Alternatives for Future U.S. Space-Launch Capabilities Pub
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Vulcan Centaur
VULCAN CENTAUR The Vulcan Centaur rocket design leverages the flight-proven success of the Delta IV and Atlas V launch vehicles while introducing new technologies and innovative features to ensure a reliable and aordable space launch service. Vulcan Centaur will service a diverse range of markets including 225 ft commercial, civil, science, cargo and national security space customers. 1 The spacecraft is encapsulated in a 5.4-m- (17.7-ft-) diameter payload fairing (PLF), a sandwich composite structure made with a vented aluminum-honeycomb core and graphite-epoxy face sheets. The bisector (two-piece shell) PLF encapsulates the spacecraft. The payload attach fitting (PAF) is a similar sandwich composite structure creating the mating interface from spacecraft to second stage. The PLF separates using a debris-free horizontal and vertical separation system with 2 200 ft spring packs and frangible joint assembly. The payload fairing is available in the 15.5-m (51-ft) standard and 21.3-m (70-ft) 1 long configurations. The Centaur upper stage is 5.4 m (17.7 ft) in diameter and 3 11.7 m (38.5 ft) long with a 120,000-lb propellant capacity. Its propellant tanks are constructed of pressure-stabilized, corrosion-resistant stainless steel. Centaur is a liquid hydrogen/liquid oxygen-fueled vehicle, with two RL10C 4 engines. The Vulcan Centaur Heavy vehicle, flies the upgraded 2 Centaur using RL10CX engines with nozzle extensions. The 5 175 ft cryogenic tanks are insulated with spray-on foam insulation (SOFI) to manage boil o of cryogens during flight. An aft equipment shelf provides the structural mountings for vehicle electronics. -
Rns Over the Long Term and Critical to Enabling This Is Continued Investment in Our Technology and People, a Capital Allocation Priority
19 May 2021 FUTURE plc 2021 HALF YEAR RESULTS Strategic momentum continues: record HY results, materially ahead of market expectations, with strong organic growth and margin progression Future plc (LSE: FUTR, “Future”, “the Group”), the global platform for specialist media, today publishes its results for the six months ended 31 March 2021. Highlights Financial results for the six months ended 31 March 2021 Adjusted results HY 2021 HY 2020 Var Revenue (£m) 272.6 144.3 +89% Adjusted operating profit (£m)1 89.2 39.9 +124% Adjusted operating profit margin (%) 33% 28% +5ppt Adjusted diluted EPS (p) 65.4 32.9 +99% Statutory results HY 2021 HY 2020 Var Revenue (£m) 272.6 144.3 +89% Operating profit (£m) 59.7 24.7 +142% Profit before tax (£m) 56.9 27.1 +110% Cash generated from operations (£m) 85.9 35.7 +141% Diluted EPS (p) 40.7 21.8 +87% Financial highlights Robust first-half performance extending our track record of growth in revenue, operating profit and cash flow: An exceptionally strong first half, with revenue up 89% to £272.6m (HY 2020: £144.3m). Revenue ahead of last year by 21% on an organic2 basis, driven by the Media division’s organic2 growth of 30% and in particular digital advertising on-platform organic2 growth of 30% and eCommerce affiliates’ organic2 growth of 56%. US achieved revenue growth of 31% on an organic2 basis and UK revenues grew by 5% organically (UK has a higher mix of events and magazines revenues which were impacted more materially by the pandemic). -
Space Administration
https://ntrs.nasa.gov/search.jsp?R=19700024651 2020-03-23T18:20:34+00:00Z TO THE CONGRESSOF THE UNITEDSTATES : Transmitted herewith is the Twenty-first Semiannual Repol* of the National Aeronautics and Space Administration. Twen~-first SEMIANNUAL REPORT TO CONGRESS JANUARY 1 - JUNE 30, 1969 NATIONAL AERONAUTICS AND SPACE ADMINISTRATION WASHINGTON, D. C. 20546 Editors: G. B. DeGennaro, H. H. Milton, W. E. Boardman, Office of Public Affairs; Art work: A. Jordan, T. L. Lindsey, Office of Organiza- tion and Management. For sale by the Superintendent of Documents, U.S. Government Printing Office Washington, D.C. 20402-Price $1.25 THE PRESIDENT May 27,1970 The White House I submit this Twenty-First Semiannual Report of the National Aeronautics and Space Aldministration to you for transmitttal to Congress in accordance with section 206(a) of the National Aero- nautics and Space Act of 1958. It reports on aotivities which took place betiween January 1 and June 30, 1969. During this time, the Nation's space program moved forward on schedule. ApolIo 9 and 10 demonstrated the ability of ;the man- ned Lunar Module to operate in earth and lunar orbit and its 'eadi- ness to attempt the lunar landing. Unmanned observatory and ex- plorer class satellites carried on scientific studies of the regions surrounding the Earth, the Moon, and the Sun; a Biosatellite oarwing complex biological science experiment was orbited; and sophisticated weather satellites and advanced commercial com- munications spacecraft became operational. Advanced research projects expanded knowledge of space flighk and spacecraft engi- neering as well as of aeronautics. -
New Pad Constructed for Smaller Rocket Launches
PROGRAM HIGHLIGHTS • JULY 2015 At NASA’s Kennedy Space Center in Florida, the Ground Systems Development and Operations (GSDO) Program Office is leading the center’s transfor- mation from a historically government-only launch complex to a spaceport bustling with activity involving government and commercial vehicles alike. GSDO is tasked with developing and using the complex equipment required to safely handle a variety of rockets and spacecraft during assembly, transport and launch. For more information about GSDO accomplishments happening around the center, visit http://go.nasa.gov/groundsystems. New Pad Constructed for Smaller Rocket Launches NASA's Kennedy Space Center in Florida took another step forward in its transformation to a 21st century multi-user spaceport with the completion of the new Small Class Vehicle Launch Pad, designated 39C, in the Launch Pad 39B area. This designated pad to test smaller rockets will make it more affordable for smaller aerospace companies to develop and launch from the center, and to break into the commercial spaceflight market. Kennedy Director Bob Cabana and representatives from the Ground Systems Development and Operations (GSDO) Program and the Center Planning and Development (CPD) and Engineering Directorates marked the completion of the new pad during a ribbon-cutting ceremony July 17. NASA Kennedy Space Center Director Bob Cabana, center, helps cut the ribbon on the new Small Class Vehicle Launch Pad, designated 39C, at Kennedy Space Center in Florida. Also helping to cut the ribbon are, from left, Pat Simpkins, director, Engineering and Technology Directorate; Rich Koller, senior vice president of design firm Jones Edmunds; Scott Col- loredo, director, Center Planning and Development; and Michelle Shoultz, president of Frazier Engineering. -
Progress Report on Apollo Program
PROGRESS REPORT ON APOLLO PROGRAM Michael Collins, LCol. USAF (M) Astronaut NASA-MANNED SPACECRAFT CENTER It is a great pleasure to be here today and to greet you hardy suMvors of the pool party. I will do my best to avoid loud noises and bright colors during my status report. Since the last SETP Symposium, the Apollo Program has been quite busy in a number of different areas. (Figure 1) My problem is to sift through this information and to talk only about those things of most interest to you. First, to review briefly our hardware, we are talking about two different spacecraft and two different boosters. (Figure 2) The Command Module is that part of the stack COLLINS which makes the complete round trip to the moon. Attached to it is the Service Module, containing expendables and a 20,000 pound thrust engine for maneuverability. The Lunar Module will be carried on later flights and is the landing vehicle and active rendezvous partner. The uprated Saturn I can put the Command and Service Modules into earth orbit; the Saturn V is required when the Lunar Module is added. Since the last symposium, we have flown the Command and Service Modules twice and the Lunar Module once, all unmanned. Apollo 4, the first Saturn V flight, was launched in November 1967. (Figure 3) The Saturn V did a beautiful, i.e. nominal, job of putting the spacecraft into earth parking orbit. After a coast period, the third stage (S-IVB by McDonnell Douglas) was ignited a second time, achieving a highly elliptical orbit. -
Proposal to Construct and Operate a Satellite Launching Facility on Christmas Island
Environment Assessment Report PROPOSAL TO CONSTRUCT AND OPERATE A SATELLITE LAUNCHING FACILITY ON CHRISTMAS ISLAND Environment Assessment Branch 2 May 2000 Christmas Island Satellite Launch Facility Proposal Environment Assessment Report - Environment Assessment Branch – May 2000 3 Table of Contents 1 INTRODUCTION..............................................................................................6 1.1 GENERAL ...........................................................................................................6 1.2 ENVIRONMENT ASSESSMENT............................................................................7 1.3 THE ASSESSMENT PROCESS ...............................................................................7 1.4 MAJOR ISSUES RAISED DURING THE PUBLIC COMMENT PERIOD ON THE DRAFT EIS .................................................................................................................9 1.4.1 Socio-economic......................................................................................10 1.4.2 Biodiversity............................................................................................10 1.4.3 Roads and infrastructure .....................................................................11 1.4.4 Other.......................................................................................................12 2 NEED FOR THE PROJECT AND KEY ALTERNATIVES ......................14 2.1 NEED FOR THE PROJECT ..................................................................................14 2.2 KEY -
Rocket Nozzles: 75 Years of Research and Development
Sådhanå Ó (2021) 46:76 Indian Academy of Sciences https://doi.org/10.1007/s12046-021-01584-6Sadhana(0123456789().,-volV)FT3](0123456789().,-volV) Rocket nozzles: 75 years of research and development SHIVANG KHARE1 and UJJWAL K SAHA2,* 1 Department of Energy and Process Engineering, Norwegian University of Science and Technology, 7491 Trondheim, Norway 2 Department of Mechanical Engineering, Indian Institute of Technology Guwahati, Guwahati 781039, India e-mail: [email protected]; [email protected] MS received 28 August 2020; revised 20 December 2020; accepted 28 January 2021 Abstract. The nozzle forms a large segment of the rocket engine structure, and as a whole, the performance of a rocket largely depends upon its aerodynamic design. The principal parameters in this context are the shape of the nozzle contour and the nozzle area expansion ratio. A careful shaping of the nozzle contour can lead to a high gain in its performance. As a consequence of intensive research, the design and the shape of rocket nozzles have undergone a series of development over the last several decades. The notable among them are conical, bell, plug, expansion-deflection and dual bell nozzles, besides the recently developed multi nozzle grid. However, to the best of authors’ knowledge, no article has reviewed the entire group of nozzles in a systematic and comprehensive manner. This paper aims to review and bring all such development in one single frame. The article mainly focuses on the aerodynamic aspects of all the rocket nozzles developed till date and summarizes the major findings covering their design, development, utilization, benefits and limitations. -
Measurements of Π , K , P and ¯P Spectra in Proton-Proton
EUROPEAN ORGANISATION FOR NUCLEAR RESEARCH (CERN) Submitted to: Eur. Phys. J. C CERN-EP-2017-066 September 28, 2017 Measurements of π±,K±, p and ¯p spectra in proton-proton interactions at 20, 31, 40, 80 and 158 GeV=c with the NA61/SHINE spectrometer at the CERN SPS The NA61/SHINE Collaboration Measurements of inclusive spectra and mean multiplicities of π±,K±, p and p¯ produced in =c inelasticp p+p interactions at incident projectile momenta of 20, 31, 40, 80 and 158 GeV ( s = 6.3, 7.7, 8.8, 12.3 and 17.3 GeV, respectively) were performed at the CERN Super Proton Synchrotron using the large acceptance NA61/SHINE hadron spectrometer. Spectra are presented as function of rapidity and transverse momentum and are compared to predictions of current models. The measurements serve as the baseline in the NA61/SHINE study of the properties of the onset of deconfinement and search for the critical point of strongly interacting matter. arXiv:1705.02467v2 [nucl-ex] 27 Sep 2017 © 2017 CERN for the benefit of the NA61/SHINE Collaboration. Reproduction of this article or parts of it is allowed as specified in the CC-BY-4.0 license. 1. Introduction This paper presents experimental results on inclusive spectra and mean multiplicities of π±,K±, p and p¯ produced in inelastic p+p interactions at 20, 31, 40, 80 and 158 GeV=c. The measurements were performed by the multi-purpose NA61/SHINE experiment [1, 2] at the CERN Super Proton Synchrotron (SPS). The new measurements complement previously published results from the same datasets on π− production [3] obtained without particle identification as well as on fluctuations of charged particles [4]. -
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. -
Human Behavior During Spaceflight - Videncee from an Analog Environment
Journal of Aviation/Aerospace Education & Research Volume 25 Number 1 JAAER Fall 2015 Article 2 Fall 2015 Human Behavior During Spaceflight - videnceE From an Analog Environment Kenny M. Arnaldi Embry-Riddle Aeronautical University, [email protected] Guy Smith Embry-Riddle Aeronautical University, [email protected] Jennifer E. Thropp Embry-Riddle Aeronautical University - Daytona Beach, [email protected] Follow this and additional works at: https://commons.erau.edu/jaaer Part of the Applied Behavior Analysis Commons, Experimental Analysis of Behavior Commons, and the Other Astrophysics and Astronomy Commons Scholarly Commons Citation Arnaldi, K. M., Smith, G., & Thropp, J. E. (2015). Human Behavior During Spaceflight - videnceE From an Analog Environment. Journal of Aviation/Aerospace Education & Research, 25(1). https://doi.org/ 10.15394/jaaer.2015.1676 This Article is brought to you for free and open access by the Journals at Scholarly Commons. It has been accepted for inclusion in Journal of Aviation/Aerospace Education & Research by an authorized administrator of Scholarly Commons. For more information, please contact [email protected]. Arnaldi et al.: Human Behavior During Spaceflight - Evidence From an Analog Environment Introduction Four years after the launch of Sputnik, the world’s first artificial satellite, Yuri Gagarin became the first human to reach space (National Aeronautics and Space Administration [NASA], 2011a). The United States soon followed on the path of manned space exploration with Project Mercury. Although this program began with suborbital flights, manned spacecraft were subsequently launched into orbit around the Earth (NASA, 2012). With President Kennedy setting the goal of landing a man on the moon, NASA focused on short-duration orbital flights as a stepping-stone to lunar missions. -
Enceladus, Moon of Saturn
National Aeronautics and and Space Space Administration Administration Enceladus, Moon of Saturn www.nasa.gov Enceladus (pronounced en-SELL-ah-dus) is an icy moon of Saturn with remarkable activity near its south pole. Covered in water ice that reflects sunlight like freshly fallen snow, Enceladus reflects almost 100 percent of the sunlight that strikes it. Because the moon reflects so much sunlight, the surface temperature is extremely cold, about –330 degrees F (–201 degrees C). The surface of Enceladus displays fissures, plains, corrugated terrain and a variety of other features. Enceladus may be heated by a tidal mechanism similar to that which provides the heat for volca- An artist’s concept of Saturn’s rings and some of the icy moons. The ring particles are composed primarily of water ice and range in size from microns to tens of meters. In 2004, the Cassini spacecraft passed through the gap between the F and G rings to begin orbiting Saturn. noes on Jupiter’s moon Io. A dramatic plume of jets sprays water ice and gas out from the interior at ring material, coating itself continually in a mantle Space Agency. The Jet Propulsion Laboratory, a many locations along the famed “tiger stripes” at of fresh, white ice. division of the California Institute of Technology, the south pole. Cassini mission data have provided manages the mission for NASA. evidence for at least 100 distinct geysers erupting Saturn’s Rings For images and information about the Cassini on Enceladus. All of this activity, plus clues hidden Saturn’s rings form an enormous, complex struc- mission, visit — http://saturn.jpl.nasa.gov/ in the moon’s gravity, indicates that the moon’s ture. -
The International Space Station and the Space Shuttle
Order Code RL33568 The International Space Station and the Space Shuttle Updated November 9, 2007 Carl E. Behrens Specialist in Energy Policy Resources, Science, and Industry Division The International Space Station and the Space Shuttle Summary The International Space Station (ISS) program began in 1993, with Russia joining the United States, Europe, Japan, and Canada. Crews have occupied ISS on a 4-6 month rotating basis since November 2000. The U.S. Space Shuttle, which first flew in April 1981, has been the major vehicle taking crews and cargo back and forth to ISS, but the shuttle system has encountered difficulties since the Columbia disaster in 2003. Russian Soyuz spacecraft are also used to take crews to and from ISS, and Russian Progress spacecraft deliver cargo, but cannot return anything to Earth, since they are not designed to survive reentry into the Earth’s atmosphere. A Soyuz is always attached to the station as a lifeboat in case of an emergency. President Bush, prompted in part by the Columbia tragedy, made a major space policy address on January 14, 2004, directing NASA to focus its activities on returning humans to the Moon and someday sending them to Mars. Included in this “Vision for Space Exploration” is a plan to retire the space shuttle in 2010. The President said the United States would fulfill its commitments to its space station partners, but the details of how to accomplish that without the shuttle were not announced. The shuttle Discovery was launched on July 4, 2006, and returned safely to Earth on July 17.