Venus Express Ground Segment and Mission Operations Venus Express

Total Page:16

File Type:pdf, Size:1020Kb

Venus Express Ground Segment and Mission Operations Venus Express Venuse Expresse n s s u s E x p r GrG oundo u r n d Segmente and g m e n t a n d Mission Operations Manfred Warhaut & Andrea Accomazzo ESA Directorate of Operations and Infrastructure, ESOC, Darmstadt, Germany SOC was responsible for developing the ground-segment facilities for both the ERosetta and Mars Express interplanetary missions. The high degree of commonality between those spacecraft and Venus Express, the twin spacecraft of Mars Express, has allowed large-scale re-use of ground-segment elements and the replication of the operations concepts for those spacecraft, resulting in significant cost and risk reductions. Operations Ground Segment Systems/Facilities The Venus Express Ground Segment provides the capabilities for monitoring and controlling the spacecraft and payload during all phases of the mission, as well as for the reception, archiving and distribution of the data gathered by the payload instruments. It therefore consists of (see figure): – a Ground Station and Communications Network – a Mission Operations Centre, and – a Science Operations Centre. The Ground Station and Communica- tions Network These elements are responsible for performing the telemetry, telecommand and tracking operations for Venus Express, using The Venus Express Ground Segment S/X-band frequencies. Tele-commands and telemetry are sent in either the S- or X- bands, with the possibility to transmit data-processing tasks essential for consolidated onward submittal to the simultaneously in both frequency bands, controlling the mission, as well as Mission Operations Centre (VMOC). The only one of which will be modulated. The S- spacecraft performance evaluation VSOC, which will be co-located with the band up/downlink is used only during the • the Data Disposition System, supporting VMOC during critical mission phases, will Launch and Early Operations Phase the acquisition and interim storage of make pre-processed scientific data and the (LEOP), in support of the Radio Science raw scientific data, to be accessible scientific data archive available to the Instrument (VeRa) campaigns, and in case together with raw housekeeping and scientific community through its Data of an emergency. The ground station used auxiliary data from the instrument Handling and Archive Service (DHAS). throughout all mission phases will be the Principal Investigators at remote The existing ESA/ESOC ground- new ESA 35 metre installation at Cebreros, locations, and to provide for production segment elements and facilities available near Madrid (Spain) (see accompanying of all data on a raw data medium for through the Rosetta and Mars Express article), complemented by the ESA New archiving purposes missions have been reused to the Norcia 35 metre station in Western Australia • the Mission Planning System, maximum extent possible, both in terms of to support the Venus Orbit Insertion and supporting command request handling hardware and software, for Venus Express. VeRa campaigns, and the Kourou 15 metre and the planning and scheduling of station during the LEOP. NASA DSN spacecraft/payload operations Flight Operations Concepts and Principles tracking support is provided as a back-up. • the Flight Dynamics System, supporting The Mission Operations Department at The Communications Network also all activities related to attitude and ESOC is responsible for the Venus Express provides the support services needed for orbit determination and prediction, mission operations preparation, planning accessing test data obtained during the preparation of slew and orbit and execution. All Venus Express spacecraft’s integration and test programme, manoeuvres, spacecraft dynamics Operations will be conducted by ESOC for the submittal of command requests to the evaluation and navigation in general according to procedures laid down in the ESOC/VMOC, for the retrieval of quick- • the Spacecraft Simulator, to support Venus Express Flight Operations Plan, a look mission products kept at ESOC, and procedure validation, operator training comprehensive document prepared by the also for supporting the electronic exchange and the simulation campaign before ESOC Venus Express Flight Control Team of scientifically processed data if required. each major phase of the mission (LEOP, based on Project/Industry deliverables VOI, etc.). (User Manual and Database), the Science The Mission Operations Centre Operations Plan, and Agreements with the The Venus Express Mission Operations The Science Operations Centre Principal Investigators. Centre (VMOC) located at ESOC in The Venus Express Science Operations Spacecraft operations during all active Darmstadt (Germany), includes: Centre (VSOC) supports the scientific mission phases – lasting about 2 years in • the Mission Control System, to support, mission planning and experiment total, with a possible extension of 1.5 years with both hardware and software, the command request preparation for – will be carried out following an 'off-line' 36 esa bulletin 124 - november 2005 www.esa.int Venus Express Ground Segment The Venus Express Mission Control Room at ESOC during the Launch and Early Operations Phase (LEOP) approach, with all activities being pre- Express Mission Operations Centre at spacecraft, with the primary responsibility planned and the appropiate telecommands ESOC and the spacecraft will not be for developing the payload operations being uplinked to the spacecraft for time- continuous and the periods of contact will strategy for the scientific mission resting tagged execution (via the onboard mission be primarily used for the pre-programming with the Venus Express Science Working timeline). The evaluation of telemetry data of autonomous operations functions on the Team (SWT). will also mainly take place off-line, with spacecraft, and for data collection for the possibility of quasi-real-time subsequent offline status assessment. The Mission Products intervention restricted to certain critical downlink will normally be configured such The mission products made available to the phases and cases of major contingencies. that most of the bandwidth is dedicated to Principal Investigators will include all There will be several communication- the dumping of onboard stored telemetry, spacecraft and experiment telemetry data blackout periods of up to two weeks with limited housekeeping and/or event and auxiliary data. Under nominal duration during the mission, due to the telemetry transmitted in real-time during conditions, all data acquired will be spacecraft-Earth-Sun geometry preventing the passes according to spacecraft available at the VMOC in engineering radio-frequency signal transmission. The monitoring requirements. format just 1 minute after their reception at round-trip communication time between the The Institutes who have developed the the ground station. r ground and the spacecraft will be up to scientific instruments are responsible for 30 minutes. Contact between the Venus defining their operation onboard the www.esa.int esa bulletin 124 - november 2005 37.
Recommended publications
  • Analysis of Narrow-Line Laser Cooling and Trapping of Sr Atoms in Microgravity Environments
    applied sciences Article Analysis of Narrow-Line Laser Cooling and Trapping of Sr Atoms in Microgravity Environments Jie Ren 1,2, Hui Liu 3,* , Xiaotong Lu 1,2 and Hong Chang 1,2,* 1 CAS Key Laboratory of Time and Frequency Primary Standards, National Time Service Center, Xi’an 710600, China; [email protected] (J.R.); [email protected] (X.L.) 2 School of Astronomy and Space Science, University of Chinese Academy of Sciences, Beijing 100049, China 3 State Key Laboratory of Photoelectric Technology and Functional Materials, International Collaborative Center on Photoelectric Technology and Nano Functional Materials, Institute of Photonics & Photon-Technology, Northwest University, Xi’an 710069, China * Correspondence: [email protected] (H.L.); [email protected] (H.C.) Received: 7 June 2020; Accepted: 15 July 2020; Published: 17 July 2020 Abstract: Obtaining ultracold alkaline earth(-like) atoms in space encounters the problem of performing narrow-line laser cooling in microgravity environments (µ-gEs). This paper reports an analysis of the magneto-optical trap (MOT) based on the narrow-line transition in 88Sr, while paying special attention to the role of the gravity. This analysis suggests the MOTs based on narrow-line transitions cannot be cold and dense enough in a µ-gE. We thus propose a strategy: that one can use a dual-frequency MOT to realize a low-temperature, high density, and high transfer efficiency, narrow-line red MOT in µ-gEs. Keywords: lasering cooling and trapping; microgravity; Monte Carlo simulation; optical lattice clocks; in space 1. Introduction Great efforts have been made in recent decades to push cold atoms into microgravity environments [1].
    [Show full text]
  • 7. Operations
    7. Operations 7.1 Ground Operations The Exploration Systems Architecture Study (ESAS) team addressed the launch site integra- tion of the exploration systems. The team was fortunate to draw on expertise from members with historical and contemporary human space flight program experience including the Mercury, Gemini, Apollo, Skylab, Apollo Soyuz Test Project, Shuttle, and International Space Station (ISS) programs, as well as from members with ground operations experience reaching back to the Redstone, Jupiter, Pershing, and Titan launch vehicle programs. The team had a wealth of experience in both management and technical responsibilities and was able to draw on recent ground system concepts and other engineering products from the Orbital Space Plane (OSP) and Space Launch Initiative (SLI) programs, diverse X-vehicle projects, and leadership in NASA/Industry/Academia groups such as the Space Propulsion Synergy Team (SPST) and the Advanced Spaceport Technology Working Group (ASTWG). 7.1.1 Ground Operations Summary The physical and functional integration of the proposed exploration architecture elements will occur at the primary launch site at the NASA Kennedy Space Center (KSC). In order to support the ESAS recommendation of the use of a Shuttle-derived Cargo Launch Vehicle (CaLV) and a separate Crew Launch Vehicle (CLV) for lunar missions and the use of a CLV for ISS missions, KSC’s Launch Complex 39 facilities and ground equipment were selected for conversion. Ground-up replacement of the pads, assembly, refurbishment, and/or process- ing facilities was determined to be too costly and time-consuming to design, build, outfit, activate, and certify in a timely manner to support initial test flights leading to an operational CEV/CLV system by 2011.
    [Show full text]
  • Future Military Space from Procurement to the Tactical Fight
    MONOGRAPH Future Military Space From Procurement to the Tactical Fight MAJ JUSTIN H. DEIFEL, USAF MAJ NICHOLAS M. SOMERMAN, USAF MAJ MARK D. THIEME, USA General Issue Current space acquisition, vehicle processing, and operations are too cumber- some and expensive to meet future emerging war fighter needs. The cost associ- ated with placing assets into orbit has been the greatest problem to the United States (US) fully recognizing its potential in space. With the emergence of com- mercially available reusable launch vehicles, the military must consider the pos- sibility of building an internal space lift capability as a core competency. Also, the military must develop and integrate new capabilities from space that will enable strategic capabilities, down to tactical war fighter implementation. Launch costs currently represent a third to half the cost of fielding a space system.1 Additionally, the current bureaucratic model for the Department of De- fense (DOD) space architecture does not enable a rapid approach to space for the US to gain space supremacy and prevent further loss of space superiority. Key hurdles must be removed and new methods utilized to accomplish this goal. This process requires a change in acquisitions, operations, doctrine, and organizational structure. Requirements for space systems are developed on a five to ten-year time hori- zon, which does not allow the development of systems that can be utilized on demand in an area of responsibility (AOR). New systems must be developed that can be deployed on demand to AORs and utilized by ground, sea, air, cyber, and space forces. Problem Statement Space access and capabilities are rapidly evolving, and the US military must pos- ture itself to utilize these capabilities to protect and defend US national security.
    [Show full text]
  • Building a Global Launch Network: Extending the Reach of Dedicated Small Satellite Launch Using New, Data-Driven Spaceport Assessment Tools
    SSC20-VIII-07 Building a Global Launch Network: Extending the Reach of Dedicated Small Satellite Launch Using New, Data-Driven Spaceport Assessment Tools John Fuller, Ren Liao, Kirit Patel, Sirisha Bandla, Monica Jan Virgin Orbit 4022 E Conant Street, Long Beach, CA 90808, United States [email protected] Wade McElroy, Mandy Vaughn VOX Space 840 Apollo St, Suite 100, El Segundo, CA 90245, United States [email protected] ABSTRACT The proliferation and sustained growth of small satellite architecture solutions, once an uncertain aspect of tomorrow’s space industry, are now largely perceived as a firm reality. Recent trends continue to show an increasing fraction of launch industry revenue being captured by small and dedicated launch vehicles, such as Virgin Orbit’s LauncherOne. Concurrently, another indicator of small satellite proliferation are recent announcements of increased rideshare opportunities by large launch vehicle operators. As numerous dedicated and rideshare launches emerge as solutions for small satellite customers, understanding the relative advantages and performance of these vehicles will be crucial to satisfy not only single launch, but broader architectural mission needs. Virgin Orbit and VOX Space have presented how a responsive air-launched architecture with multiple hosting spaceports and modularized systems at each can be leveraged to launch entire constellations within days. We have since continued to grow our spaceport network to support domestic and international mission planners that desire a launch vehicle that isn’t constrained to a permanent fixed site or departure corridor. Building upon that work, new analytical methods to analyze and communicate the advantages of air-launch from spaceports around the globe have been devised.
    [Show full text]
  • Introducing the New Generation of Chinese Geostationary Weather Satellites, Fengyun-4
    INTRODUCING THE NEW GENERATION OF CHINESE GEOSTATIONARY WEATHER SATELLITES, FENGYUN-4 JUN YANG, ZHIQING ZHANG, CAIYING WEI, FENG LU, AND QIANG GUO Fengyun-4 is the new generation of Chinese geostationary meteorological satellites with greatly enhanced capabilities for high-impact weather event monitoring, warning, and forecasting. n 7 September 1988, the Long March rocket FY-2 satellites carry the Visible and Infrared Spin Scan carried the Fengyun-1A (FY-1A) polar-orbiting Radiometer (VISSR) capable of imagery in five spectral O satellite into orbit, marking the start of the bands. Derived products include atmospheric motion Chinese Fengyun (FY; meaning wind and cloud in vectors (AMVs), sea surface temperatures (SSTs), total Chinese) meteorological satellite observing systems pro- precipitable water vapor (TPW), quantitative precipi- gram. On 10 June 1997, the FY-2A geostationary satellite tation estimations (QPEs), fire locations and intensity, was successfully launched and the Chinese meteorologi- surface albedo, and several others. cal satellite program took a large step toward its goal The FY-4 introduces a new generation of Chinese of establishing both polar-orbiting and geostationary geostationary meteorological satellites, with the first observational systems. Over time the Fengyun satellites have become increasingly important for protecting lives and property from natural disasters in China. TABLE 1. FY-2D/FY-2E overlap region observation The Chinese FY satellites are launched as a series. schedule. Full-disc and north-disc observations The odd numbers denote the polar-orbiting satellite are abbreviated as F and N, respectively. series, and the even numbers denote the geostationary Time (UTC) Region Satellite satellite series. After launch, a letter is appended to 0000 F FY-2E indicate the order in the satellite series; for instance, 0015 F FY-2D FY-2F is the sixth satellite that has been launched 0030 N FY-2E in the first generation of the Chinese geostationary 0045 N FY-2D satellites (FY-2).
    [Show full text]
  • Satellite Ground Segment
    Satellite Ground Segment: Moving to the Cloud January 2021 1 NSR- Satellite Ground Segment: Moving to the Cloud Introduction: A Foundational Shift The satellite industry is poised at the convergence of multiple trends from the wider ICT ecosystem. Taking cues from its influence as an enabling technology in other industries, only in recent years has Cloud Computing emerged as influential in the satellite world - in the context of efficient and automated delivery of business value to satellite customers, whether in Earth Observation or Communications. Much activity has focused on the “space” segment, ranging from investments and announcements related to new technology such as non-GEO HTS constellations, software defined radio, network function virtualization, and flat panel antennas, amongst others. Here the Cloud is largely seen as the foundational layer for the industry to morph into a complex arena for flexibly dynamic networks that are interoperable across layers and applications. In comparison, the “ground” segment in the industry is just beginning to ramp up, with relatively slower developments, in part due to the siloed nature of advancements at a components and sub-systems level. It is only now that the wider Big Data industry recognizes a market gap in the satellite value chain, one that it is well positioned to address. At the same time, traditional satellite companies realize the critical role that Cloud Computing will play in ensuring their businesses remain competitive. The Earth Observation market is continuously evolving, driven by downstream non-data segments. With a lower barrier to entry, new-space EO players are open to adopting alternative solutions such as on-board processing, optical satcom, and more importantly, virtualized ground stations and Cloud- based systems.
    [Show full text]
  • NASA's Space Network Ground Segment Sustainment Project
    NASA’s Space Network Ground Segment Sustainment Project Preparing for the Future Thomas Gitlin1 and Keith Walyus2 NASA Goddard Space Flight Center, Greenbelt, MD 20771 NASA’s Tracking and Data Relay Satellite System (TDRSS) ground terminals will be replaced in the 2015 timeframe. The existing terminals have been subject to many small scale upgrades and modifications since their last major refurbishment in 1994. The ground terminals, in conjunction with seven operational geosynchronous communication relay satellites, support over 20 customer spacecraft, including Terra, Hubble Space Telescope, the International Space Station and others. The terminal replacement effort, called the Space Network Ground Segment Sustainment (SGSS), will modernize the ground terminal communications infrastructure and provide new capabilities for customers. This paper describes the new architecture, some of the significant technology upgrades and the operations concepts that will enable TDRSS to provide additional services to more customers at lower cost. The SGSS will provide a flexible, extensible, scalable and sustainable ground segment that will: 1) maintain existing Space Network (SN) capabilities and interfaces; 2) accommodate new customers and capabilities, including higher data rate support and additional modulation and coding schemes; 3) reduce the effort required to maintain the ground terminals; 4) transition operations from the existing system to SGSS without disrupting services, and; 5) achieve a 99.99% operational availability for customer services. The SGSS will accomplish this by: 1) implementing an architecture using state-of- the-practice technology which enables low impact incremental upgrades; 2) simplifying the expansion process for adding ground and space assets; 3) incorporating commercial off-the- shelf (COTS) products to a very large extent, and; 4) maximizing equipment commonality.
    [Show full text]
  • 18.1 Development of a Commercial Spaceport
    11/07/16 DEVELOPMENT* OF*COMMERCIAL* SPACEPORT* AND* ASSOCIATED* GROUND* SEGMENT* DRIVEN* BY*SPECIFIC*SPACEPLANE* VEHICLE*AND* MISSION* OPERATION* REQUIREMENTS F.SANTORO,*ALTEC*S.p.A . Altec 2 7 ©220142 res erv ed rights International/Symposium:/‘’Hypersonic:/from/100,000/to/400,000/ft ’’/Rome,/Italy,/June/30thBJuly/1st/2016/ All www.altecspace.it CONTENTS ! Introduction ! Methodology/Overview/ ! The/Reference/Mission ! The/Reference/Spaceplane ! Ground/Segment/Concept Altec 2 7 ! Spaceports ©220142 ! The/Taiping/Airport Study Case res erv ed ! Reentry/Risk/and/Footprint/Analysis rights All ! The/Ground/Station ! The/Space/City www.altecspace.it Page22 1 11/07/16 INTRODUCTION Study case of an initiative aimed at es t ablis hing suborbital flight capabilities with emphasis to the development of the Ground Segment and evaluation of a site as candidate Spaceport From stakeholder analysis to the mission conceptselection Altec 2 7 ©220142 res erv ed rights All Space mission analysis and design: it erat iv e and recursive process, permitting a continue refinement of requirements and constraints leading to a deeper component definition level www.altecspace.it Page23 THE/REFERENCE/MISSION Suborbital Parabolic Mission • Safe VTOL passengers transportation for touristic purposes up to 100 Km altitude over a parabolic flight and reach at least 120 seconds of microgravity • Capability to execute microgravity science during parabolic flights Altec 2 7 ©220142 res erv ed rights All www.altecspace.it Page24 2 11/07/16 THE/REFERENCE/MISSION Point to
    [Show full text]
  • The Newsletter of the Directorate of Manned Spaceflight and Microgravity
    number 7, december 2001 on station The Newsletter of the Directorate of Manned Spaceflight and Microgravity http://www.esa.int/export/esaHS/ 2001: A Good Year - But Hard Work Lies Ahead Jörg Feustel-Büechl ESA Director of Manned Spaceflight and Microgravity We have had a really excellent 2001 in technical terms. Since the first launch, of Zarya in November 1998, we have had 24 launches either to build up the International Space Station with new equipment and facilities, or to service it – a remarkable achievement. Indeed, there have been 12 launches in 2001 alone! Altogether, we have seen some remarkable hardware progress in the programme and – even better – there have been no major in-orbit problems. So we have created an operational Station with a permanent 3-man crew and we have already seen the first experiments (including European experiments) completed. All in all, the Station is working really well, both in terms of its technical realisation and of the international cooperation between the five Partners. Unfortunately, the rest of the picture is not so rosy.We heard from NASA earlier in 2001 of the likelihood of major cost overruns on their part. So far, overall US costs have been around $25 billion and NASA has announced increases of some $4.8 billion to take Station assembly to completion.The Bush Administration declared this to be unacceptable and initiated a review by the NASA Advisory Council.This Review, chaired by Thomas Young, was tasked to investigate what kind of management, cost and technical changes must be implemented in order to contain the costs within the original funding plan.The outcome includes a number of drastic recommendations not only in management and cost control, but also in the Station’s configuration.
    [Show full text]
  • 30 Voices on 2030 – the Future of Space
    30 Voices on 2030 The future of space Communal, commercial, contested May 2020 KPMG.com/au/30voicesonspace © 2020 KPMG, an Australian partnership and a member firm of the KPMG network of independent member firms affiliated with KPMG International Cooperative (“KPMG International”), a Swiss entity. All rights reserved. The KPMG name and logo are registered trademarks or trademarks of KPMG International. Liability limited by a scheme approved under Professional Standards Legislation. 30 Voices on 2030 The future of space Communal, commercial, contested © 2020 KPMG, an Australian partnership and a member firm of the KPMG network of independent member firms affiliated with KPMG International Cooperative (“KPMG International”), a Swiss entity. All rights reserved. The KPMG name and logo are registered trademarks or trademarks of KPMG International. Liability limited by a scheme approved under Professional Standards Legislation. 2 | 30 Voices on 2030: The Future of Space 30 Voices on 2030: The Future of Space Our 30 Voices on 2030 cover every facet of the global space industry and beyond – from space agencies and start-ups to VCs and media organisations. Taken together they create a valuable chorus of insight and expertise. Many of the views expressed in this report may be personal and not necessarily represent those of the Voices’ organisations or KPMG. Visit KPMG.com/au/30voicesonspace to view the report online. Share online #KPMG30Voices © 2020 KPMG, an Australian partnership and a member firm of the KPMG network of independent member firms affiliated with KPMG International Cooperative (“KPMG International”), a Swiss entity. All rights reserved. The KPMG name and logo are registered trademarks or trademarks of KPMG International.
    [Show full text]
  • ISO Cluster-II
    programmes & operations ISO Some of the closest and best-studied star luminous and the bright regions are dark. factories in our Galaxy sprawl across the By penetrating the dust, ISO reveals Operations of ISO continue to go very Orion and Taurus constellations. Without dense regions inside the obscuring clouds smoothly, with all satellite and ground- the extension of its life, ISO could never where new stars are forming. segment systems continuing to perform have looked safely in that direction in the excellently. On 11 December, a third sky as the cold telescope must always station-keeping manoeuvre was remain averted from the intense infrared Cluster-II successfully carried out with performance glow of both the Earth and the Sun. The matching plans to within 0.27%. On the first chance to look at these areas came The contract with the Prime Contractor same day, the third direct measurement in August-September and, despite the Dornier has been successfully negotiated of the amount of liquid helium remaining necessary operational restrictions and agreed by both parties. The on-board was made. The results were described above, many scientific procurement of all spacecraft and consistent with the earlier measurements, observations were performed. With its payload equipment has been initiated, with indications that the lifetime will be at lifetime currently predicted to last until consistent with the delivery of four Cluster the upper end of the predicted range of April 1998, ISO will even have a second spacecraft for launch in mid-2000. For 10 April 1998 ± 2.5 weeks. chance to observe these exciting regions most equipment, this involves a rebuilding in the Spring.
    [Show full text]
  • China's Ground Segment
    China’s Ground Segment Building the Pillars of a Great Space Power Peter Wood with Alex Stone and Taylor A. Lee BluePath Labs, 2020 BluePath Labs, 2020 Labs, BluePath Power Space Great a the Pillars Segment: of Ground Building China’s 10 15 20 25 30 0 5 1970 1971 1972 1973 *Does not include private space private include not *Does 1974 1975 1976 1977 1978 Chinese Space Launches per Year ( Year per Launches Space Chinese 1979 1980 1981 1982 1983 1984 1985 launches 1986 1987 1988 1989 | Source 1990 1991 Abstract 1992 : Launch Record [ Launch Record : 1993 1994 1995 1996 1997 1970 1998 1999 发射记录 2000 - 2001 31 2002 August 2020 August ], ], 2003 CASC, accessed CASC, 2004 2005 2006 2007 2008 2009 )* August 2020 August 2010 2011 2012 2013 2014 2015 2016 2017 2018 2019 2020 2 China’s Ground Segment: Building the Pillars of a Great Space Power What is the Ground Segment? • Includes ground stations such as telemetry, tracking and command (TT&C) stations but also launch facilities, command centers, space tracking ships and other support elements BluePath Labs, 2020 3 China’s Ground Segment: Building the Pillars of a Great Space Power Milestones for Chinese Space Programs “Make major breakthroughs in key Complete Beidou GNSS points and enter the ranks of Space Launch China’s Mars Mission (Tianwen-1) 2020 Great Powers” Complete the “China High-Resolution Earth Observation [重点突破, 进入航天强国行列] System” Lunar sample return mission (Chang’e 5) Begin construction of a long-term space station (completion expected 2022) “Make comprehensive improvements,
    [Show full text]