the Social Influence and oliticalP Communication Commons Find similar works at: https://stars.library.ucf.edu/centralfloridafuture University of Central Florida Libraries http://library.ucf.edu This Newsletter is brought to you for free and open access by the University Archives at STARS. It has been accepted for inclusion in Central Florida Future by an authorized administrator of STARS. For more information, please contact [email protected]. Recommended Citation "Central Florida Future, Vol. 12 No. 14, November 30, 1979" (1979). Central Florida Future. 380. https://stars.library.ucf.edu/centralfloridafuture/380 .U C F LIBRARY ARCHIVES University of .·central Florida) Fr~day, November 30, 1979 N~. l_ ~ . -; ~ _ ill __ Energy. costs exceed university's budget by Barbara °Cowell aaaoclate editor UCF's energy consumption has rise.n and is no longer within the budget .project for : this yea_r, according to Richard V. Neuhaus, assistant director of thP Physical Plant. The proposed budget for the year underestimated the rising cost of energy. Ac·· cording to Neuhaus, the cost per energy unit has riseq over 35 percent and show5 no sign of abating. "At this time," he said, "the cost of the kilowatt hour has risen from three to five cents." "They tell me that at other universities they're having problems. '.with . budgets," said N~uhaus. "Especially campuses like USF and UF, where medical centers are situated and consume a great amount of energy." According to Neuhaus, UCF has implemented a Delta 1000 and 2000 Horeywell system for energy management.