NASA HISTORICAL DATA BOOK Volume !I
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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. -
SATELLITES at WORK Space in the Seventies
SaLf ILMITRATBONS REPROMhdONkp N BLACK ANd WHiT? SATELLITES AT WORK Space in the Seventies 4 (SPACE IN N72-13 8 6 6 (NASA-EP-8 ) SATELLITES AT WORK THE SEVENTIES) W.R. Corliss (NASA) Jun. 1971 29 p CSCL 22B Unclas Reproduced by G3/31 11470 NATIONAL TECHNICAL u. INFORMATION SERVICE U S Department of Commerce Springfield VA 22151 J National Aeronautics and Space Administration SPACE IN THE SEVENTIES Man has walked on the Moon, made scientific observations there, and brought back to Earth samples of the lunar surface. Unmanned scientific spacecraft have probed for facts about matter, radiation and magnetism in space, and have collected data relating to the Moon, Venus, Mars, the Sun and some of the stars, and reported their findings to ground stations on Earth. Spacecraft have been put into orbit around the Earth as weather observation stations, as communications relay stations for a world-wide telephone and television network, and as aids to navigation. In addition, the space program has accelerated the advance of technology for science and industry, contributing many new ideas, processes and materials. All this took place in the decade of the Sixties. What next? What may be expected of space exploration in the Seventies? NASA has prepared a series of publications and motion pictures to provide a look forward to SPACE IN THE SEVENTIES. The topics covered in this series include: Earth orbital science; planetary exploration; practical applications of satellites; technology utilization; man in space; and aeronautics. SPACE IN THE SEVENTIES presents the planned programs of NASA for the coming decade. -
Chapter Fourteen Men Into Space: the Space Race and Entertainment Television Margaret A. Weitekamp
CHAPTER FOURTEEN MEN INTO SPACE: THE SPACE RACE AND ENTERTAINMENT TELEVISION MARGARET A. WEITEKAMP The origins of the Cold War space race were not only political and technological, but also cultural.1 On American television, the drama, Men into Space (CBS, 1959-60), illustrated one way that entertainment television shaped the United States’ entry into the Cold War space race in the 1950s. By examining the program’s relationship to previous space operas and spaceflight advocacy, a close reading of the 38 episodes reveals how gender roles, the dangers of spaceflight, and the realities of the Moon as a place were depicted. By doing so, this article seeks to build upon and develop the recent scholarly investigations into cultural aspects of the Cold War. The space age began with the launch of the first artificial satellite, Sputnik, by the Soviet Union on October 4, 1957. But the space race that followed was not a foregone conclusion. When examining the United States, scholars have examined all of the factors that led to the space technology competition that emerged.2 Notably, Howard McCurdy has argued in Space and the American Imagination (1997) that proponents of human spaceflight 1 Notably, Asif A. Siddiqi, The Rocket’s Red Glare: Spaceflight and the Soviet Imagination, 1857-1957, Cambridge Centennial of Flight (Cambridge: Cambridge University Press, 2010) offers the first history of the social and cultural contexts of Soviet science and the military rocket program. Alexander C. T. Geppert, ed., Imagining Outer Space: European Astroculture in the Twentieth Century (New York: Palgrave Macmillan, 2012) resulted from a conference examining the intersections of the social, cultural, and political histories of spaceflight in the Western European context. -
Rocket Propulsion Fundamentals 2
https://ntrs.nasa.gov/search.jsp?R=20140002716 2019-08-29T14:36:45+00:00Z Liquid Propulsion Systems – Evolution & Advancements Launch Vehicle Propulsion & Systems LPTC Liquid Propulsion Technical Committee Rick Ballard Liquid Engine Systems Lead SLS Liquid Engines Office NASA / MSFC All rights reserved. No part of this publication may be reproduced, distributed, or transmitted, unless for course participation and to a paid course student, in any form or by any means, or stored in a database or retrieval system, without the prior written permission of AIAA and/or course instructor. Contact the American Institute of Aeronautics and Astronautics, Professional Development Program, Suite 500, 1801 Alexander Bell Drive, Reston, VA 20191-4344 Modules 1. Rocket Propulsion Fundamentals 2. LRE Applications 3. Liquid Propellants 4. Engine Power Cycles 5. Engine Components Module 1: Rocket Propulsion TOPICS Fundamentals • Thrust • Specific Impulse • Mixture Ratio • Isp vs. MR • Density vs. Isp • Propellant Mass vs. Volume Warning: Contents deal with math, • Area Ratio physics and thermodynamics. Be afraid…be very afraid… Terms A Area a Acceleration F Force (thrust) g Gravity constant (32.2 ft/sec2) I Impulse m Mass P Pressure Subscripts t Time a Ambient T Temperature c Chamber e Exit V Velocity o Initial state r Reaction ∆ Delta / Difference s Stagnation sp Specific ε Area Ratio t Throat or Total γ Ratio of specific heats Thrust (1/3) Rocket thrust can be explained using Newton’s 2nd and 3rd laws of motion. 2nd Law: a force applied to a body is equal to the mass of the body and its acceleration in the direction of the force. -
Why NASA Consistently Fails at Congress
W&M ScholarWorks Undergraduate Honors Theses Theses, Dissertations, & Master Projects 6-2013 The Wrong Right Stuff: Why NASA Consistently Fails at Congress Andrew Follett College of William and Mary Follow this and additional works at: https://scholarworks.wm.edu/honorstheses Part of the Political Science Commons Recommended Citation Follett, Andrew, "The Wrong Right Stuff: Why NASA Consistently Fails at Congress" (2013). Undergraduate Honors Theses. Paper 584. https://scholarworks.wm.edu/honorstheses/584 This Honors Thesis is brought to you for free and open access by the Theses, Dissertations, & Master Projects at W&M ScholarWorks. It has been accepted for inclusion in Undergraduate Honors Theses by an authorized administrator of W&M ScholarWorks. For more information, please contact [email protected]. The Wrong Right Stuff: Why NASA Consistently Fails at Congress A thesis submitted in partial fulfillment of the requirement for the degree of Bachelors of Arts in Government from The College of William and Mary by Andrew Follett Accepted for . John Gilmour, Director . Sophia Hart . Rowan Lockwood Williamsburg, VA May 3, 2013 1 Table of Contents: Acknowledgements 3 Part 1: Introduction and Background 4 Pre Soviet Collapse: Early American Failures in Space 13 Pre Soviet Collapse: The Successful Mercury, Gemini, and Apollo Programs 17 Pre Soviet Collapse: The Quasi-Successful Shuttle Program 22 Part 2: The Thin Years, Repeated Failure in NASA in the Post-Soviet Era 27 The Failure of the Space Exploration Initiative 28 The Failed Vision for Space Exploration 30 The Success of Unmanned Space Flight 32 Part 3: Why NASA Fails 37 Part 4: Putting this to the Test 87 Part 5: Changing the Method. -
Privacy Statement Link at the Bottom of Aerojet Rocketdyne Websites
Privacy Notice Aerojet Rocketdyne – For external use Contents Introduction ...................................................................................................................... 3 Why we collect personal information? ............................................................................. 3 How we collect personal information? ............................................................................. 3 How we use information we collect? ............................................................................... 4 How we share your information? .................................................................................... 4 How we protect your personal information? ..................................................................... 4 How we collect consent? .............................................................................................. 4 How we provide you access? ........................................................................................ 4 How to contact Aerojet Rocketdyne privacy?.................................................................... 5 Collection of personal information .................................................................................. 5 Disclosure of personal information.................................................................................. 5 Sale of personal information .......................................................................................... 6 Children’s online privacy .............................................................................................. -
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. -
Design for Demise Analysis for Launch Vehicles
A first design for demise analysis for launch vehicles Henrik Simon, Stijn Lemmens Space debris: Inactive, manmade objects in space Source: ESA Overview Introduction Fundamentals Modelling approach Results and discussion Summary and outlook What is the motivation and task? INTRODUCTION Motivation . Mitigation: Prevention of creation and limitation of long-term presence . Guidelines: LEO removal within 25 years . LEO removal within 25 years after mission end . Casualty risk limit for re-entry: 1 in 10,000 Rising altitude Decay & re-entry above 2000 km Source: NASA Source: NASA Solution: Design for demise Source: ESA Scope of the thesis . Typical design of upper stages . General Risk assessment . Design for demise solutions to reduce the risk ? ? ? Risk A Risk B Risk C Source: CNES How do we assess the risk and simulate the re-entry? FUNDAMENTALS Fundamentals: Ground risk assessment Ah = + 2 Ai � ℎ = =1 � Source: NASA Source: NASA 3.5 m 5.0 m 2 2 ≈ ≈ Fundamentals: Re-entry simulation tools SCARAB: Spacecraft-oriented approach . CAD-like modelling . 6 DoF flight dynamics . Break-up / fragmentation computed How does a rocket upper stage look like? MODELLING Modelling approach . Research on typical design: . Elongated . Platform . Solid Rocket Motor . Lack of information: . Create common intersection . Deliberately stay top-level and only compare effects Modelling approach Modelling approach 12 Length [m] 9 7 5 3 2 150 300 500 700 800 1500 2200 Mass [kg] How much is the risk and how can we reduce it? SIMULATIONS Example of SCARAB re-entry simulation 6x Casualty risk of all reference cases Typical survivors Smaller Smaller fragments fragments Pressure tanks Pressure tanks Main tank Engine Main structure + tanks Design for Demise . -
Nasa, 1957-61
ORGANIZATION AND EARLY HISTORY OF NASA, 1957-61 Allen, George E.: Papers Box 1 Eisenhower, Dwight D. – 1961 [space program] Aurand, Evan P.: Papers Box 7 Reading File, Aug. 16, 1958-Sept. 26. 1958 [Polaris] Box 8 Reading File, Jan. 7, 1958-Mar. 5, 1959 [missile program] Reading File, Oct. 2, 1959-Dec. 31, 1959 [Polaris missiles] Box 14 Aurand, Henry S., Writings of (1)-(7) [satellite orbits] Box 15 Ballistic Missile System Box 17 Missile Trip, April 9-17, 1959 (1)(2) Navy Line File Folder No. One [missile programs] Box 18 Navy Line, 1959 (1)-(4) [missiles and space] Box 19 Outer Space Brownell, Herbert Jr.: Additional Papers Box 10 Sh (1)(2) [missiles] Cochran, Jacqueline: Papers Air Force Series Box 3 Air Force: Space Program 1959 Articles Series Box 7 Article by JC re Women in space for Parade 1961 (1)-(4) Article by JC: “Women Will Go Into Space” 1962 (1)-(4) Box 8 Life Magazine Article re “Women in Space” 1963 Federation Aeronautique Internationale Series (FAI) Box 14 FAI: Space Flight (Alan B. Shepard) May 5, 1961 (1)-(7) National Aeronautic Association Series Box 11 NAA Convention 1961 Speeches (copies) [manned space flight] Box 18 NAA: Col. John Glenn’s Space Flight 2/20/62 Scrapbook Series Box 4 NASA Lunar Orbit Rendezvous 1962 NASA Manned Suborbital Flight 1961 NASA Miscellaneous Items General File Series Box 138 Women in Space: Dr. Hugh Dryden thru Box 140 Women in Space: James Webb, NASA Box 147 National Aeronautics and Space Administration 1963 (1)(2) NASA – JC on “Women in Aerospace” Box 150 Women in Space: Myrtle Cagle (Mrs. -
ARIEL – 13Th Appleton Space Conference PLANETS ARE UBIQUITOUS
Background image credit NASA ARIEL – 13th Appleton Space Conference PLANETS ARE UBIQUITOUS OUR GALAXY IS MADE OF GAS, STARS & PLANETS There are at least as many planets as stars Cassan et al, 2012; Batalha et al., 2015; ARIEL – 13th Appleton Space Conference 2 EXOPLANETS TODAY: HUGE DIVERSITY 3700+ PLANETS, 2700 PLANETARY SYSTEMS KNOWN IN OUR GALAXY ARIEL – 13th Appleton Space Conference 3 HUGE DIVERSITY: WHY? FORMATION & EVOLUTION PROCESSES? MIGRATION? INTERACTION WITH STAR? Accretion Gaseous planets form here Interaction with star Planet migration Ices, dust, gas ARIEL – 13th Appleton Space Conference 4 STAR & PLANET FORMATION/EVOLUTION WHAT WE KNOW: CONSTRAINTS FROM OBSERVATIONS – HERSCHEL, ALMA, SOLAR SYSTEM Measured elements in Solar system ? Image credit ESA-Herschel, ALMA (ESO/NAOJ/NRAO), Marty et al, 2016; André, 2012; ARIEL – 13th Appleton Space Conference 5 THE SUN’S PLANETS ARE COLD SOME KEY O, C, N, S MOLECULES ARE NOT IN GAS FORM T ~ 150 K Image credit NASA Juno mission, NASA Galileo ARIEL – 13th Appleton Space Conference 6 WARM/HOT EXOPLANETS O, C, N, S (TI, VO, SI) MOLECULES ARE IN GAS FORM Atmospheric pressure 0.01Bar H2O gas CO2 gas CO gas CH4 gas HCN gas TiO gas T ~ 500-2500 K Condensates VO gas H2S gas 1 Bar Gases from interior ARIEL – 13th Appleton Space Conference 7 CHEMICAL MEASUREMENTS TODAY SPECTROSCOPIC OBSERVATIONS WITH CURRENT INSTRUMENTS (HUBBLE, SPITZER,SPHERE,GPI) • Precision of 20 ppm can be reached today by Hubble-WFC3 • Current data are sparse, instruments not absolutely calibrated • ~ 40 planets analysed -
Launch Options for the Future: a Buyer's Guide (Part 7 Of
— Chapter 3 Enhanced Baseline CONTENTS , Page Improving the Shuttle . 27 Advanced Solid Rocket Motors (ASRMs) . 27 Liquid Rocket Boosters (LRBs) . 28 Lighter Tanks . 29 Improving Shuttle Ground Operations . 29 Improving Existing ELVs . 29 Delta . 30 Atlas-Centaur . ● ● . .* . 30 Titan . ● . ✎ ✎ . 30 Capability . ✎ . ✎ ✎ . ● ✎ ✎ . 30 Table 3-1. Theoretical Lift Capability of Enhanced U.S. Launch Systems. 31 Chapter 3 Enhanced Baseline The ENHANCED BASELINE option is the U.S. Government’s “Best Buy” if . it desires a space program with current or slightly greater levels of activity. By making in- cremental improvements to existing launch vehicles, production and launch facilities, the U.S. could increase its launch capacity to about 1.4 million pounds per year to LEO. The investment required would be low compared to building new vehicles; however, the ade- quacy of the resulting fleet resiliency and dependability is uncertain. This option would not provide the low launch costs (e.g. 10 percent of current costs) sought for SDI deploy- ment or an aggressive civilian space initiative, like a piloted mission to Mars, IMPROVING THE SHUTTLE The Shuttle, though a remarkable tech- . reducing the number of factory joints and nological achievement, never achieved its in- the number of parts, tended payload capacity and recent safety . designing the ASRMs so that the Space modifications have further degraded its per- Shuttle Main Engines no longer need to formance by approximately 4,800 pounds. be throttled during the region of maxi- Advanced Solid Rocket Motors (ASRMs) or mum dynamic pressure, Liquid Rocket Boosters (LRBs) have the potential to restore some of this perfor- ● replacing asbestos-bearing materials, mance; studies on both are underway. -
Jacques Tiziou Space Collection
Jacques Tiziou Space Collection Isaac Middleton and Melissa A. N. Keiser 2019 National Air and Space Museum Archives 14390 Air & Space Museum Parkway Chantilly, VA 20151 [email protected] https://airandspace.si.edu/archives Table of Contents Collection Overview ........................................................................................................ 1 Administrative Information .............................................................................................. 1 Biographical / Historical.................................................................................................... 1 Scope and Contents........................................................................................................ 2 Arrangement..................................................................................................................... 2 Names and Subjects ...................................................................................................... 2 Container Listing ............................................................................................................. 4 Series : Files, (bulk 1960-2011)............................................................................... 4 Series : Photography, (bulk 1960-2011)................................................................. 25 Jacques Tiziou Space Collection NASM.2018.0078 Collection Overview Repository: National Air and Space Museum Archives Title: Jacques Tiziou Space Collection Identifier: NASM.2018.0078 Date: (bulk 1960s through