Douglas Missile & Space Systems Division
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1957 – the Year the Space Age Began Conditions in 1957
1957 – The Year the Space Age Began Roger L. Easton, retired Naval Research Laboratory Linda Hall Library Kansas City MO 6 September 2007 Conditions in 1957 z Much different from now, slower, more optimistic in some ways z Simpler, yet very frightening, time 1 1957 in Politics z January 20: Second Presidential Inauguration of Dwight Eisenhower 1957 in Toys z First “Frisbee” from Wham-O 2 1957 in Sports z Third Year of Major League Baseball in Kansas City z the “Athletics,” not the “Royals” 1957 in Sports z No pro football in Kansas City z AFL was three years in future z no Chiefs until 1963 3 1957 at Home z No microwave ovens z (TV dinners since 1954) z Few color television sets z (first broadcasts late in 1953) z No postal Zip Codes z Circular phone diales z No cell phones z (heck, no Area Codes, no direct long-distance dialing!) z No Internet, no personal computers z Music recorded on vinyl discs, not compact or computer disks 1957 in Transportation z Gas cost 27¢ per gallon z September 4: Introduction of the Edsel by Ford Motor Company z cancelled in 1959 after loss of $250M 4 1957 in Transportation z October 28: rollout of first production Boeing 707 1957 in Science z International Geophysical Year (IGY) z (actually, “year and a half”) 5 IGY Accomplishments z South Polar Stations established z Operation Deep Freeze z Discovery of mid-ocean submarine ridges z evidence of plate tectonics z USSR and USA pledged to launch artificial satellites (“man-made moons”) z discovery of Van Allen radiation belts 1957: “First” Year of Space Age z Space Age arguably began in 1955 z President Eisenhower announced that USA would launch small unmanned earth-orbiting satellite as part of IGY z Project Vanguard 6 Our Story: z The battle to determine who would launch the first artificial satellite: z Werner von Braun of the U.S. -
Information Summaries
TIROS 8 12/21/63 Delta-22 TIROS-H (A-53) 17B S National Aeronautics and TIROS 9 1/22/65 Delta-28 TIROS-I (A-54) 17A S Space Administration TIROS Operational 2TIROS 10 7/1/65 Delta-32 OT-1 17B S John F. Kennedy Space Center 2ESSA 1 2/3/66 Delta-36 OT-3 (TOS) 17A S Information Summaries 2 2 ESSA 2 2/28/66 Delta-37 OT-2 (TOS) 17B S 2ESSA 3 10/2/66 2Delta-41 TOS-A 1SLC-2E S PMS 031 (KSC) OSO (Orbiting Solar Observatories) Lunar and Planetary 2ESSA 4 1/26/67 2Delta-45 TOS-B 1SLC-2E S June 1999 OSO 1 3/7/62 Delta-8 OSO-A (S-16) 17A S 2ESSA 5 4/20/67 2Delta-48 TOS-C 1SLC-2E S OSO 2 2/3/65 Delta-29 OSO-B2 (S-17) 17B S Mission Launch Launch Payload Launch 2ESSA 6 11/10/67 2Delta-54 TOS-D 1SLC-2E S OSO 8/25/65 Delta-33 OSO-C 17B U Name Date Vehicle Code Pad Results 2ESSA 7 8/16/68 2Delta-58 TOS-E 1SLC-2E S OSO 3 3/8/67 Delta-46 OSO-E1 17A S 2ESSA 8 12/15/68 2Delta-62 TOS-F 1SLC-2E S OSO 4 10/18/67 Delta-53 OSO-D 17B S PIONEER (Lunar) 2ESSA 9 2/26/69 2Delta-67 TOS-G 17B S OSO 5 1/22/69 Delta-64 OSO-F 17B S Pioneer 1 10/11/58 Thor-Able-1 –– 17A U Major NASA 2 1 OSO 6/PAC 8/9/69 Delta-72 OSO-G/PAC 17A S Pioneer 2 11/8/58 Thor-Able-2 –– 17A U IMPROVED TIROS OPERATIONAL 2 1 OSO 7/TETR 3 9/29/71 Delta-85 OSO-H/TETR-D 17A S Pioneer 3 12/6/58 Juno II AM-11 –– 5 U 3ITOS 1/OSCAR 5 1/23/70 2Delta-76 1TIROS-M/OSCAR 1SLC-2W S 2 OSO 8 6/21/75 Delta-112 OSO-1 17B S Pioneer 4 3/3/59 Juno II AM-14 –– 5 S 3NOAA 1 12/11/70 2Delta-81 ITOS-A 1SLC-2W S Launches Pioneer 11/26/59 Atlas-Able-1 –– 14 U 3ITOS 10/21/71 2Delta-86 ITOS-B 1SLC-2E U OGO (Orbiting Geophysical -
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. -
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. -
Photo Release -- Space Systems/Loral-Built Telstar 11N Satellite on Track with Post Launch Maneuvers
Photo Release -- Space Systems/Loral-Built Telstar 11N Satellite On Track With Post Launch Maneuvers Solar Arrays Deployed On Schedule Following Successful Launch PALO ALTO, Calif., Feb 27, 2009 (GlobeNewswire via COMTEX News Network) -- Space Systems/Loral (SS/L), a subsidiary of Loral Space & Communications (Nasdaq:LORL) and the leading provider of commercial satellites, today announced that the Telstar 11N satellite built for Telesat, one of the world's leading fixed satellite services operators, is performing post launch maneuvers according to plan. The satellite's solar arrays deployed on schedule several hours after separation, following yesterday's successful launch aboard a Zenit-3SLB rocket from the Baikonur Space Center in Kazakhstan. Tomorrow the satellite will begin firing its thrusters to maneuver into its final geosynchronous orbit. A photo accompanying this release is available at http://www.globenewswire.com/newsroom/prs/?pkgid=5941 "We are proud to know that this high-power satellite will help make information and entertainment more accessible around the world," said John Celli, President and Chief Operating Officer of Space Systems/Loral. "Telstar 11N demonstrates the flexibility of our standard 1300 satellite platform, which in this case was engineered to accommodate a smaller launch vehicle. It is this flexibility together with long term proven reliability that have helped SS/L achieve more than 40 percent market share over the past five years." When it reaches its final geosynchronous orbit, Telstar 11N will support video and data applications in North America, Western Europe, and Africa. Space Systems/Loral designed the satellite with a unique Atlantic Ocean beam, which will help Telesat meet growing demand for mobile broadband from both commercial and government customers in shipping and aviation. -
ESPA Ring Datasheet
PAYLOAD ADAPTERS | ESPA ESPA THE EVOLVED SECONDARY PAYLOAD ADAPTER ESPA mounts to the standard NSSL (formerly EELV) interface bolt pattern (Atlas V, Falcon 9, Delta IV, OmegA, Vulcan, Courtesy of Lockheed Martin New Glenn) and is a drop-in component in the launch stack. Small payloads mount to ESPA ports featuring either a Ø15-inch bolt circle with 24 fasteners or a 4-point mount with pads at each corner of a 15-inch square; both of these interfaces have become small satellite standards. ESPA is qualified to carry 567 lbs (257 kg), and a Heavy interface Courtesy of NASA (with Ø5/16” fastener hardware) has been introduced with a capacity of 991 lbs (450 kg). All small satellite mass capabilities require the center of gravity (CG) to be within 20 inches (50.8 cm) of the ESPA port surface. Alternative configurations can be accommodated. ESPA GRANDE ESPA Grande is a more capable version of ESPA with Ø24-inch ports; the ring height is typically 42 inches. The Ø24-inch port has been qualified by test to Courtesy of ORBCOMM & Sierra Nevada Corp. carry small satellites up to 1543 lb (700 kg). ESPA ESPA IS ADAPTABLE TO UNIQUE MISSION REQUIREMENTS • The Air Force’s STP-1 mission delivered multiple small satellites on an Atlas V. • NASA’s Lunar Crater Observation and Sensing Satellite (LCROSS): ESPA was the spacecraft hub for the LCROSS shepherding satellite in 2009. • ORBCOMM Generation 2 (OG2) launched stacks of two and three ESPA Grandes on two different Falcon 9 missions and in total deployed 17 satellites. -
Orbital Fueling Architectures Leveraging Commercial Launch Vehicles for More Affordable Human Exploration
ORBITAL FUELING ARCHITECTURES LEVERAGING COMMERCIAL LAUNCH VEHICLES FOR MORE AFFORDABLE HUMAN EXPLORATION by DANIEL J TIFFIN Submitted in partial fulfillment of the requirements for the degree of: Master of Science Department of Mechanical and Aerospace Engineering CASE WESTERN RESERVE UNIVERSITY January, 2020 CASE WESTERN RESERVE UNIVERSITY SCHOOL OF GRADUATE STUDIES We hereby approve the thesis of DANIEL JOSEPH TIFFIN Candidate for the degree of Master of Science*. Committee Chair Paul Barnhart, PhD Committee Member Sunniva Collins, PhD Committee Member Yasuhiro Kamotani, PhD Date of Defense 21 November, 2019 *We also certify that written approval has been obtained for any proprietary material contained therein. 2 Table of Contents List of Tables................................................................................................................... 5 List of Figures ................................................................................................................. 6 List of Abbreviations ....................................................................................................... 8 1. Introduction and Background.................................................................................. 14 1.1 Human Exploration Campaigns ....................................................................... 21 1.1.1. Previous Mars Architectures ..................................................................... 21 1.1.2. Latest Mars Architecture ......................................................................... -
Spectrum and the Technological Transformation of the Satellite Industry Prepared by Strand Consulting on Behalf of the Satellite Industry Association1
Spectrum & the Technological Transformation of the Satellite Industry Spectrum and the Technological Transformation of the Satellite Industry Prepared by Strand Consulting on behalf of the Satellite Industry Association1 1 AT&T, a member of SIA, does not necessarily endorse all conclusions of this study. Page 1 of 75 Spectrum & the Technological Transformation of the Satellite Industry 1. Table of Contents 1. Table of Contents ................................................................................................ 1 2. Executive Summary ............................................................................................. 4 2.1. What the satellite industry does for the U.S. today ............................................... 4 2.2. What the satellite industry offers going forward ................................................... 4 2.3. Innovation in the satellite industry ........................................................................ 5 3. Introduction ......................................................................................................... 7 3.1. Overview .................................................................................................................. 7 3.2. Spectrum Basics ...................................................................................................... 8 3.3. Satellite Industry Segments .................................................................................... 9 3.3.1. Satellite Communications .............................................................................. -
The Advanced Cryogenic Evolved Stage (ACES)- a Low-Cost, Low-Risk Approach to Space Exploration Launch
The Advanced Cryogenic Evolved Stage (ACES)- A Low-Cost, Low-Risk Approach to Space Exploration Launch J. F. LeBar1 and E. C. Cady2 Boeing Phantom Works, Huntington Beach CA 92647 Space exploration top-level objectives have been defined with the United States first returning to the moon as a precursor to missions to Mars and beyond. System architecture studies are being conducted to develop the overall approach and define requirements for the various system elements, both Earth-to-orbit and in-space. One way of minimizing cost and risk is through the use of proven systems and/or multiple-use elements. Use of a Delta IV second stage derivative as a long duration in-space transportation stage offers cost, reliability, and performance advantages over earth-storable propellants and/or all new stages. The Delta IV second stage mission currently is measured in hours, and the various vehicle and propellant systems have been designed for these durations. In order for the ACES to have sufficient life to be useful as an Earth Departure Stage (EDS), many systems must be modified for long duration missions. One of the highest risk subsystems is the propellant storage Thermal Control System (TCS). The ACES effort concentrated on a lower risk passive TCS, the RL10 engine, and the other subsystems. An active TCS incorporating a cryocoolers was also studied. In addition, a number of computational models were developed to aid in the subsystem studies. The high performance TCS developed under ACES was simulated within the Delta IV thermal model and long-duration mission stage performance assessed. -
Orbital Debris: a Chronology
NASA/TP-1999-208856 January 1999 Orbital Debris: A Chronology David S. F. Portree Houston, Texas Joseph P. Loftus, Jr Lwldon B. Johnson Space Center Houston, Texas David S. F. Portree is a freelance writer working in Houston_ Texas Contents List of Figures ................................................................................................................ iv Preface ........................................................................................................................... v Acknowledgments ......................................................................................................... vii Acronyms and Abbreviations ........................................................................................ ix The Chronology ............................................................................................................. 1 1961 ......................................................................................................................... 4 1962 ......................................................................................................................... 5 963 ......................................................................................................................... 5 964 ......................................................................................................................... 6 965 ......................................................................................................................... 6 966 ........................................................................................................................ -
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. -
ULA Rideshare Capabilities for Providing Low-Cost Access to Space
United Launch Alliance Rideshare Capabilities for Providing Low-Cost Access to Space Keith Karuntzos United Launch Alliance PO Box 3788, MIS C4102 Centennial, CO 80155-3788 303-269-5499 [email protected] Abstract-United Launch Alliance (ULA) has a long history of REFERENCES ••••••••••••••••••••••••••••••••••••••••••••••••••••••••• 9 providing launch services to high-value payloads for a variety BIOGRAPHY •••••••••••••••••••••••••••••••••••••••••••••••••••••••••• 9 of customers, including the US Department of Defense, the National Reconnaissance Office, NASA, and commercial customers. These missions have deployed a wide variety of capabilities into Earth orbit and beyond, such as navigation, 1. VVHAT IS RIDESHARE? communication, R&D, observation, and science, all which have Since the dawn of the space age, spacecraft have often provided us with a tremendous amount of knowledge about Earth and our solar system. The majority of these spacecraft shared launch services with one another while being has been launched as primary payloads, and used the full delivered into space. This approach has normally been done capability of the launch vehicle; yet there is a lower-cost to support spacecraftmuch smaller than the primary payload alternative for achieving similar mission objectives: rideshare. it is launching with. By designing launch services in this manner, spacecraft operators were able to deliver more Rideshare is the approach of sharing available launch vehicle payloads to orbit for a fraction of the cost of a full-up launch performance and volume margins with two or more spacecraft service. that would otherwise go underutilized by the spacecraft community. This allows spacecraft customers the opportunity This method of launching multiple payloads into orbit on a to get their spacecraft to orbit and beyond in an inexpensive single launch vehicle is called rideshare.