The Orbital-Hub: Low Cost Platform for Human Spaceflight After ISS
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TINA Small Force-Controlled Robotic Arm for Exploration and Small Satellites
DLR.de/en TINA Small force-controlled robotic arm for exploration and small satellites Brief description The robotic arm TINA is a four-axis space demonstrator to investigate autonomous operations during exploration missions on Earth. Aims The aim of the research project is to demonstrate the technology needed for a small, force-controlled robotic arm for use in space. By selecting specific components, it is possible to use TINA in Parties involved microgravity conditions as well as on Earth. DLR Institute of Robotics and Mechatronics Applications Facts and figures - Exploration, rover - Degrees of freedom: up to 7 - Controller: hard real time - Small satellites - Size: up to 2 m long - Radiation hardness: - Weight: 1.6 kg per joint various levels possible - Data transmission: - Tools: different end effectors can be Spacewire selected - Data rate: 3kHz - Supply voltage: +20V to +70V @DLR_en DLR.de/en TINA Small force-controlled robotic arm for exploration and small satellites The design of TINA follows the ‘qualifiable’ philosophy of DEXHAND [1], which uses industrial-grade compo- nents with a similar performance to their space equivalents and follows the ECSS guidelines closely, or uses the industrial-grade versions of radiation-hardened electronic components. This philosophy ensures that the transition to a fully qualified design can be achieved with a minimum number of changes. It also provides an almost perfect version for thermal and EMI modelling. Another big advantage is the low price compared to the fully qualified, radiation-hardened version, which allows the construction of multiple test arms for grasp- ing, object handling and many other applications. Each joint is made up of a brushless DC motor in combination with a resolver for commutation and position sensing, a harmonic drive gearbox, a brake for safety reasons and a torque sensor to give TINA the ability to ‘feel’. -
ORION ORION a to Z APOGEE to Break the Frangible Joints and Separate the Fairings, Three Parachutes
National Aeronautics and Space Administration ORION www.nasa.gov ORION A to Z APOGEE to break the frangible joints and separate the fairings, three parachutes. The next two parachutes will then VAN ALLEN RADIATION BELTS The term apogee refers to the point in an elliptical exposing the spacecraft to space. LAS - LAUNCH ABORT SYSTEM deploy and open. Once the spacecraft slows to around The Van Allen Belts are belts of plasma trapped by orbit when a spacecraft is farthest from the Earth. Orion’s Launch Abort System (LAS) is designed to 100 mph, the three main parachutes will then deploy the Earth’s magnetic field that shield the surface of During Exploration Flight Test-1, Orion’s flight path will GUPPY propel the crew module away from an emergency on using three pilot parachutes and slow the spacecraft the Earth from much of the radiation in space. During take it to an apogee of 3,600 miles. Just how high is The Super Guppy is a special airplane capable of the launch pad or during initial takeoff, moving the to around 20 mph for splashdown in the Pacific Ocean. Exploration Flight Test-1, Orion will pass within the Van that? A commercial airliner flies about 8 miles above transporting up to 26 tons in its cargo compartment crew away from danger. Orion’s LAS has three new When fully deployed, the canopies of three main Allen Radiation Belts and will spend more time in the the Earth’s surface, so Orion’s flight is 450 times farther measuring 25 feet tall, 25 feet wide, and 111 feet long. -
SPACE RESEARCH in POLAND Report to COMMITTEE
SPACE RESEARCH IN POLAND Report to COMMITTEE ON SPACE RESEARCH (COSPAR) 2020 Space Research Centre Polish Academy of Sciences and The Committee on Space and Satellite Research PAS Report to COMMITTEE ON SPACE RESEARCH (COSPAR) ISBN 978-83-89439-04-8 First edition © Copyright by Space Research Centre Polish Academy of Sciences and The Committee on Space and Satellite Research PAS Warsaw, 2020 Editor: Iwona Stanisławska, Aneta Popowska Report to COSPAR 2020 1 SATELLITE GEODESY Space Research in Poland 3 1. SATELLITE GEODESY Compiled by Mariusz Figurski, Grzegorz Nykiel, Paweł Wielgosz, and Anna Krypiak-Gregorczyk Introduction This part of the Polish National Report concerns research on Satellite Geodesy performed in Poland from 2018 to 2020. The activity of the Polish institutions in the field of satellite geodesy and navigation are focused on the several main fields: • global and regional GPS and SLR measurements in the frame of International GNSS Service (IGS), International Laser Ranging Service (ILRS), International Earth Rotation and Reference Systems Service (IERS), European Reference Frame Permanent Network (EPN), • Polish geodetic permanent network – ASG-EUPOS, • modeling of ionosphere and troposphere, • practical utilization of satellite methods in local geodetic applications, • geodynamic study, • metrological control of Global Navigation Satellite System (GNSS) equipment, • use of gravimetric satellite missions, • application of GNSS in overland, maritime and air navigation, • multi-GNSS application in geodetic studies. Report -
SPACE EXPLORATION SYMPOSIUM (A3) Small Bodies Missions and Technologies (Part 1) (4A)
68th International Astronautical Congress 2017 Paper ID: 39010 oral SPACE EXPLORATION SYMPOSIUM (A3) Small Bodies Missions and Technologies (Part 1) (4A) Author: Dr. Aur´elieMoussi Centre National d'Etudes Spatiales (CNES), France, [email protected] Mrs. Laurence Lorda Centre National d'Etudes Spatiales (CNES), France, [email protected] Mr. Clement Dudal Centre National d'Etudes Spatiales (CNES), France, [email protected] Mrs. Celine Cenac Centre National d'Etudes Spatiales (CNES), France, [email protected] Mr. David Granena Centre National d'Etudes Spatiales (CNES), France, [email protected] Mr. Thierry Martin Centre National d'Etudes Spatiales (CNES), France, [email protected] Dr. Elisabet Canalias CNES, France, [email protected] Mrs. Muriel Deleuze Centre National d'Etudes Spatiales (CNES), France, [email protected] Dr. Tra Mi Ho DLR (German Aerospace Center), Germany, [email protected] Mr. Christian Ziach Deutsches Zentrum f¨urLuft- und Raumfahrt e.V. (DLR), Germany, [email protected] Dr. Stephan Ulamec Deutsches Zentrum f¨urLuft- und Raumfahrt e.V. (DLR), Germany, [email protected] Dr. Jens Biele Deutsches Zentrum f¨urLuft- und Raumfahrt e.V. (DLR), Germany, [email protected] Mrs. Caroline Lange Deutsches Zentrum f¨urLuft- und Raumfahrt e.V. (DLR), Germany, [email protected] Mr. Jan Thimo Grundmann DLR (German Aerospace Center), Germany, [email protected] Ms. Nawarat Termtanasombat Lule˚aTechnical University, Germany, [email protected] Mr. Christian Krause Deutsches Zentrum f¨urLuft- und Raumfahrt e.V. (DLR), Germany, [email protected] Mrs. Cinzia Fantinati Deutsches Zentrum f¨urLuft- und Raumfahrt e.V. -
Exomars Flush Air Data System: Experimental and Numerical
ExoMars Flush Air Data System: Experimental and Numerical Investigation Thorn Schleutker a and Ali Gülhan b DLR, German Aerospace Center, 51147 Cologne, Germany Bart Van Hove c and Özgür Karatekin d Royal Observatory of Belgium, 1180 Brussel, Belgium The atmospheric reconstruction based on a ush air data system requires knowl- edge of the surface pressure distribution, which depends on various factors such as the Mach number, angle of attack and aeroshell geometry of the entry vehicle. The purpose of this work is to provide this information for the post-ight analysis of the Entry, Descent and Landing Module of ExoMars 2016, called Schiaparelli. Because the ow around the capsule cannot be duplicated exactly in ground testing facilities, and to account for the uncertainties in physical modelling by numerical simulation, a hybrid approach is chosen for the study. First, the atmospheric entry is simulated experimentally and these experiments are then simulated numerically. The experimen- tal and numerical results are compared and discussed. The almost perfect agreement validates the numerical tool, which afterwards is applied to the analysis of the entry ight of Schiaparelli. A focus lies on the understanding of experimental uncertainties and on the impact of necessary numerical simplications. a Research Scientist, Supersonic and Hypersonic Technology Department, Institute of Aerodynamics and Flow Tech- nologies, Linder Höhe. b Head of Department and PI of the ExoMars 2016 instrumentation COMARS+, Supersonic and Hypersonic Tech- nologies Department, Institute of Aerodynamics and Flow Technology, Linder Höhe. c Assistant Researcher, Department of Reference Systems and Planetology, Ringlaan 3. d Senior Scientist, Department of Reference Systems and Planetology, Ringlaan 3. -
The Space Race Continues
The Space Race Continues The Evolution of Space Tourism from Novelty to Opportunity Matthew D. Melville, Vice President Shira Amrany, Consulting and Valuation Analyst HVS GLOBAL HOSPITALITY SERVICES 369 Willis Avenue Mineola, NY 11501 USA Tel: +1 516 248-8828 Fax: +1 516 742-3059 June 2009 NORTH AMERICA - Atlanta | Boston | Boulder | Chicago | Dallas | Denver | Mexico City | Miami | New York | Newport, RI | San Francisco | Toronto | Vancouver | Washington, D.C. | EUROPE - Athens | London | Madrid | Moscow | ASIA - 1 Beijing | Hong Kong | Mumbai | New Delhi | Shanghai | Singapore | SOUTH AMERICA - Buenos Aires | São Paulo | MIDDLE EAST - Dubai HVS Global Hospitality Services The Space Race Continues At a space business forum in June 2008, Dr. George C. Nield, Associate Administrator for Commercial Space Transportation at the Federal Aviation Administration (FAA), addressed the future of commercial space travel: “There is tangible work underway by a number of companies aiming for space, partly because of their dreams, but primarily because they are confident it can be done by the private sector and it can be done at a profit.” Indeed, private companies and entrepreneurs are currently aiming to make this dream a reality. While the current economic downturn will likely slow industry progress, space tourism, currently in its infancy, is poised to become a significant part of the hospitality industry. Unlike the space race of the 1950s and 1960s between the United States and the former Soviet Union, the current rivalry is not defined on a national level, but by a collection of first-mover entrepreneurs that are working to define the industry and position it for long- term profitability. -
Sentinel-1A – Start of a New Era in Earth Observation
Sentinel-1A – start of a new era in Earth observation 03 April 2014 Mapping flood events, observing oil slicks in the oceans, detecting ice distribution in the sea and measuring ground movements with millimetric precision – just some of the tasks of Sentinel-1A, the new flagship in European Earth observation. The roughly 2.3-ton, four-metre-high, two-and- a-half-metre-wide satellite was launched from the European Spaceport in French Guiana at 23:02 CEST (18:02 local time) on 3 April 2014. The launch of Sentinel-1A also marks the start of the European Union (EU) and European Space Agency (ESA) Earth observation programme called Copernicus. The DLR Space Administration is financing one third of the ESA element of the programme with funds provided by the German Federal Government. The satellite will undergo a three-month-long commissioning phase before making its first routine data delivery in mid-year. "The radar system on the new European Earth observation satellite is one of the most powerful ever used in Earth orbit for civilian purposes. Using this instrument, which was developed and built in Germany on the basis of decades of experience, Sentinel-1A will be able to observe land and water surfaces day and night, regardless of the weather conditions. This is the start of a new era in remote sensing – consistent data collection is essential for the scientific analysis of global change," emphasised Johann-Dietrich Wörner, Chairman of the DLR Executive Board. Flying over every point on Earth in 12 days "With the launch of Sentinel-1A, Copernicus, the Earth observation programme of the European Union and the European Space Agency has begun. -
Rex D. Hall and David J. Shayler
Rex D. Hall and David J. Shayler Soyuz A Universal Spacecraft ruuiiMicPublishedu 11in1 aaaundiiuiassociationi witwimh ^^ • Springer Praxis Publishing PRHB Chichester, UK "^UF Table of contents Foreword xvii Authors' preface xix Acknowledgements xxi List of illustrations and tables xxiii Prologue xxix ORIGINS 1 Soviet manned spaceflight after Vostok 1 Design requirements 1 Sever and the 1L: the genesis of Soyuz 3 The Vostok 7/1L Soyuz Complex 4 The mission sequence of the early Soyuz Complex 6 The Soyuz 7K complex 7 Soyuz 7K (Soyuz A) design features 8 The American General Electric concept 10 Soyuz 9K and Soyuz 1 IK 11 The Soyuz Complex mission profile 12 Contracts, funding and schedules 13 Soyuz to the Moon 14 A redirection for Soyuz 14 The N1/L3 lunar landing mission profile 15 Exploring the potential of Soyuz 16 Soyuz 7K-P: a piloted anti-satellite interceptor 16 Soyuz 7K-R: a piloted reconnaissance space station 17 Soyuz VI: the military research spacecraft Zvezda 18 Adapting Soyuz for lunar missions 20 Spacecraft design changes 21 Crewing for circumlunar missions 22 The Zond missions 23 The end of the Soviet lunar programme 33 The lunar orbit module (7K-LOK) 33 viii Table of contents A change of direction 35 References 35 MISSION HARDWARE AND SUPPORT 39 Hardware and systems 39 Crew positions 40 The spacecraft 41 The Propulsion Module (PM) 41 The Descent Module (DM) 41 The Orbital Module (OM) 44 Pyrotechnic devices 45 Spacecraft sub-systems 46 Rendezvous, docking and transfer 47 Electrical power 53 Thermal control 54 Life support 54 -
Dr. Thomas Krueger European Space Agency (ESA), the Netherlands, [email protected]
Paper ID: 58165 IAC CyberSpace Edition 2020 oral IAF SPACE SYSTEMS SYMPOSIUM (D1) Cooperative and Robotic Space Systems (6) Author: Dr. Thomas Krueger European Space Agency (ESA), The Netherlands, [email protected] Mr. Edmundo Ferreira European Space Agency (ESA), The Netherlands, [email protected] Mr. Andrei Gherghescu ESA - European Space Agency, The Netherlands, [email protected] Mr. Lukas Hann ESA - European Space Agency, The Netherlands, [email protected] Mr. Emiel den Exter ESA - European Space Agency, The Netherlands, [email protected] Mr. Frank van der Hulst ESA - European Space Agency, The Netherlands, [email protected] Mr. Levin Gerdes European Space Agency (ESA), The Netherlands, [email protected] Mr. Leonardo Cencetti ESA - European Space Agency, The Netherlands, [email protected] Dr. Aaron Pereira DLR (German Aerospace Center), Germany, [email protected] Dr. Harsimran Singh DLR (German Aerospace Center), Germany, [email protected] Mr. Michael Panzirsch German Aerospace Center (DLR), Germany, [email protected] Dr. Thomas Hulin DLR (German Aerospace Center), Germany, [email protected] Mr. Ribin Balachandran German Aerospace Center (DLR), Germany, [email protected] Dr. Bernhard Weber German Aerospace Center (DLR), Germany, [email protected] Dr. Neal Lii German Aerospace Center (DLR), Germany, [email protected] DESIGNING AND TESTING A ROBOTIC AVATAR FOR SPACE-TO-GROUND TELEOPERATION: THE DEVELOPERS' INSIGHTS Abstract In late 2019 astronaut Luca Parmitano remotely controlled a rover equipped with a robotic manip- ulator, performing geology tasks on a moon-analog site from the ISS. 7 months later, in July 2020, he controls the same rover in a more realistic moon-analog environment: a field of volcanic rock and regolith on mount Etna, Italy. -
Space Rescue Ensuring the Safety of Manned Space¯Ight David J
Space Rescue Ensuring the Safety of Manned Space¯ight David J. Shayler Space Rescue Ensuring the Safety of Manned Spaceflight Published in association with Praxis Publishing Chichester, UK David J. Shayler Astronautical Historian Astro Info Service Halesowen West Midlands UK Front cover illustrations: (Main image) Early artist's impression of the land recovery of the Crew Exploration Vehicle. (Inset) Artist's impression of a launch abort test for the CEV under the Constellation Program. Back cover illustrations: (Left) Airborne drop test of a Crew Rescue Vehicle proposed for ISS. (Center) Water egress training for Shuttle astronauts. (Right) Beach abort test of a Launch Escape System. SPRINGER±PRAXIS BOOKS IN SPACE EXPLORATION SUBJECT ADVISORY EDITOR: John Mason, B.Sc., M.Sc., Ph.D. ISBN 978-0-387-69905-9 Springer Berlin Heidelberg New York Springer is part of Springer-Science + Business Media (springer.com) Library of Congress Control Number: 2008934752 Apart from any fair dealing for the purposes of research or private study, or criticism or review, as permitted under the Copyright, Designs and Patents Act 1988, this publication may only be reproduced, stored or transmitted, in any form or by any means, with the prior permission in writing of the publishers, or in the case of reprographic reproduction in accordance with the terms of licences issued by the Copyright Licensing Agency. Enquiries concerning reproduction outside those terms should be sent to the publishers. # Praxis Publishing Ltd, Chichester, UK, 2009 Printed in Germany The use of general descriptive names, registered names, trademarks, etc. in this publication does not imply, even in the absence of a speci®c statement, that such names are exempt from the relevant protective laws and regulations and therefore free for general use. -
Deployable Modular Frame for Inflatable Space Habitats
70th International Astronautical Congress (IAC), Washington D.C., United States, 21-25 October 2019. Copyright ©2019 by the International Astronautical Federation (IAF). All rights reserved. IAC-19,B3,8-GTS.2,4,x48931 DMF: Deployable Modular Frame for Inflatable Space Habitats Vittorio Netti1, * 1University of Houston, [email protected] *Corresponding author Abstract Inflatable Space Modules for space exploration are now a reality. In 2016, Bigelow Aerospace tested the first inflatable module Bigelow Expandable Activity Module (BEAM) on the International Space Station (ISS), achieving success. This technology has higher volume limits than other launchers, substantially changing the previous concepts of construction and life in space. Nevertheless, inflatable modules technology lacks a reliable and functional platform to efficiently use all this space. Due to its limited dimension, the International Standard Payload Rack (ISPR), currently used on ISS, is not suitable for this purpose. The project aims at developing a new standard for payload rack in the inflatable space modules: the Deployable Modular Frame (DMF). The DMF expands itself radially from the center of the module, starting from four structural pylons. It creates a solid infrastructure allowing for the configuration of a variety of spaces, including storage space, laboratories, workstations and living quarters. The DMF consists of two main parts: the Deployable Frame (DF) and the Modular Rack (MR). Once the frame is deployed, it provides four linear slots suitable to install the modular racks. The rack is the basic element that allows for the storage of equipment inside the frame. Once they are installed, the racks can slide on the frame’s rails, dynamically changing the space inside the module. -
The New American Space Age: a Progress Report on Human Spaceflight the New American Space Age: a Progress Report on Human Spaceflight the International Space
The New American Space Age: A PROGRESS REPORT ON HUMAN SpaCEFLIGHT The New American Space Age: A Progress Report on Human Spaceflight The International Space Station: the largest international scientific and engineering achievement in human history. The New American Space Age: A Progress Report on Human Spaceflight Lately, it seems the public cannot get enough of space! The recent hit movie “Gravity” not only won 7 Academy Awards – it was a runaway box office success, no doubt inspiring young future scientists, engineers and mathematicians just as “2001: A Space Odyssey” did more than 40 years ago. “Cosmos,” a PBS series on the origins of the universe from the 1980s, has been updated to include the latest discoveries – and funded by a major television network in primetime. And let’s not forget the terrific online videos of science experiments from former International Space Station Commander Chris Hadfield that were viewed by millions of people online. Clearly, the American public is eager to carry the torch of space exploration again. Thankfully, NASA and the space industry are building a host of new vehicles that will do just that. American industry is hard at work developing new commercial transportation services to suborbital altitudes and even low Earth orbit. NASA and the space industry are also building vehicles to take astronauts beyond low Earth orbit for the first time since the Apollo program. Meanwhile, in the U.S. National Lab on the space station, unprecedented research in zero-g is paving the way for Earth breakthroughs in genetics, gerontology, new vaccines and much more.