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Appendix 1: Venus Missions
Appendix 1: Venus Missions Sputnik 7 (USSR) Launch 02/04/1961 First attempted Venus atmosphere craft; upper stage failed to leave Earth orbit Venera 1 (USSR) Launch 02/12/1961 First attempted flyby; contact lost en route Mariner 1 (US) Launch 07/22/1961 Attempted flyby; launch failure Sputnik 19 (USSR) Launch 08/25/1962 Attempted flyby, stranded in Earth orbit Mariner 2 (US) Launch 08/27/1962 First successful Venus flyby Sputnik 20 (USSR) Launch 09/01/1962 Attempted flyby, upper stage failure Sputnik 21 (USSR) Launch 09/12/1962 Attempted flyby, upper stage failure Cosmos 21 (USSR) Launch 11/11/1963 Possible Venera engineering test flight or attempted flyby Venera 1964A (USSR) Launch 02/19/1964 Attempted flyby, launch failure Venera 1964B (USSR) Launch 03/01/1964 Attempted flyby, launch failure Cosmos 27 (USSR) Launch 03/27/1964 Attempted flyby, upper stage failure Zond 1 (USSR) Launch 04/02/1964 Venus flyby, contact lost May 14; flyby July 14 Venera 2 (USSR) Launch 11/12/1965 Venus flyby, contact lost en route Venera 3 (USSR) Launch 11/16/1965 Venus lander, contact lost en route, first Venus impact March 1, 1966 Cosmos 96 (USSR) Launch 11/23/1965 Possible attempted landing, craft fragmented in Earth orbit Venera 1965A (USSR) Launch 11/23/1965 Flyby attempt (launch failure) Venera 4 (USSR) Launch 06/12/1967 Successful atmospheric probe, arrived at Venus 10/18/1967 Mariner 5 (US) Launch 06/14/1967 Successful flyby 10/19/1967 Cosmos 167 (USSR) Launch 06/17/1967 Attempted atmospheric probe, stranded in Earth orbit Venera 5 (USSR) Launch 01/05/1969 Returned atmospheric data for 53 min on 05/16/1969 M. -
Habitable Zone ? UE Zu Habitable Planeten Präsentation 1
Venus Habitable Zone ? UE zu Habitable Planeten Präsentation 1. Juni 2006 Eisenkölbl, Grohs, Hren, Lendl Venus 1. Raumsonden zur Venus Überblick • Raumfahrt zur Venus – Allgemeines – Beweggründe – Technische Hintergründe • Venus – Missionen – Zeittafel und Überblick – erfolgreiche Missionen – Zukünftige Missionen Raumfahrt zur Venus Allgemeines • Venus ist der meistbesuchte Planet in unserem Sonnensystem. (~ 25 erfolgreiche Missionen von 44) • Heutige Daten der Venus sind ein Ergebnis der zahlreichen Raummissionen Raumfahrt zur Venus Beweggründe • Dichte Wolkendecke – keine Beobachtungsmöglichkeit von der Erde aus im sichtbaren Licht • Vorstellung von Leben auf Venus • Suche nach habitabler Zone • Ressourcensuche Raumfahrt zur Venus technische Hintergründe • Venus ist der Planet mit der geringsten Entfernung von der Erde – Minimum 38.2 x 106 km – Maximum 261.0 x 106 km • Sonden leisten Pionierarbeit – Erprobung von Raumsonden • Technik • Material • Bauart Raumfahrt zur Venus – Zeittafel 1 (1961-1967) 1961 Sputnik 7 - 4 February 1961 - Attempted Venus Impact Venera 1 - 12 February 1961 - Venus Flyby (Contact Lost) 1962 Mariner 1 - 22 July 1962 - Attempted Venus Flyby (Launch Failure) Sputnik 19 - 25 August 1962 - Attempted Venus Flyby Mariner 2 - 27 August 1962 - Venus Flyby Sputnik 20 - 1 September 1962 - Attempted Venus Flyby Sputnik 21 - 12 September 1962 - Attempted Venus Flyby 1963 Cosmos 21 - 11 November 1963 - Attempted Venera Test Flight? 1964 Venera 1964A - 19 February 1964 - Attempted Venus Flyby (Launch Failure) Venera 1964B -
Dsc Pub Edited
1965 50) just 24 kilometers from its intended target Ranger 8 point in the equatorial region of the Sea of Nation: U.S. (21) Tranquillity—an area that Apollo mission Objective(s): lunar impact planners were particularly interested in Spacecraft: Ranger-C studying. Spacecraft Mass: 366.87 kg Mission Design and Management: NASA JPL 51) Launch Vehicle: Atlas-Agena B (no. 13 / Atlas “Atlas-Centaur 5” D no. 196 / Agena B no. 6006) Nation: U.S. (22) Launch Date and Time: 17 February 1965 / Objective(s): highly elliptical orbit 17:05:00 UT Spacecraft: SD-1 Launch Site: ETR / launch complex 12 Spacecraft Mass: 951 kg Scientific Instruments: Imaging system (six TV Mission Design and Management: NASA JPL cameras) Launch Vehicle: Atlas-Centaur (AC-5 / Atlas C Results: As successful as its predecessor, no. 156D / Centaur C) Ranger 8 returned 7,137 high-resolution pho- Launch Date and Time: 2 March 1965 / tographs of the lunar surface prior to its 13:25 UT scheduled impact at 09:57:37 UT on 20 Launch Site: ETR / launch complex 36A February. Unlike Ranger 7, however, Ranger 8 Scientific Instruments: none turned on its cameras about 8 minutes earlier Results: This mission was designed to rehearse a to return pictures with resolution comparable complete Centaur upper-stage burn in support to Earth-based telescopes (for calibration and of the Surveyor lunar lander program. On a comparison purposes). Controllers attempted nominal mission, the Centaur would boost its to align the cameras along the main velocity payload on a direct-ascent trajectory to the vector (to reduce imagine smear) but aban- Moon. -
Venus Exploration Themes
Venus Exploration Themes VEXAG Meeting #11 November 2013 VEXAG (Venus Exploration Analysis Group) is NASA’s community‐based forum that provides science and technical assessment of Venus exploration for the next few decades. VEXAG is chartered by NASA Headquarters Science Mission Directorate’s Planetary Science Division and reports its findings to both the Division and to the Planetary Science Subcommittee of NASA’s Advisory Council, which is open to all interested scientists and engineers, and regularly evaluates Venus exploration goals, objectives, and priorities on the basis of the widest possible community outreach. Front cover is a collage showing Venus at radar wavelength, the Magellan spacecraft, and artists’ concepts for a Venus Balloon, the Venus In‐Situ Explorer, and the Venus Mobile Explorer. (Collage prepared by Tibor Balint) Perspective view of Ishtar Terra, one of two main highland regions on Venus. The smaller of the two, Ishtar Terra, is located near the north pole and rises over 11 km above the mean surface level. Courtesy NASA/JPL–Caltech. VEXAG Charter. The Venus Exploration Analysis Group is NASA's community‐based forum designed to provide scientific input and technology development plans for planning and prioritizing the exploration of Venus over the next several decades. VEXAG is chartered by NASA's Solar System Exploration Division and reports its findings to NASA. Open to all interested scientists, VEXAG regularly evaluates Venus exploration goals, scientific objectives, investigations, and critical measurement requirements, including especially recommendations in the NRC Decadal Survey and the Solar System Exploration Strategic Roadmap. Venus Exploration Themes: November 2013 Prepared as an adjunct to the three VEXAG documents: Goals, Objectives and Investigations; Roadmap; as well as Technologies distributed at VEXAG Meeting #11 in November 2013. -
Venus Exploration Themes: September 2011
Venus Exploration Themes Adjunct to Venus Exploration Goals and Objectives 2011 September 2011 Fifty Years of Venus Missions Venus Exploration Vignettes Technologies for Venus Exploration Front cover is a collage showing Venus at radar wavelength, the Magellan spacecraft, and artists’ concepts for a Venus Balloon, the Venus In Situ Explorer, and the Venus Mobile Explorer. (Collage prepared by Tibor Balint) Perspective view of Ishtar Terra, one of two main highland regions on Venus. The smaller of the two, Ishtar Terra, is located near the north pole and rises over 11 km above the mean surface level. Courtesy NASA/JPL–Caltech. Venus Exploration Themes: September 2011 Prepared as an adjunct to the Venus Exploration Goals and Objectives document to preserve extracts from the October 2009 Venus Exploration Pathways document. TABLE OF CONTENTS Table of Contents ........................................................................................................................... iii Fifty Years of Venus Missions ....................................................................................................... 1 Venus Exploration Vignettes .......................................................................................................... 3 Vignette 1: Magellan ................................................................................................................... 3 Vignette 2: Experiencing Venus by Air: The Advantages of Balloon-Borne In Situ Exploration .............................................................................................................. -
Venus Exploration Goals, Objectives, Investigations, and Priorities: 2007
Venus Exploration Goals, Objectives, Investigations, and Priorities: 2007 A Report of the Venus Exploration Analysis Group (VEXAG) October 2007 VEXAG is NASA’s community-based forum, which provides science input for planning and prioritizing Venus exploration for the next few decades. VEXAG is chartered by NASA Headquarters Planetary Science Division and reports its findings to both the Division and to the Planetary Science Sub-Committee of the NASA Advisory Council. VEXAG, which is open to all interested scientists and engineers, regularly evaluates Venus exploration goals, objectives, investigations and priorities on the basis of the widest possible community outreach. http://www.lpi.usra.edu/vexag Front cover is a collage showing Venus at optical wavelength, the Magellan spacecraft, and artists’ concepts for a Venus Balloon, the Venus In-Situ Explorer, and the Venus Mobile Explorer. Venus Exploration Goals, Objectives, Investigations, and Priorities: 2007 VEXAG (Venus Exploration Analysis Group) October 2007 Prepared by the VEXAG (Venus Exploration Analysis Group) Organizing Committee: Janet Luhmann, VEXAG Co-Chair, University of California, Berkeley, California ([email protected]) Sushil Atreya, VEXAG Co-Chair, University of Michigan, Ann Arbor, Michigan ([email protected]) Steve Mackwell, Focus Group Lead for Planetary Formation and Evolution, Lunar and Planetary Institute, Houston, Texas ([email protected]) Kevin Baines, Focus Group Lead for Atmospheric Evolution, JPL, Pasadena, California ([email protected]) James Cutts, Focus Group Lead for Venus Exploration Technologies, JPL, Pasadena, California ([email protected]) Adriana Ocampo, Venus Program Executive, NASA Headquarters, Washington DC. ([email protected]) Other supporting members of the VEXAG Organizing Committee are: Tibor Balint, JPL; Mark Bullock, Southwest Research Institute, Boulder, Colorado; Larry Esposito, LASP, University of Colorado; Ellen Stofan, Proxemy, Inc.; Tommy Thompson, JPL. -
NASA News National Aeronautics and Space Administration Washington, D.C
NASA News National Aeronautics and Space Administration Washington, D.C. 20546 AC 202 755-8370 For Release THURSDAY July 27, 1978 Pr6SS Kit Project Pioneer Venus 2 RELEASE NO: 78-101 CNASA-Ne»s-Eelease-78-101) SECOND VENOS N78-28105 SPACECBAFT SET FOB LAUNCH {National Aeronautics and Space Administration) 120 p CSCL 22A CJnclas 00/1_2 27327 Contents V* i GENERAL RELEASE ^At^S^T. 1-6 MISSION PROFILE 7-24 Pioneer Venus Multiprobe Mission 13-24 THE PLANET VENUS 25-40 MAJOR QUESTIONS ABOUT VENUS 41-42 HISTORICAL DISCOVERIES ABOUT VENUS 43-45 EXPLORATION OF VENUS BY SPACECRAFT 46-47 THE PIONEER VENUS SPACECRAFT 48-62 The Orbiter Spacecraft 53-58 The Multiprobe Spacecraft 58-62 VENUS ATMOSPHERIC PROBES 63-76 The Large Probe 63-70 The Small Probe 70-76 11 SCIENTIFIC INVESTIGATIONS 77-97 Orbiter 77-85 Orbiter Radio Science 85-88 Large Probe Experiments 88-92 Large and Small Probe Instruments 92-93 Small Probe Experiments 94 Multiprobe Bus Experiment 94-95 Multiprobe Radio Science Experiments 95-96 PRINCIPAL INVESTIGATORS AND SCIENTIFIC INSTRUMENTS 97-100 LAUNCH VEHICLE 101-102 LAUNCH FLIGHT SEQUENCE 102 LAUNCH VEHICLE CHARACTERISTICS , . 103 ATLAS CENTAUR FLIGHT SEQUENCE (AC-50) 104 LAUNCH OPERATIONS 105 MISSION OPERATIONS 105-107 DATA RETURN, COMMAND AND TRACKING 108-111 PIONEER VENUS TEAM 112-114 CONTRACTORS 114-117 VENUS STATISTICS 118 NOTE TO EDITORS; This press kit covers the launch phase of the Pioneer Venus Multiprobe spacecraft and cruise phases of both the Pioneer Venus Orbiter and the Multiprobe spacecraft. Much of the material is also pertinent to the Venus encounter, but an updated press kit will be issued shortly before arrival at the planet in December 1978. -
ISU Team Project
Additional copies of the Project Report or the Executive Summary for this project may be ordered from the International Space University (ISU) Headquarters. The Executive Summary and the Project Report also can be found on the ISU website. International Space University Strasbourg Central Campus Attention: Publications Parc d’Innovation 1 rue Jean-Dominque Cassini 67400 Illkirch-Graffenstaden France Tel : +33 (0)3 88 65 54 30 Fax: +33(0) 88 65 54 47 http://www.isunet.edu Copyright 2003 by the International Space University All Rights Reserved TRACKS TO SPACE ACKNOWLEDGEMENTS The following individuals and organisations have generously contributed their time, resources, expertise and facilities to help us make TRACKS to Space possible. PROJECT SPONSOR European Space Agency — Industrial Matters and Technology Programmes Hans Kappler Director Marco Guglielmi Head of Technology Strategy Section Marco Freire Technology Strategy Engineer PROJECT FACULTY AND TA Project Initiator Walter Peeters Co-chair Nicolas Peter Co-chair Ray Williamson Teaching Associate Philippos Beveratos English Tutor Sarah Delaveaud English Tutor Carol Carnett EXTERNAL EXPERTS Andrew Aldrin Boeing, NASA Systems Randall Correll Science Applications International Corporation Dan Glover NASA Glenn Research Center Tetsuichi Ito NASDA, ISU Faculty Joan Johnson-Freese United States Naval War College Chiaki Mukai NASDA Astronaut Ichiro Nakatani Institute of Space and Astronautical Science (ISAS) Jean-Claude Piedboeuf Canadian Space Agency Roy Sach Director Defence Space, Australia Gongling Sun EurasSpace GmbH Simon P. Worden Brigadier General, United States Air Force PERSONAL THANKS The authors would like to extend a heartfelt thanks to those who made the greatest sacrifices during this two-month space odyssey. -
Low-Frequency Turbulence in the Anisotropic Plasma Namig Dzhalilov
Solar Wind: Low-frequency Turbulence in the Anisotropic Plasma Namig Dzhalilov Shamakhy Astrophysical Observatory, Azerbaijan 1 A g e n d a • Global structure of the heliosphere - general views • Solar wind measurements • The solar wind as a turbulence laboratory • MHD - Wave instability theory • Conclusions 2 3 The solar corona • Hot rarefied atmosphere above visible surface • Plasma beta <<1 in corona • magnetic field dominates • Closed magnetic field: plasma trapped • Open magnetic field: plasma can expand into interplanetary space 4 Eclipse: RED 1.1 106 K Iron X‐XI (RED) GREEN 2 106 K Iron XIII‐XIV (GREEN) This eclipse image shows the magnetic topology of the corona. 5 There is a clear separation of the high and low latitude solar wind. 6 This SOHO extreme ultraviolet (EIT) and scattered visible light (LASCO) composite image shows the outward streaming solar corona forming the supersonic solar wind 7 Expansion of the upper corona • Corona is very hot • Pressure is higher than ambient interstellar medium • Expands into interplanetary space (Parker, 1958): solar wind • Carves a cavity in interstellar medium: heliosphere • Nearly radial flow • Accelerates to full speed by ~20 solar radii SoHO coronagraph (LASCO) Artificial eclipse 8 9 What is the solar wind? • Collisionless, magnetised plasma • Continual, but variable, outflow from Sun’s corona • Blows a cavity in interstellar medium: heliosphere • Carries magnetic field, waves and turbulence from Sun’s corona • At edge of heliosphere, merges with interstellar medium • Interacts with -
Overview of Past Venus Missions and Potential Architectures for Future
S 6 th h o I n r t t e C r o n u a r t i s o e n a o l n P E l a Overview of Past Venus Missions x Overview of Past Venus Missions n t r e e t m a r e and Potential Architectures for Future Missions y E P n r o v b – architectures – issues – failures – i r e o n W m o e r n k t s s h T By o p e , c A h n t l Dr. Tibor S. Balint o Tibor S. Balint a l n o t g a i , Jet Propulsion Laboratory, California Institute of Technology e G s e Pasadena, CA o r g i a 0 6 / 2 2 1 0 - 2 0 2 8 Preliminary - For Discussion Purposes Only Page 1 Overview • Introduction S 6 th h o I n – Extreme environments & Science drivers r t t e C r o n u a r t i s o e n a • Typical Mission Architectures to Explore Venus o l n P E l a – Role of mission architectures x n t r e e t m – Mission elements & Architectures a r e y E P n r o v b i r e o n • Brief Overview of Venus Missions W m o e r n – Past missions k t s s h T o p – Present missions & Missions under development e , c A h n t l o – Future mission concepts a l n o t g a i , e G s e • The Good, the Bad, & the Future o r g i – Lessons learned from past missions a – Challenges for future missions 0 6 / 2 2 1 0 - 2 0 2 • Conclusions 8 Preliminary - For Discussion Purposes Only Page 2 Introduction A First Look at Venus S 6 th h o I n r t t e C r o n u a r t i s o e n a o l n P E l a x n t r e e t m a r e y E P n r o v b i r e o n W m o e r n k t s s h T o p e , c A h n t l o a l n o t g a i , e G s e o r g i a 0 6 / 2 2 1 0 - 2 0 2 8 Preliminary - For Discussion Purposes Only Page 3 Introduction Venus: World of Contrasts -
NI\SI\ National Aeronautics and Space Administration Washington, D.C
NI\SI\ National Aeronautics and Space Administration Washington, D.C. 20546 APR 13 \989 Reply to Attn of EL TO: A/Administrator FROM: E/Associate Administrator for Space Science and Applications SUBJECT: Magellan Prelaunch Mission Operations Report The single Magellan spacecraft will be launched from KSC on board Atlantis (STS-30) on April 28, 1989, at 2:24 p.m. EDT. The nominal launch period extends from April 28 to May 24; the overall launch period can be extended to as late as May 28 if certain compromises are made in the deployment constraints and Venus orbital insertion changes accepted. The daily launch window increases from 23 minutes the first day to 121 minutes on the 16th day and remains at 121 minutes through the remainder of the period. Following Shuttle insertion into a 296 km parking orbit inclined at 28.85 0 , the combined Magellan spacecraft/2-Stage IUS will be deployed from Atlantis on Rev 5 (6:17 hrs MET). Approximately one hour later, the IUS will ignite and inject the Magellan spacecraft onto an Earth-Venus transfer trajectory. Separation of the Magellan spacecraft from the depleted IUS will occur at 7:42 hrs MET. The Magellan spacecraft is powered by single degree-of-freedom sun-tracking solar panels. The spacecraft is 3-axis stabilized by reaction wheels using gyros and a star sensor for attitude reference. The spacecraft carries a large solid rocket motor for Venus Orbit Insertion (VOl). A small hydrazine system with thrusters ranging from O.9N to 445N provides Delta-V for trajectory correction maneuvers and certain attitude control functions. -
Beyond Earth a CHRONICLE of DEEP SPACE EXPLORATION, 1958–2016
Beyond Earth A CHRONICLE OF DEEP SPACE EXPLORATION, 1958–2016 Asif A. Siddiqi Beyond Earth A CHRONICLE OF DEEP SPACE EXPLORATION, 1958–2016 by Asif A. Siddiqi NATIONAL AERONAUTICS AND SPACE ADMINISTRATION Office of Communications NASA History Division Washington, DC 20546 NASA SP-2018-4041 Library of Congress Cataloging-in-Publication Data Names: Siddiqi, Asif A., 1966– author. | United States. NASA History Division, issuing body. | United States. NASA History Program Office, publisher. Title: Beyond Earth : a chronicle of deep space exploration, 1958–2016 / by Asif A. Siddiqi. Other titles: Deep space chronicle Description: Second edition. | Washington, DC : National Aeronautics and Space Administration, Office of Communications, NASA History Division, [2018] | Series: NASA SP ; 2018-4041 | Series: The NASA history series | Includes bibliographical references and index. Identifiers: LCCN 2017058675 (print) | LCCN 2017059404 (ebook) | ISBN 9781626830424 | ISBN 9781626830431 | ISBN 9781626830431?q(paperback) Subjects: LCSH: Space flight—History. | Planets—Exploration—History. Classification: LCC TL790 (ebook) | LCC TL790 .S53 2018 (print) | DDC 629.43/509—dc23 | SUDOC NAS 1.21:2018-4041 LC record available at https://lccn.loc.gov/2017058675 Original Cover Artwork provided by Ariel Waldman The artwork titled Spaceprob.es is a companion piece to the Web site that catalogs the active human-made machines that freckle our solar system. Each space probe’s silhouette has been paired with its distance from Earth via the Deep Space Network or its last known coordinates. This publication is available as a free download at http://www.nasa.gov/ebooks. ISBN 978-1-62683-043-1 90000 9 781626 830431 For my beloved father Dr.