+ Dec. 5, 1997 -- U.S. Space Exploration in the Next
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An Overview of Mars Vicinity Transportation Concepts for a Human Mars Mission
An Overview of Mars Vicinity Transportation Concepts for a Human Mars Mission Carol E. Dexter NASA/MSFC Exploration Transportation Office Larry Kos NASA/MSFC Preliminary Design Office/Mission Analysis Team Abstract To send a piloted mission to Mars, transportation systems must be developed for the Earth to Orbit, trans Mars injection (TMI), capture into Mars orbit, Mars descent, surface stay, Mars ascent, trans Earth injection (TEI), and Earth return phases. This paper presents a brief overview of the transportation systems for the Human Mars Mission (HMM) only in the vicinity of Mars. This includes: capture into Mars orbit, Mars descent, surface stay, and Mars ascent. Development of feasible mission scenarios now is important for identification of critical technology areas that must be developed to support future human missions. Although there is no funded human Mars mission today, architecture studies are focusing on missions traveling to Mars between 2011 and the early 2020's. Introduction For several years engineers and scientists at NASA have been developing mission scenarios for sending humans to Mars and returning them safely to Earth. The HMM has evolved as analyses have been completed and updated. The design reference mission (DRM) :'2 describes the baseline mission architecture at a given time, it is not intended to be a final or recommended mission scenario. As development of the HMM continues, the DRM and various mission architecture options or design reference points (DRPs) are refined and updated. Several locations are included in the DRPs: Mars, the Moon, and asteroids. At this time, only the Mars DRP has been evaluated in any detail. -
Paper Session II-A - Energy Block of International Space Station "Alpha"
1995 (32nd) People and Technology - The Case The Space Congress® Proceedings For Space Apr 26th, 2:00 PM - 5:00 PM Paper Session II-A - Energy Block of International Space Station "Alpha" Anatoli I. Kiselev General Director Khrunichev, SRPSC Follow this and additional works at: https://commons.erau.edu/space-congress-proceedings Scholarly Commons Citation Kiselev, Anatoli I., "Paper Session II-A - Energy Block of International Space Station "Alpha"" (1995). The Space Congress® Proceedings. 28. https://commons.erau.edu/space-congress-proceedings/proceedings-1995-32nd/april-26-1995/28 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]. ENERGY BLOCK OF INTERNATIONAL SPACE STATION "ALPHA" Ana10Ji I.Kisclev - General Director K.hrunichcv SRPSC Anatoli i.Nedaivoda - General Designer Valdimir K.Karra.sk - Professor, Design Center Director The international space station "Alpha" consists of the American, Rus sian, European and Japanese segments. Its integration in the orbit will take place in November, 1997 starting from the injection of 20-tonn erergy block on the basis of the unified functional c.argo blade (russian abbr1.. "' iation as EFGB) by means of the "Proton" LY. The EFG B is designed by the KHRUNICHEV State Research and Production Space Center (KSRPSC) The orbit hight with the inclination of 51.6 deg for EFGB is so selected thett by the end of December, 1997 it can be decreased upto the hight (approx. -
GB-ASTRA 3B-Comsatbw-21Mai V
A BOOST FOR SPACE COMMUNICATIONS SATELLITES For its first launch of the year, Arianespace will orbit two communications satellites: ASTRA 3B for the Luxembourg-based operator SES ASTRA, and COMSATBw-2 for Astrium as part of a contract with the German Ministry of Defense. The choice of Arianespace by leading space communications operators and manufacturers is clear international recognition of the company’s excellence in launch services. Because of its reliability and availability, the Arianespace launch system continues to set the global standard. Ariane 5 is the only commercial satellite launcher now on the market capable of simultaneously launching two payloads. Over the last two decades, Arianespace and SES have developed an exceptional relationship. ASTRA 3B will be the 33rd satellite from the SES group (Euronext Paris and Luxembourg Bourse: SESG) to have chosen the European launcher. SES ASTRA operates the leading direct-to-home TV broadcast system in Europe, serving more than 125 million households via DTH and cable networks. ASTRA 3B was built by Astrium using a Eurostar E 3000 platform, and will weigh approximately 5,500 kg at launch. Fitted with 60 active Ku-band transponders and four Ka-band transponders, ASTRA 3B will be positioned at 23.5 degrees East. It will deliver high-power broadcast services across all of Europe, and offers a design life of 15 years. Astrium chose Arianespace for the launch of two military communications satellites, COMSATBw-1 and COMSATBw-2, as part of a satellite communications system supplied to the German Ministry of Defense. The first satellite in this family, COMSATBw-1, was launched by Arianespace in October 2009. -
Small Satellite Launchers
SMALL SATELLITE LAUNCHERS NewSpace Index 2020/04/20 Current status and time from development start to the first successful or planned orbital launch NEWSPACE.IM Northrop Grumman Pegasus 1990 Scorpius Space Launch Demi-Sprite ? Makeyev OKB Shtil 1998 Interorbital Systems NEPTUNE N1 ? SpaceX Falcon 1e 2008 Interstellar Technologies Zero 2021 MT Aerospace MTA, WARR, Daneo ? Rocket Lab Electron 2017 Nammo North Star 2020 CTA VLM 2020 Acrux Montenegro ? Frontier Astronautics ? ? Earth to Sky ? 2021 Zero 2 Infinity Bloostar ? CASIC / ExPace Kuaizhou-1A (Fei Tian 1) 2017 SpaceLS Prometheus-1 ? MISHAAL Aerospace M-OV ? CONAE Tronador II 2020 TLON Space Aventura I ? Rocketcrafters Intrepid-1 2020 ARCA Space Haas 2CA ? Aerojet Rocketdyne SPARK / Super Strypi 2015 Generation Orbit GoLauncher 2 ? PLD Space Miura 5 (Arion 2) 2021 Swiss Space Systems SOAR 2018 Heliaq ALV-2 ? Gilmour Space Eris-S 2021 Roketsan UFS 2023 Independence-X DNLV 2021 Beyond Earth ? ? Bagaveev Corporation Bagaveev ? Open Space Orbital Neutrino I ? LIA Aerospace Procyon 2026 JAXA SS-520-4 2017 Swedish Space Corporation Rainbow 2021 SpinLaunch ? 2022 Pipeline2Space ? ? Perigee Blue Whale 2020 Link Space New Line 1 2021 Lin Industrial Taymyr-1A ? Leaf Space Primo ? Firefly 2020 Exos Aerospace Jaguar ? Cubecab Cab-3A 2022 Celestia Aerospace Space Arrow CM ? bluShift Aerospace Red Dwarf 2022 Black Arrow Black Arrow 2 ? Tranquility Aerospace Devon Two ? Masterra Space MINSAT-2000 2021 LEO Launcher & Logistics ? ? ISRO SSLV (PSLV Light) 2020 Wagner Industries Konshu ? VSAT ? ? VALT -
NASA Expendable Launch Services Current Use of EELV
NASA Expendable Launch Services Current Use of EELV Lynn F. H. Cline Deputy Associate Administrator for Space Operations National Aeronautics and Space Administration June 17, 2009 Overview • NASA’s expendable launch vehicles are run by the Launch Services Program (LSP) consolidated at Kennedy Space Center in 1998 – LSP provides acquisition, technical management, mission integration and launch management • NASA utilizes a mixed fleet of vehicles (small, medium & intermediate) with varying levels of performance used to support a mix of mission sizes – Mainly for Science Mission Directorate payloads, but other NASA Directorates and other government agencies also use NASA launch services – Launches conducted from multiple ranges, including RTS, WFF, Kodiak • Vehicles are selected from the NASA Launch Services Contract (NLS) – Through competition based on mass, orbit, class of payload, and best value – Current NLS contract expires in 2010, RFP released to extend the contract • Most recent contract action purchased four intermediate class missions – TDRS – K & L, RBSP and MMS • Important issues – Loss of Medium Class launch service provider, which has been 50% of NASA missions historically – Compressed manifest – Possibility that NASA incurs a portion of the intermediate class infrastructure costs post 2010 NASA Launch Services Manifest FPB Approved 3/25/09 2009 2010 2011 2012 2013 2014 2015 2016 Release 6/03/09 Rev. 1 Q1 Q2 Q3 Q4 Q1 Q2 Q3 Q4 Q1 Q2 Q3 Q4 Q1 Q2 Q3 Q4 Q1 Q2 Q3 Q4 Q1 Q2 Q3 Q4 Q1 Q2 Q3 Q4 Q1 Q2 Q3 Q4 Small Class (SC) NuSTAR (P-XL) -
Space Shuttle Chronology Spacecalc
CBS News/Spaceflight Now STS Flight History by Launch Date 7/20/06 Space Shuttle Chronology SpaceCalc Space Shuttle DD HH MM SS Flights Notes Challenger 062 07 56 22 10 MET based on main gear Columbia 300 17 40 22 28 touchdown. Compiled from Discovery 268 15 29 30 32 news reports, NASA files. Atlantis 219 21 27 17 26 Endeavour 206 14 12 17 19 Compiled by William Harwood Program Total 1058 04 45 48 115 CBS News/Spaceflight Now OV # STS DD HH MM SS Launch Mission Description 102 N/A 01 00 00 00 00 02/28/81 Flight readiness firing 102 01 01 02 06 20 53 04/12/81 First shuttle flight 102 02 02 02 06 13 11 11/12/81 Fuel cell failure; MDM flight 102 03 03 08 00 04 46 03/22/82 White Sands, N.M., landing 102 04 04 07 01 09 31 06/27/82 Final shuttle test flight 102 05 05 05 02 14 26 11/11/82 1st STS satellites launched 99 N/A 06 00 00 00 00 12/18/82 Flight Readiness Firing 99 N/A 06 00 00 00 00 01/25/83 FRF-2 99 06 06 05 00 23 42 04/04/83 TDRS-1; 1st STS spacewalk 99 07 07 06 02 23 59 06/18/83 Three comsats 99 08 08 06 01 08 43 08/30/83 Insat, CFES 102 09 09 10 07 47 24 11/28/83 First Spacelab flight 99 10 41B 07 23 15 55 02/02/84 2 comsats lost; MMU EVA 99 11 41C 06 23 40 07 04/06/84 Solar Max repair; MMU EVA 103 N/A 41D 00 00 00 00 06/02/84 Flight readiness firing 103 N/A 41D 00 00 00 00 06/26/84 RSLS abort 103 12 41D 06 00 56 04 08/30/84 SBS, Syncom, Telstar 99 13 41G 08 05 23 38 10/05/84 ERBS; 1st female EVA 103 14 51A 07 23 44 56 11/07/84 Westar, Palapa retrieval 103 15 51C 03 01 33 23 01/24/85 DOD (Magnum?) 103 16 51D 06 23 55 23 04/12/85 -
Photographs Written Historical and Descriptive
CAPE CANAVERAL AIR FORCE STATION, MISSILE ASSEMBLY HAER FL-8-B BUILDING AE HAER FL-8-B (John F. Kennedy Space Center, Hanger AE) Cape Canaveral Brevard County Florida PHOTOGRAPHS WRITTEN HISTORICAL AND DESCRIPTIVE DATA HISTORIC AMERICAN ENGINEERING RECORD SOUTHEAST REGIONAL OFFICE National Park Service U.S. Department of the Interior 100 Alabama St. NW Atlanta, GA 30303 HISTORIC AMERICAN ENGINEERING RECORD CAPE CANAVERAL AIR FORCE STATION, MISSILE ASSEMBLY BUILDING AE (Hangar AE) HAER NO. FL-8-B Location: Hangar Road, Cape Canaveral Air Force Station (CCAFS), Industrial Area, Brevard County, Florida. USGS Cape Canaveral, Florida, Quadrangle. Universal Transverse Mercator Coordinates: E 540610 N 3151547, Zone 17, NAD 1983. Date of Construction: 1959 Present Owner: National Aeronautics and Space Administration (NASA) Present Use: Home to NASA’s Launch Services Program (LSP) and the Launch Vehicle Data Center (LVDC). The LVDC allows engineers to monitor telemetry data during unmanned rocket launches. Significance: Missile Assembly Building AE, commonly called Hangar AE, is nationally significant as the telemetry station for NASA KSC’s unmanned Expendable Launch Vehicle (ELV) program. Since 1961, the building has been the principal facility for monitoring telemetry communications data during ELV launches and until 1995 it processed scientifically significant ELV satellite payloads. Still in operation, Hangar AE is essential to the continuing mission and success of NASA’s unmanned rocket launch program at KSC. It is eligible for listing on the National Register of Historic Places (NRHP) under Criterion A in the area of Space Exploration as Kennedy Space Center’s (KSC) original Mission Control Center for its program of unmanned launch missions and under Criterion C as a contributing resource in the CCAFS Industrial Area Historic District. -
INVESTOR PRESENTATION JANUARY 2021 February 2, 2021
INVESTOR PRESENTATION JANUARY 2021 February 2, 2021 PROPRIETARY & CONFIDENTIAL – DO NOT REDISTRIBUTE DISCLAIMER AND FORWARD LOOKING STATEMENTS This presentation (this “Presentation”) was prepared for informational purposes only to assist interested parties in making their own evaluation of the proposed transaction (the “Transaction”) between Holicity Inc. (“HOL”, “we”, or “our”) and Astra Space, Inc. (“Astra”). By accepting this Presentation, each recipient agrees: (i) to maintain the confidentiality of all information that is contained in this Presentation and not already in the public domain; and (ii) to use this Presentation for the sole purpose of evaluating Astra. This Presentation is for strategic discussion purposes only and does not constitute an offer to purchase nor a solicitation of an offer to sell shares of HOL, Astra or any successor entity of the Transaction. This presentation is incomplete without reference to, and should be viewed solely in conjunction with, the oral briefing provided by HOL. This Presentation is not intended to form the basis of any investment decision by the recipient and does not constitute investment, tax or legal advice. No representation, express or implied, is or will be given by HOL, Astra or their respective affiliates and advisors as to the accuracy or completeness of the information contained herein, or any other written or oral information made available in the course of an evaluation of the Transaction. This Presentation and the oral briefing provided by HOL or Astra may contain certain “forward-looking statements” within the meaning of the Private Securities Litigation Reform Act of 1995, Section 27A of the Securities Act and Section 21E of the Securities Exchange Act of 1934, as amended, including statements regarding HOL’s, Astra’s on their management teams’ expectations, hopes, beliefs, intentions or strategies regarding the future. -
A Call for a New Human Missions Cost Model
A Call For A New Human Missions Cost Model NASA 2019 Cost and Schedule Analysis Symposium NASA Johnson Space Center, August 13-15, 2019 Joseph Hamaker, PhD Christian Smart, PhD Galorath Human Missions Cost Model Advocates Dr. Joseph Hamaker Dr. Christian Smart Director, NASA and DoD Programs Chief Scientist • Former Director for Cost Analytics • Founding Director of the Cost and Parametric Estimating for the Analysis Division at NASA U.S. Missile Defense Agency Headquarters • Oversaw development of the • Originator of NASA’s NAFCOM NASA/Air Force Cost Model cost model, the NASA QuickCost (NAFCOM) Model, the NASA Cost Analysis • Provides subject matter expertise to Data Requirement and the NASA NASA Headquarters, DARPA, and ONCE database Space Development Agency • Recognized expert on parametrics 2 Agenda Historical human space projects Why consider a new Human Missions Cost Model Database for a Human Missions Cost Model • NASA has over 50 years of Human Space Missions experience • NASA’s International Partners have accomplished additional projects . • There are around 70 projects that can provide cost and schedule data • This talk will explore how that data might be assembled to form the basis for a Human Missions Cost Model WHY A NEW HUMAN MISSIONS COST MODEL? NASA’s Artemis Program plans to Artemis needs cost and schedule land humans on the moon by 2024 estimates Lots of projects: Lunar Gateway, Existing tools have some Orion, landers, SLS, commercially applicability but it seems obvious provided elements (which we may (to us) that a dedicated HMCM is want to independently estimate) needed Some of these elements have And this can be done—all we ongoing cost trajectories (e.g. -
Exploring Space
EXPLORING SPACE: Opening New Frontiers Past, Present, and Future Space Launch Activities at Cape Canaveral Air Force Station and NASA’s John F. Kennedy Space Center EXPLORING SPACE: OPENING NEW FRONTIERS Dr. Al Koller COPYRIGHT © 2016, A. KOLLER, JR. All rights reserved. No part of this book may be reproduced without the written consent of the copyright holder Library of Congress Control Number: 2016917577 ISBN: 978-0-9668570-1-6 e3 Company Titusville, Florida http://www.e3company.com 0 TABLE OF CONTENTS Page Foreword …………………………………………………………………………2 Dedications …………………………………………………………………...…3 A Place of Canes and Reeds……………………………………………….…4 Cape Canaveral and The Eastern Range………………………………...…7 Early Missile Launches ...……………………………………………….....9-17 Explorer 1 – First Satellite …………………….……………………………...18 First Seven Astronauts ………………………………………………….……20 Mercury Program …………………………………………………….……23-27 Gemini Program ……………………………………………..….…………….28 Air Force Titan Program …………………………………………………..29-30 Apollo Program …………………………………………………………....31-35 Skylab Program ……………………………………………………………….35 Space Shuttle Program …………………………………………………..36-40 Evolved Expendable Launch Program ……………………………………..41 Constellation Program ………………………………………………………..42 International Space Station ………………………………...………………..42 Cape Canaveral Spaceport Today………………………..…………………43 ULA – Atlas V, Delta IV ………………………………………………………44 Boeing X-37B …………………………………………………………………45 SpaceX Falcon 1, Falcon 9, Dragon Capsule .………….........................46 Boeing CST-100 Starliner …………………………………………………...47 Sierra -
Spacewalk Database
Purchaser First Inscribed First ID Name Purchaser Last Name Name Inscribed Last Name Biographic_Infomation 01558 Beth / Forrest Goodwin Ron & Margo Borrup In 1957 CURTISS S. (ARMY) ARMSTRONG became a member of America's Space Team. His career began with the launch of Explorer I and Apollo programs. His tireless dedication has contributed to America's future. He is truly 00022 Cheryl Ann Armstrong Curtiss S. Armstrong an American Space Pioneer. Science teacher and aerospace educator since 00023 Thomas J. Sarko Thomas J. Sarko 1975. McDonnell Douglas 25 Years, AMF Board of 00024 Lowell Grissom Lowell Grissom Directors Joined KSC in 1962 in the Director's Protocol Office. Responsible for the meticulous details for the arrival, lodging, and banquets for Kings, Queens and other VIP worldwide and their comprehensive tours of KSC with top KSC 00025 Major Jay M. Viehman Jay Merle Viehman Personnel briefing at each poi WWII US Army Air Force 1st Lt. 1943-1946. US Civil Service 1946-1972 Engineer. US Army Ballistic Missile Launch Operations. Redstone, Jupiter, Pershing. 1st Satellite (US), Mercury 1st Flight Saturn, Lunar Landing. Retired 1972 from 00026 Robert F. Heiser Robert F. Heiser NASA John F. Kennedy S Involved in Air Force, NASA, National and Commercial Space Programs since 1959. Commander Air Force Space Division 1983 to 1986. Director Kennedy Space Center - 1986 to 1 Jan 1992. Vice President, Lockheed Martin 00027 Gen. Forrest S. McCartney Forrest S. McCartney Launch Operations. Involved in the operations of the first 41 manned missions. Twenty years with NASA. Ten years 00028 Paul C. Donnelly Paul C. -
Apollo Rocket Propulsion Development
REMEMBERING THE GIANTS APOLLO ROCKET PROPULSION DEVELOPMENT Editors: Steven C. Fisher Shamim A. Rahman John C. Stennis Space Center The NASA History Series National Aeronautics and Space Administration NASA History Division Office of External Relations Washington, DC December 2009 NASA SP-2009-4545 Library of Congress Cataloging-in-Publication Data Remembering the Giants: Apollo Rocket Propulsion Development / editors, Steven C. Fisher, Shamim A. Rahman. p. cm. -- (The NASA history series) Papers from a lecture series held April 25, 2006 at the John C. Stennis Space Center. Includes bibliographical references. 1. Saturn Project (U.S.)--Congresses. 2. Saturn launch vehicles--Congresses. 3. Project Apollo (U.S.)--Congresses. 4. Rocketry--Research--United States--History--20th century-- Congresses. I. Fisher, Steven C., 1949- II. Rahman, Shamim A., 1963- TL781.5.S3R46 2009 629.47’52--dc22 2009054178 Table of Contents Foreword ...............................................................................................................................7 Acknowledgments .................................................................................................................9 Welcome Remarks Richard Gilbrech ..........................................................................................................11 Steve Fisher ...................................................................................................................13 Chapter One - Robert Biggs, Rocketdyne - F-1 Saturn V First Stage Engine .......................15