Air University Space Primer
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Materials for Liquid Propulsion Systems
https://ntrs.nasa.gov/search.jsp?R=20160008869 2019-08-29T17:47:59+00:00Z CHAPTER 12 Materials for Liquid Propulsion Systems John A. Halchak Consultant, Los Angeles, California James L. Cannon NASA Marshall Space Flight Center, Huntsville, Alabama Corey Brown Aerojet-Rocketdyne, West Palm Beach, Florida 12.1 Introduction Earth to orbit launch vehicles are propelled by rocket engines and motors, both liquid and solid. This chapter will discuss liquid engines. The heart of a launch vehicle is its engine. The remainder of the vehicle (with the notable exceptions of the payload and guidance system) is an aero structure to support the propellant tanks which provide the fuel and oxidizer to feed the engine or engines. The basic principle behind a rocket engine is straightforward. The engine is a means to convert potential thermochemical energy of one or more propellants into exhaust jet kinetic energy. Fuel and oxidizer are burned in a combustion chamber where they create hot gases under high pressure. These hot gases are allowed to expand through a nozzle. The molecules of hot gas are first constricted by the throat of the nozzle (de-Laval nozzle) which forces them to accelerate; then as the nozzle flares outwards, they expand and further accelerate. It is the mass of the combustion gases times their velocity, reacting against the walls of the combustion chamber and nozzle, which produce thrust according to Newton’s third law: for every action there is an equal and opposite reaction. [1] Solid rocket motors are cheaper to manufacture and offer good values for their cost. -
Past, Present, and Future
Rockets: Past, Present, and Future Robert Goddard With his Original Rocket system Delta IV … biggest commercial Rocket system currently in US arsenal Material from Rockets into Space by Frank H. Winter, ISBN 0-674-77660-7 MAE 5540 - Propulsion Systems Earliest Rockets as weapons • Chinese development, Sung dynasty (A.D. 960-1279) – Primarily psychological • William Congreve, England, 1804 – thus “the rockets red glare” during the war of 1812. – 1.5 mile range, very poor accuracy. • V2 in WWII MAE 5540 - Propulsion Systems First Principle of Rocket Flight • “For every action there is an equal and opposite reaction.” Isaac Newton, 1687, following Archytas of Tarentum, 360 BC, and Hero of Alexandria, circa 50 AD. • “Rockets move because the flame pushes against the surrounding air.” Edme Mariotte, 1717 • Which one is correct? MAE 5540 - Propulsion Systems Isaac Newton explains how to launch a Satellite MAE 5540 - Propulsion Systems The Reaction-propelled Spaceship of Hermann Ganswindt (1890) • The fuel for his spaceship consisted of heavy steel cartridges with dynamite charges. They were to be fed machine gun style into a reaction chamber where they would fire and be dropped away. • “Shock absorbers protected the travelers” MAE 5540 - Propulsion Systems The Three Amigos of Spaceflight Theory • Konstantin Tsiolkovsky • Hermann Oberth • Robert Goddard • Independent and parallel development of Rocket theory MAE 5540 - Propulsion Systems Three Amigos • Goddard • Oberth • Tsiolkovsky MAE 5540 - Propulsion Systems Konstantin Tsiolkovsky 1857 - 1935 • Deaf Russian School Teacher - fascinated with space flight, started by writing Science Fiction Novels • Discovered that practical space flight depended on liquid fuel rockets in the 1890’s, and developed the fundamental Rocket equation in 1897. -
The Annual Compendium of Commercial Space Transportation: 2017
Federal Aviation Administration The Annual Compendium of Commercial Space Transportation: 2017 January 2017 Annual Compendium of Commercial Space Transportation: 2017 i Contents About the FAA 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 51 United States Code, Subtitle V, Chapter 509 (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 website: http://www.faa.gov/go/ast Cover art: Phil Smith, The Tauri Group (2017) Publication produced for FAA AST by The Tauri Group under contract. 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. ii Annual Compendium of Commercial Space Transportation: 2017 GENERAL CONTENTS Executive Summary 1 Introduction 5 Launch Vehicles 9 Launch and Reentry Sites 21 Payloads 35 2016 Launch Events 39 2017 Annual Commercial Space Transportation Forecast 45 Space Transportation Law and Policy 83 Appendices 89 Orbital Launch Vehicle Fact Sheets 100 iii Contents DETAILED CONTENTS EXECUTIVE SUMMARY . -
Evolved Expendable Launch Operations at Cape Canaveral, 2002-2009
EVOLVED EXPENDABLE LAUNCH OPERATIONS AT CAPE CANAVERAL 2002 – 2009 by Mark C. Cleary 45th SPACE WING History Office PREFACE This study addresses ATLAS V and DELTA IV Evolved Expendable Launch Vehicle (EELV) operations at Cape Canaveral, Florida. It features all the EELV missions launched from the Cape through the end of Calendar Year (CY) 2009. In addition, the first chapter provides an overview of the EELV effort in the 1990s, summaries of EELV contracts and requests for facilities at Cape Canaveral, deactivation and/or reconstruction of launch complexes 37 and 41 to support EELV operations, typical EELV flight profiles, and military supervision of EELV space operations. The lion’s share of this work highlights EELV launch campaigns and the outcome of each flight through the end of 2009. To avoid confusion, ATLAS V missions are presented in Chapter II, and DELTA IV missions appear in Chapter III. Furthermore, missions are placed in three categories within each chapter: 1) commercial, 2) civilian agency, and 3) military space operations. All EELV customers employ commercial launch contractors to put their respective payloads into orbit. Consequently, the type of agency sponsoring a payload (the Air Force, NASA, NOAA or a commercial satellite company) determines where its mission summary is placed. Range officials mark all launch times in Greenwich Mean Time, as indicated by a “Z” at various points in the narrative. Unfortunately, the convention creates a one-day discrepancy between the local date reported by the media and the “Z” time’s date whenever the launch occurs late at night, but before midnight. (This proved true for seven of the military ATLAS V and DELTA IV missions presented here.) In any event, competent authorities have reviewed all the material presented in this study, and it is releasable to the general public. -
+ Part 17: Acronyms and Abbreviations (265 Kb PDF)
17. Acronyms and Abbreviations °C . Degrees.Celsius °F. Degrees.Fahrenheit °R . Degrees.Rankine 24/7. 24.Hours/day,.7.days/week 2–D. Two-Dimensional 3C. Command,.Control,.and.Checkout 3–D. Three-Dimensional 3–DOF . Three-Degrees.of.Freedom 6-DOF. Six-Degrees.of.Freedom A&E. Architectural.and.Engineering ACEIT. Automated.Cost-Estimating.Integrated.Tools ACES . Acceptance.and.Checkout.Evaluation.System ACP. Analytical.Consistency.Plan ACRN. Assured.Crew.Return.Vehicle ACRV. Assured.Crew.Return.Vehicle AD. Analog.to.Digital ADBS. Advanced.Docking.Berthing.System ADRA. Atlantic.Downrange.Recovery.Area AEDC. Arnold.Engineering.Development.Center AEG . Apollo.Entry.Guidance AETB. Alumina.Enhanced.Thermal.Barrier AFB .. .. .. .. .. .. .. Air.Force.Base AFE. Aero-assist.Flight.Experiment AFPG. Apollo.Final.Phase.Guidance AFRSI. Advanced.Flexible.Reusable.Surface.Insulation AFV . Anti-Flood.Valve AIAA . American.Institute.of.Aeronautics.and.Astronautics AL. Aluminum ALARA . As.Low.As.Reasonably.Achievable 17. Acronyms and Abbreviations 731 AL-Li . Aluminum-Lithium ALS. Advanced.Launch.System ALTV. Approach.and.Landing.Test.Vehicle AMS. Alpha.Magnetic.Spectrometer AMSAA. Army.Material.System.Analysis.Activity AOA . Analysis.of.Alternatives AOD. Aircraft.Operations.Division APAS . Androgynous.Peripheral.Attachment.System APS. Auxiliary.Propulsion.System APU . Auxiliary.Power.Unit APU . Auxiliary.Propulsion.Unit AR&D. Automated.Rendezvous.and.Docking. ARC . Ames.Research.Center ARF . Assembly/Remanufacturing.Facility ASE. Airborne.Support.Equipment ASI . Augmented.Space.Igniter ASTWG . Advanced.Spaceport.Technology.Working.Group ASTP. Advanced.Space.Transportation.Program AT. Alternate.Turbopump ATCO. Ambient.Temperature.Catalytic.Oxidation ATCS . Active.Thermal.Control.System ATO . Abort-To-Orbit ATP. Authority.to.Proceed ATS. Access.to.Space ATV . Automated.Transfer.Vehicles ATV . -
US Commercial Space Transportation Developments and Concepts
Federal Aviation Administration 2008 U.S. Commercial Space Transportation Developments and Concepts: Vehicles, Technologies, and Spaceports January 2008 HQ-08368.INDD 2008 U.S. Commercial Space Transportation Developments and 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/. Federal Aviation Administration Office of Commercial Space Transportation i About FAA/AST 2008 U.S. Commercial Space Transportation Developments and Concepts 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. ii Federal Aviation Administration Office of Commercial Space Transportation 2008 U.S. Commercial Space Transportation Developments and Concepts Contents Table of Contents Introduction . .1 Space Competitions . .1 Expendable Launch Vehicle Industry . .2 Reusable Launch Vehicle Industry . -
Boeing's Delta Rockets Have Been a Mainstay of the Space Launch
Historical Perspective Boeing’s Delta rockets have been a mainstay of the space launch business for 50 years by Robert Villanueva n May 13, 1960, the first Delta satellites and scientific probes to planetary Delta would launch satellites that rocket lifted off from Cape Canav- rover vehicles. revolutionized weather forecasting and the Oeral’s launch pad 17A carrying Delta’s origins date back to Boeing first Telstar and Intelsat satellites, which the Echo 1 satellite. Although that mission predecessor company Douglas’ design enabled the TV phrase, “live via satellite.” failed, the program quickly followed up for the Thor intermediate-range ballistic Design changes allowed Delta to carry in August with the successful launch of missile, developed in the mid-1950s for increasingly larger and heavier payloads Echo 1A. It marked the beginning of what the U.S. Air Force. Thor, a single-stage, to space. These included larger first-stage would become one of the most successful liquid-fueled rocket, made its first success- tanks, the addition of strap-on solid rocket space launch systems ever developed. ful launch on Sept. 20, 1957, and provided boosters, increased propellant capacity, Fifty years and some 348 launches later, nuclear deterrence before intercontinental an improved main engine, adoption of Delta rockets are still flying, carrying into ballistic missiles. Thor later was modified advanced electronics and guidance space everything from earth-orbiting to become the Delta launch vehicle. systems, and development of upper 12 BOEING FRONTIERS / HISTORICAL PERSPECTIVE BOEING FRONTIERS / MAY 2010 stage and satellite payload systems. The Delta IV is manufactured at a Until the early 1980s, Delta was NASA’s 1.5-million-square-foot (140,000-square- primary launch vehicle for communications, meter) production facility in Decatur, Ala. -
Evolved Expendable Launch Vehicle Program
FINAL Supplemental Environmental Impact Statement for the Evolved Expendable Launch Vehicle Program ENOVARUM PRAESTARUM (Affordability Through Innovation) EXPE D N E D V A L B L O E V E L E A U L N I C C H V E H March 2000 SCO152209.00.03.01.03\Covers EELV GBC Cover-1.FH8 03/00 COVER SHEET FINAL SUPPLEMENTAL ENVIRONMENTAL IMPACT STATEMENT EVOLVED EXPENDABLE LAUNCH VEHICLE PROGRAM a. Responsible Agency: U.S. Air Force b. Cooperating Agencies: Federal Aviation Administration (FAA) National Aeronautics and Space Administration (NASA) c. Proposed Action: To allow the addition of up to five strap-on solid rocket motors (SRMs) to the Atlas V lift vehicle and to allow the use of larger SRMs on the Delta IV lift vehicle. Both vehicles are part of the Evolved Expendable Launch Vehicle (EELV) program. d. Inquiries on this document should be directed to: Mr. Jonathan D. Farthing, Chief, Environmental Analysis Division, HQ AFCEE/ECA, 3207 North Road, Brooks Air Force Base, Texas, 78235-5363, (210) 536-3668, facsimile number (210) 536-3890. e. Designation: Final Supplemental Environmental Impact Statement (FSEIS) f. Abstract: This FSEIS has been prepared in accordance with the National Environmental Policy Act (NEPA). Implementation of the EELV program was previously assessed in the April 1998 Final Environmental Impact Statement, Evolved Expendable Launch Vehicle Program. The Proposed Action of this FSEIS is to allow the addition of up to five strap-on SRMs to the Lockheed Martin Corporation (LMC) Atlas V launch vehicle and to allow the use of larger SRMs on the Boeing Delta IV launch vehicle, both of which are part of the EELV program. -
Critical Events of the Inaugural Launch of the Boeing Delta Iv Expendable Launch Vehicle
CRITICAL EVENTS OF THE INAUGURAL LAUNCH OF THE BOEING DELTA IV EXPENDABLE LAUNCH VEHICLE Michael D. Berglund* [email protected] Mark Wilkins† Chief Engineer The Boeing Company Huntington Beach, California 92647 ABSTRACT Integrating a new launch vehicle with new ground On 20 November 2002, in its inaugural launch, The systems and achieving mission success on the inaugural Boeing Company’s Delta IV expendable launch vehicle launch posed many unique challenges. This paper lifted off from Cape Canaveral Air Force Station, summarizes the critical events and challenges of the day Florida, at 5:39 EST. The rocket flawlessly deployed of launch, from tanking through spacecraft separation. its payload (Eutelsat’s W5 spacecraft) approximately 35 Liftoff, max Q, solid rocket motor separation, main min later into a geosynchronous transfer orbit. This engine cutoff (MECO), stage I/II separation, and launch represented the beginning of a new family of second-stage engine cutoff (SECO) are some of the rockets, designed to deliver highly reliable, low-cost critical events that are summarized. Also, this paper access to space for military, commercial, and scientific presents the methodology used in post-flight data endeavors. reconstruction and analysis. Delta II Delta IV Delta IV 7920/7925 Delta III Medium Delta IV Medium+ Heavy 5-m Fairing (Boeing-built) 4-m Fairing (Delta III) Delta III US Modified Delta III US Stretched Tank RL10B-2 RL10B-2 Isogrid First- Stage LO2 Tank Common Booster Core CBC 4 GEM Rocketdyne 2 GEM Engine 60s RS-27 60s RS-68 Main Engine M+ (4,2) M+ (5,2) M+ (5,4) 2,142 kg 3,810 kg 3,934 kg 5,691 kg 4,540 kg 6,411 kg 12,369 kg 4,723 lb 8,400 lb 8,672 lb 12,546 lb 10,008 lb 14,135 lb 27,269 lb Delta IV Nominal Performance to GTO (185 km x 35,786 km x 27 deg) 3P255001.1 Delta II Nominal Performance to GTO (185 km x 35,786 km x 28.7 deg) Note: All Values are Assured Separated Spacecraft Mass and are Derived From the October 2000 Delta IV Payload Planners Guide Figure 1. -
Air Force Science and Technology Contributions to the Nation
The Limitless Sky Air Force Science and Technology Contributions to the Nation Edited by: Alexander H. Levis Chief Scientist, USAF with the assistance of Colonel John C. Bedford, USAF, Ret. Captain Sandra Davis Air Force History and Museums Program United States Air Force Washington, D.C. 2004 “…problems never have a final or universal answer, and only constant inquisitive attitude towards science and a ceaseless and swift adaptation to new development can maintain the security of this nation through… air supremacy” Dr. Theodore onv Kármán to General Henry H. “Hap” Arnold 15 December 1945 To the Air Force scientists and engineers, military and civilian, for keeping true to von Kármán’s vision. Acknowledgement Neither the Symposium nor this book would have been possible without the support of a number of organizations. The Air Force Association provided a venue for the Symposium and made it a part of its Fall ’03 convention in Washington, D.C. The Air Force Legislative Liaison and the Public Affairs Offices provided administrative support and publicity, while the Centennial of Flight Office included this activity in the centennial program. The organizing committee was chaired by Col. John B. Bedford, AF/ST, and included Alexander G. Levis and Nancy C. Stenger from AF/ST, Bill Heimdahl from AF/HO, Col. Tom Schubert from AF/LL, Maj. Michelle Ryan, AF/CVAH, and Napoleon Byars from AFA. The Program Committee had the responsibility of selecting the topics and working with the multiple authors to produce the papers and the presentations. The committee was chaired by Alexander H. Levis, AF/ST, and included Barbara A. -
National Security Space Launch Report
THE ARTS This PDF document was made available from www.rand.org as a public CHILD POLICY service of the RAND Corporation. CIVIL JUSTICE EDUCATION Jump down to document ENERGY AND ENVIRONMENT 6 HEALTH AND HEALTH CARE INTERNATIONAL AFFAIRS The RAND Corporation is a nonprofit research NATIONAL SECURITY POPULATION AND AGING organization providing objective analysis and effective PUBLIC SAFETY solutions that address the challenges facing the public SCIENCE AND TECHNOLOGY and private sectors around the world. SUBSTANCE ABUSE TERRORISM AND HOMELAND SECURITY TRANSPORTATION AND INFRASTRUCTURE Support RAND WORKFORCE AND WORKPLACE Purchase this document Browse Books & Publications Make a charitable contribution For More Information Visit RAND at www.rand.org Explore RAND National Defense Research Institute View document details Limited Electronic Distribution Rights This document and trademark(s) contained herein are protected by law as indicated in a notice appearing later in this work. This electronic representation of RAND intellectual property is provided for non- commercial use only. Permission is required from RAND to reproduce, or reuse in another form, any of our research documents for commercial use. This product is part of the RAND Corporation monograph series. RAND mono- graphs present major research findings that address the challenges facing the public and private sectors. All RAND monographs undergo rigorous peer review to ensure high standards for research quality and objectivity. National Security Space Launch Report The Congressionally Mandated National Security Space Launch Requirements Panel Prepared for the Office of the Secretary of Defense Approved for public release; distribution unlimited The research described in this report was prepared for the Office of the Secretary of Defense (OSD). -
Delta 4 Fact Sheet
Mission: GPS II-5 Launch Vehicle: Delta 4 Launch Date: February 20, 2014 www.spaceflightnow.com Launch Window: 8:40 - 8:59 p.m. Text by: Justin Ray [email protected] Design by: Walter Scriptunas II [email protected] Fact SHEET Delta rockets have been flying for more than 50 years, but the Delta 4 dwarfs its predecessors in sheer size and Earth-shaking power to launch much larger cargos than possible in the past. Development of Delta 4 began in the mid-1990s, giving the Delta team the chance to create a fleet of heavy-lift rockets that would fly through at least 2020, lofting commercial, military and civilian spacecraft. The Delta 4 family features a brand new first stage and main engine, rebuilt launch pads at Cape Canaveral, Florida, and Vandenberg Air Force Base in California, and a new rocket manufacturing plant in Decatur, Alabama. Image Credit: Pat Corkery/ United Launch Alliance There are five versions of the Delta 4 launcher, each incrementally increasing the size or weight of the payload to be placed in space. All configurations feature a Common Booster Core first stage and Rocketdyne-made RS-68 liquid hydrogen/liquid oxygen main engine and an upper stage with Aerojet Rocketdyne's RL10B-2 cryogenic engine. The upper stage and RL10 have already flown on the Delta 3 rocket, along with the Delta program's proven avionics and Redundant Inertial Flight Control Assembly (RIFCA) guidance computer. What separates the different variants is the use of either two or four Alliant-made strap-on solid rocket motors and the selection of either a four- or five-meter diameter nose cone to enclose the satellite cargo.