Chapter 0 Contents

Total Page:16

File Type:pdf, Size:1020Kb

Chapter 0 Contents LM-3A Series Launch Vehicle User’s Manual LM-3A Series Launch Vehicle User’s Manual Issue 2011 APPROVALS CEN Zheng GAO Ruofei SHEN Lei Director General Executive Vice President President LM-3A Series China Academy of Launch China Great Wall Industry China Satellite Launch & Vehicle Technology Corporation Tracking Control General (CALT) (CGWIC) (CLTC) Issue 2011 0-1 LM-3A Series Launch Vehicle User’s Manual [ Intentionally Blank ] 0-2 Issue 2011 LM-3A Series Launch Vehicle User’s Manual FOREWORD This Long March 3A (LM-3A) Series Launch Vehicle User’s Manual is intended to provide the essential technical and programmatic information on the LM-3A, LM-3B, LM-3B Enhanced (LM-3BE) and LM-3C launch vehicles for the customers’ preliminary mission planning and spacecraft design. The Manual also provides information of the launch site facilities, the documentation required, typical launch processing, the mission analysis requirements and details of the additional engineering support available to the customer’s mission. This Manual is to be used as the baseline for using the LM-3A Series launch vehicle, and the detailed requirements will be defined in the relevant technical documents of the launch services contract. This Manual will be updated as necessary. The updated information will be provided to existing customers. The current version and all updates will also be posted to the www.cgwic.com and www.calt.com web site for download as needed. This Issue will supersede any information given in the previous issues or occasions. Users of this Manual are encouraged to contact the offices listed below to discuss the LM-3A Series launch vehicle and how the Long March (LM) launch vehicles can meet the user’s requirements. For general issues: Launch Services Division China Great Wall Industry Corporation Building 2, No. 18A, Xing Shi Kou Road, Haidian District Beijing 100195, P. R. China Tel: +86 10 8810 2168 Fax: +86 10 8810 2109 E-mail: [email protected] www.cgwic.com For technical issues: Space Division China Academy of Launch Vehicle Technology No.1, Nan Da Hong Men Road, Fengtai District Beijing 100076, P. R. China Tel: +86 10 6876 9837, +86 10 6875 3701 Fax: +86 10 6875 7398 E-mail: [email protected] or [email protected] www.calt.com Issue 2011 0-3 LM-3A Series Launch Vehicle User’s Manual REVISION HISTORY Issue Title Change Description Approval CEN Zheng LM-3A Series Launch Completely revised compared to 2011 Director General Vehicle User’s Manual Issue 1999. LM-3A Series Three manuals in Issue 1999 were LM-3A Series Launch LONG Lehao integrated into one manual in Issue 2003 Vehicle User’s Manual Director General 2003. (Only Chinese version was (Chinese Version) LM-3A Series published for Issue 2003.) LM-3A User’s Manual There were three independent LONG Lehao 1999 LM-3B User’s Manual manuals in Issue 1999, for LM-3A, Director General LM-3C User’s Manual LM-3B and LM-3C respectively. LM-3A Series 0-4 Issue 2011 LM-3A Series Launch Vehicle User’s Manual PREFACE China Aerospace Science and Technology Corporation (CASC) evolved from China Aerospace Corporation, which was created from the Fifth Academy of the Ministry of National Defense established on October 8, 1956. The Fifth Academy was expanded into the Seventh Ministry of Machinery Industry and underwent further changes through the Ministry of Space Industry, the Ministry of Aerospace Industry and China Aerospace Industry Corporation, from which CASC was formally founded on July 1, 1999 with the approval of the State Council of the People’s Republic of China. CASC is a large state-owned enterprise group with its own internationally recognized brands such as Long March and Shenzhou. CASC has developed its own intellectual properties in the space industry, and it has an outstanding record for its core business and is highly competitive in the international market. As an institutional investor authorized by the State Council, CASC has eight large R&D and production entities in addition to China Great Wall Industry Corporation, plus many other institutions and companies directly subordinated to it. CASC’s primary business includes research, design, manufacture and launch of space systems and products, such as launch vehicles, satellites and manned spaceships. China Great Wall Industry Corporation (CGWIC) is a launch services provider offering low risk and reliable solutions to deliver the customers’ satellites into a wide range of orbits. The launch services are provided directly through CGWIC, which is the exclusive commercial organization authorized by the Chinese Government to offer Long March launch services to the international market. As the prime contractor for launch services, CGWIC is responsible for marketing launch services, negotiation and implementation of the launch services contract. CGWIC provides the customer with a single point of contact for all communications related to launch services contract. China Academy of Launch Vehicle Technology (CALT) is the designer and manufacturer of LM-3A Series launch vehicles and is a subcontractor for launch services. CALT is responsible for the launch vehicle design, development, manufacture, testing, mission analyses, launch vehicle technical interface coordination and flight safety engineering. CGWIC and CALT are both wholly – owned subsidiaries of CASC. China Satellite Launch and Tracking Control General (CLTC) is in charge of China’s TT&C network and launch sites, including XSLC, JSLC and TSLC. As the subcontractor of Long Issue 2011 0-5 LM-3A Series Launch Vehicle User’s Manual March launch services, CLTC is responsible for the TT&C and launch site technical and interface coordination, launch site operations, launch control and launch site safety. In cooperation with CALT and CLTC, CGWIC has established an outstanding launch record that clearly demonstrates the high reliability of Long March launch vehicles and their ability to deliver the customers’ satellite into designed orbit in an accurate and reliable manner. 0-6 Issue 2011 LM-3A Series Launch Vehicle User’s Manual TABLE OF CONTENTS APPROVAL PAGE .............................................................................................................0-1 FOREWORD ......................................................................................................................0-3 REVISION HISTORY..........................................................................................................0-4 PREFACE...........................................................................................................................0-5 TABLE OF CONTENTS .....................................................................................................0-7 LIST OF FIGURES ...........................................................................................................0-15 LIST OF TABLES.............................................................................................................0-20 ABBREVIATIONS AND ACRONYMS ..............................................................................0-22 CHAPTER 1 INTRODUCTION...........................................................................................1-1 1.1 Long March Family of Launch Vehicles - Development History ......................................1-3 1.2 Long March Launch Services....................................................................................1-4 1.2.1 Overview.............................................................................................................1-4 1.2.2 Customer Interfaces ...........................................................................................1-6 1.3 Overview of the Launch Centers ...............................................................................1-6 1.3.1 Xichang Satellite Launch Center (XSLC)............................................................1-7 1.3.2 Taiyuan Satellite Launch Center (TSLC).............................................................1-8 1.3.3 Jiuquan Satellite Launch Center (JSLC).............................................................1-9 1.4 Launch Record of Long March ..................................................................................1-9 1.5 Long March Launch Services Advantages ..............................................................1-10 CHAPTER 2 GENERAL DESCRIPTION............................................................................2-1 2.1 Summary...................................................................................................................2-1 2.2 LM-3A Launch Vehicle ..............................................................................................2-2 2.2.1 Technical Parameters.........................................................................................2-2 2.2.2 LM-3A Description ..............................................................................................2-4 2.3 LM-3B and LM-3BE Launch Vehicles .....................................................................2-15 2.3.1 Technical Parameters.......................................................................................2-15 2.3.2 LM-3B and LM-3BE Description .......................................................................2-17 2.4 LM-3C Launch Vehicle............................................................................................2-21 2.5 Launch Vehicle Coordinate System ........................................................................2-22 2.6 Launch Missions of LM-3A Series Launch Vehicles................................................2-23
Recommended publications
  • Call for M5 Missions
    ESA UNCLASSIFIED - For Official Use M5 Call - Technical Annex Prepared by SCI-F Reference ESA-SCI-F-ESTEC-TN-2016-002 Issue 1 Revision 0 Date of Issue 25/04/2016 Status Issued Document Type Distribution ESA UNCLASSIFIED - For Official Use Table of contents: 1 Introduction .......................................................................................................................... 3 1.1 Scope of document ................................................................................................................................................................ 3 1.2 Reference documents .......................................................................................................................................................... 3 1.3 List of acronyms ..................................................................................................................................................................... 3 2 General Guidelines ................................................................................................................ 6 3 Analysis of some potential mission profiles ........................................................................... 7 3.1 Introduction ............................................................................................................................................................................. 7 3.2 Current European launchers ...........................................................................................................................................
    [Show full text]
  • Space Launch System (Sls) Motors
    Propulsion Products Catalog SPACE LAUNCH SYSTEM (SLS) MOTORS For NASA’s Space Launch System (SLS), Northrop Grumman manufactures the five-segment SLS heavy- lift boosters, the booster separation motors (BSM), and the Launch Abort System’s (LAS) launch abort motor and attitude control motor. The SLS five-segment booster is the largest solid rocket motor ever built for flight. The SLS booster shares some design heritage with flight-proven four-segment space shuttle reusable solid rocket motors (RSRM), but generates 20 percent greater average thrust and 24 percent greater total impulse. While space shuttle RSRM production has ended, sustained booster production for SLS helps provide cost savings and access to reliable material sources. Designed to push the spent RSRMs safely away from the space shuttle, Northrop Grumman BSMs were rigorously qualified for human space flight and successfully used on the last fifteen space shuttle missions. These same motors are a critical part of NASA’s SLS. Four BSMs are installed in the forward frustum of each five-segment booster and four are installed in the aft skirt, for a total of 16 BSMs per launch. The launch abort motor is an integral part of NASA’s LAS. The LAS is designed to safely pull the Orion crew module away from the SLS launch vehicle in the event of an emergency on the launch pad or during ascent. Northrop Grumman is on contract to Lockheed Martin to build the abort motor and attitude control motor—Lockheed is the prime contractor for building the Orion Multi-Purpose Crew Vehicle designed for use on NASA’s SLS.
    [Show full text]
  • Paper Session IA-Shuttle-C Heavy-Lift Vehicle of the 90'S
    The Space Congress® Proceedings 1989 (26th) Space - The New Generation Apr 25th, 2:00 PM Paper Session I-A - Shuttle-C Heavy-Lift Vehicle of the 90's Robert G. Eudy Manager, Shuttle-C Task Team, Marshall Space Flight Center Follow this and additional works at: https://commons.erau.edu/space-congress-proceedings Scholarly Commons Citation Eudy, Robert G., "Paper Session I-A - Shuttle-C Heavy-Lift Vehicle of the 90's" (1989). The Space Congress® Proceedings. 5. https://commons.erau.edu/space-congress-proceedings/proceedings-1989-26th/april-25-1989/5 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]. SHUTTLE-C HEAVY-LIFT VEHICLE OF THE 90 ' S Mr. Robert G. Eudy, Manager Shuttle-C Task Team Marshall Space Flight Center ABSTRACT United States current and planned space activities identify the need for increased payload capacity and unmanned flight to complement the existing Shuttle. To meet this challenge the National Aeronautics and Space Administration is defining an unmanned cargo version of the Shuttle that can give the nation early heavy-lift capability. Called Shuttle-C, this unmanned vehicle is a natural, low-cost evolution of the current Space Shuttle that can be flying 100,000 to 170,000 pound payloads by late 1994. At the core of Shuttle-C design philosophy is the principle of evolvement from the United State's Space Transportation System.
    [Show full text]
  • View / Download
    www.arianespace.com www.starsem.com www.avio Arianespace’s eighth launch of 2021 with the fifth Soyuz of the year will place its satellite passengers into low Earth orbit. The launcher will be carrying a total payload of approximately 5 518 kg. The launch will be performed from Baikonur, in Kazakhstan. MISSION DESCRIPTION 2 ONEWEB SATELLITES 3 Liftoff is planned on at exactly: SOYUZ LAUNCHER 4 06:23 p.m. Washington, D.C. time, 10:23 p.m. Universal time (UTC), LAUNCH CAMPAIGN 4 00:23 a.m. Paris time, FLIGHT SEQUENCES 5 01:23 a.m. Moscow time, 03:23 a.m. Baikonur Cosmodrome. STAKEHOLDERS OF A LAUNCH 6 The nominal duration of the mission (from liftoff to separation of the satellites) is: 3 hours and 45 minutes. Satellites: OneWeb satellite #255 to #288 Customer: OneWeb • Altitude at separation: 450 km Cyrielle BOUJU • Inclination: 84.7degrees [email protected] +33 (0)6 32 65 97 48 RUAG Space AB (Linköping, Sweden) is the prime contractor in charge of development and production of the dispenser system used on Flight ST34. It will carry the satellites during their flight to low Earth orbit and then release them into space. The dedicated dispenser is designed to Flight ST34, the 29th commercial mission from the Baikonur Cosmodrome in Kazakhstan performed by accommodate up to 36 spacecraft per launch, allowing Arianespace and its Starsem affiliate, will put 34 of OneWeb’s satellites bringing the total fleet to 288 satellites Arianespace to timely deliver the lion’s share of the initial into a near-polar orbit at an altitude of 450 kilometers.
    [Show full text]
  • Monsoon 2008 (July-September) AIR POWER CENTRE for AIR POWER STUDIES New Delhi
    AIR POWER Journal of Air Power and Space Studies Vol. 3, No. 3, Monsoon 2008 (July-September) AIR POWER CENTRE FOR AIR POWER STUDIES New Delhi AIR POWER is published quarterly by the Centre for Air Power Studies, New Delhi, established under an independent trust titled Forum for National Security Studies registered in 2002 in New Delhi. Board of Trustees Shri M.K. Rasgotra, former Foreign Secretary and former High Commissioner to the UK Chairman Air Chief Marshal O.P. Mehra, former Chief of the Air Staff and former Governor Maharashtra and Rajasthan Smt. H.K. Pannu, IDAS, FA (DS), Ministry of Defence (Finance) Shri K. Subrahmanyam, former Secretary Defence Production and former Director IDSA Dr. Sanjaya Baru, Media Advisor to the Prime Minister (former Chief Editor Financial Express) Captain Ajay Singh, Jet Airways, former Deputy Director Air Defence, Air HQ Air Commodore Jasjit Singh, former Director IDSA Managing Trustee AIR POWER Journal welcomes research articles on defence, military affairs and strategy (especially air power and space issues) of contemporary and historical interest. Articles in the Journal reflect the views and conclusions of the authors and not necessarily the opinions or policy of the Centre or any other institution. Editor-in-Chief Air Commodore Jasjit Singh AVSM VrC VM (Retd) Managing Editor Group Captain D.C. Bakshi VSM (Retd) Publications Advisor Anoop Kamath Distributor KW Publishers Pvt. Ltd. All correspondence may be addressed to Managing Editor AIR POWER P-284, Arjan Path, Subroto Park, New Delhi 110 010 Telephone: (91.11) 25699131-32 Fax: (91.11) 25682533 e-mail: [email protected] website: www.aerospaceindia.org © Centre for Air Power Studies All rights reserved.
    [Show full text]
  • Spacewatchafrica April Edition 2019
    Paul Kagame launches Rwanda into space VVVolVolVolVol o6 o6 66l l. .No. NoNo. No77 N N 55 oo5.. 816 April 2018 2019 AFRICA By Marcel Dischinger Prof.(Sir) Martin Sweeting “SSTL transfer know-how, not technology developing countries.” C O N T E N T S Vol. 7 No. 16 Editor in-chief Aliyu Bello 2018 was another good year Executive Manager Tonia Gerrald NASRDA's chief executive to step down SA to the editor in-Chief Ngozi Okey Head, Application Services M. Yakubu SES posted strong revenue growth in 2018 Editorial/ICT Services John Daniel Nestle using satellites to monitor palm oil plantations Usman Bello for deforestation Alozie Nwankwo How global satellite network convinced Juliet Nnamdi FAA grounding of Boeing's 737 Max Client Relations Sunday Tache Nigeria plans new systems to improve GPS accuracy over Africa Lookman Bello Safiya Thani Ivory Coast begins digital TV switch over with GatesAir Marketing Offy Pat Eutelsat successfully mate KONNECT satellite payload Tunde Nathaniel with its all-electric platform Wasiu Olatunde SSTL transfer know-how not technology to Media Relations Favour Madu developing countries Khadijat Yakubu Paul Kagame launches Rwanda into space Zacheous Felicia Monitoring desertification using integrated Finance Folarin Tunde geospatial technologies APT Satellite releases 2018 annual results Space Watch Magazine is a publication of Communication Science, Inc. All correspondence should be addressed to editor, space Watch Magazine. Abuja office: Plot 2009, Awka Street, UTC Building, GF 11, Area 10, Garki, Abuja, Nigeria Tel: 234 80336471114, 07084706167, email: [email protected] LEGAL CONSULTANTS Idowu Oriola & Co. Garki, Abuja DISTRIBUTION CONTACTS Ade Adejo ABIJAN INTERNATIONAL Suleija, Abuja AYO DISTRIBUTION AGENCY Emir Road, Ilorin Olumayowa Ojo NEWSROUND INTERNATIONAL Area 10, Garki, Abuja Magazine Circulation Nigeria Limited 90, Obafemi Awolowo Way, Ikeja Magazine Subscription Nigeria Limited Ikeja, Lagos.
    [Show full text]
  • Orbital Debris: a Chronology
    NASA/TP-1999-208856 January 1999 Orbital Debris: A Chronology David S. F. Portree Houston, Texas Joseph P. Loftus, Jr Lwldon B. Johnson Space Center Houston, Texas David S. F. Portree is a freelance writer working in Houston_ Texas Contents List of Figures ................................................................................................................ iv Preface ........................................................................................................................... v Acknowledgments ......................................................................................................... vii Acronyms and Abbreviations ........................................................................................ ix The Chronology ............................................................................................................. 1 1961 ......................................................................................................................... 4 1962 ......................................................................................................................... 5 963 ......................................................................................................................... 5 964 ......................................................................................................................... 6 965 ......................................................................................................................... 6 966 ........................................................................................................................
    [Show full text]
  • Spaceport Infrastructure Cost Trends
    AIAA 2014-4397 SPACE Conferences & Exposition 4-7 August 2014, San Diego, CA AIAA SPACE 2014 Conference and Exposition Spaceport Infrastructure Cost Trends Brian S. Gulliver, PE1, and G. Wayne Finger, PhD, PE2 RS&H, Inc. The total cost of employing a new or revised space launch system is critical to understanding its business potential, analyzing its business case and funding its development. The design, construction and activation of a commercial launch complex or spaceport can represent a significant portion of the non-recurring costs for a new launch system. While the historical cost trends for traditional launch site infrastructure are fairly well understood, significant changes in the approach to commercial launch systems in recent years have required a reevaluation of the cost of ground infrastructure. By understanding the factors which drive these costs, informed decisions can be made early in a program to give the business case the best chance of economic success. The authors have designed several NASA, military, commercial and private launch complexes and supported the evaluation and licensing of commercial aerospaceports. Data from these designs has been used to identify the major factors which, on a broad scale, drive their non-recurring costs. Both vehicle specific and location specific factors play major roles in establishing costs. I. Introduction It is critical for launch vehicle operators and other stakeholders to understand the factors and trends that affect the non-recurring costs of launch site infrastructure. These costs are often an area of concern when planning for the development of a new launch vehicle program as they can represent a significant capital investment that must be recovered over the lifecycle of the program.
    [Show full text]
  • Another Global History of Science: Making Space for India and China
    BJHS: Themes 1: 115–143, 2016. © British Society for the History of Science 2016. This is an Open Access article, distributed under the terms of the Creative Commons Attribution licence (http://creativecommons.org/licenses/by/4.0/), which permits unrestricted re-use, distribution, and reproduction in any medium, provided the original work is properly cited. doi:10.1017/bjt.2016.4 First published online 22 March 2016 Another global history of science: making space for India and China ASIF SIDDIQI* Abstract. Drawing from recent theoretical insights on the circulation of knowledge, this article, grounded in real-world examples, illustrates the importance of ‘the site’ as an analytical heur- istic for revealing processes, movements and connections illegible within either nation-centred histories or comparative national studies. By investigating place instead of project, the study reframes the birth of modern rocket developments in both China and India as fundamentally intertwined within common global networks of science. I investigate four seemingly discon- nected sites in the US, India, China and Ukraine, each separated by politics but connected and embedded in conduits that enabled the flow of expertise during (and in some cases despite) the Cold War. By doing so, it is possible to reconstruct an exemplar of a kind of global history of science, some of which takes place in China, some in India, and some else- where, but all of it connected. There are no discrete beginnings or endings here, merely points of intervention to take stock of processes in action. Each site produces objects and knowledge that contribute to our understanding of the other sites, furthering the overall narra- tive on Chinese and Indian efforts to formalize a ‘national’ space programme.
    [Show full text]
  • Launcherone Success Opens New Space Access Gateway Guy Norris January 22, 2021
    1/22/21 7:05 1/6 LauncherOne Success Opens New Space Access Gateway Guy Norris January 22, 2021 With San Nicolas Island far below, LauncherOne headed for polar orbit. Credit: Virgin Orbit Virgin Orbit had barely tweeted news of the successful Jan. 17 space debut of its LauncherOne vehicle on social media when new launch contracts began arriving in the company’s email inbox. A testament to the pent-up market demand for small-satellite launch capability, the speedy reaction to the long-awaited demonstration of the new space-access vehicle paves the way for multiple follow-on Virgin Orbit missions by year-end and a potential doubling of the rate in 2022. First successful privately developed air-launched, liquid-fueled rocket Payloads deployed for NASA’s Venture Class Launch Services program The glitch-free !ight of LauncherOne on its second demonstration test was a critical and much-welcomed milestone for the Long Beach, California-based company. Coming almost nine years a"er the air-launch concept was #rst unveiled by Virgin founder Richard Branson, and six years a"er the start of full-scale development, the !ight followed last May’s #rst demonstration mission, which ended abruptly when the rocket motor shut o$ a"er just 4 sec. 1/22/21 7:05 2/6 A"er an exhaustive analysis and modi#cations to beef up the oxidizer feed line at the heart of the #rst !ight failure, the path to the Launch Demo 2 test was then delayed until January 2021 by the COVID-19 pandemic. With the LauncherOne system now proven, design changes veri#ed and the #rst 10 small satellites placed in orbit, Virgin Orbit is already focusing on the next steps to ramp up its production and launch-cadence capabilities.
    [Show full text]
  • The New Commercial Spaceports
    The New Commercial Spaceports Derek Webber1 Spaceport Associates, Rockville, Maryland 20852,USA During the second half of the 20th Century, the first launch sites were established, mostly during the ‘fifties and ‘sixties. They were originally a product of the cold war and served military and civil government purposes. They were used for launching sounding rockets, space probes, for missile testing and injecting military, scientific, and eventually commercial satellites into orbit. Initially the sites were in either the USA or the former Soviet Union, but gradually they were introduced in other countries too. Governmental astronaut crews were also sent into orbit from these early launch sites. As the 21st Century begins, a new era is emerging where a fuller range of commercial missions will be undertaken and moreover where public space travel will become common place. This situation ushers in a new kind of launch facility, known as the commercial spaceport. I. Introduction here will be vastly different requirements for the future public space travelers, and their families and friends, T than are normally available at the traditional launch sites built fifty years ago. Indeed, the creation of this emerging kind of facility, the commercial spaceport, is in some ways a very necessary part of the creation of the new space businesses that the twenty-first century offers. It will be essential that, while the space tourism companies are becoming established in order to provide services to the new public space travelers, suitable ground based facilities will be developed in parallel to sustain and support these operations. This paper provides an insight into these commercial spaceport facilities, and their characteristics, in order to assist in both design and business planning processes.
    [Show full text]
  • NIDS China Security Report 2021 China’S Military Strategy in the New Era
    ISBN: 978-4-86482-088-2 NIDS CHINA SECURITY REPORT NIDS China Security Report 2021 China’s Military Strategy in the New Era National Institute for Defense Studies, Japan National Institute for Defense Studies, Japan NIDS China Security Report 2021 China’s Military Strategy in the New Era Published by The National Institute for Defense Studies 5-1 Honmura-cho, Ichigaya, Shinjuku-ku, Tokyo 162-8808 Japan Website: http://www.nids.mod.go.jp Translated by INTERBOOKS Copyright © 2020 by the National Institute for Defense Studies, Japan All rights reserved. No part of this publication may be reproduced in any form without written, prior permission from the publisher. The China Security Report 2021 comprises NIDS researchers’ analyses and descriptions based on information compiled from open sources in Japan and overseas. The statements contained herein do not necessarily represent the official position of the Government of Japan or the Ministry of Defense. This publication is a translation of the Japanese version originally published in November 2020. ISBN978-4-86482-088-2 Printed in Japan NIDS China Security Report 2021 Contents Preface iii Summary v Acronyms and Abbreviations viii Introduction 2 Chapter 1: China’s Preparations for Informatized Warfare 1. Changes in China’s Military Strategy 6 (1) The Era of Mao Zedong (1927–1976): The Curse of the Final War and Active Defense 6 (2) The Era of Deng Xiaoping (1976–1989): A Break from the Final War and a Shift to Local War 7 (3) The Era of Jiang Zemin (1989–2004): Local Wars under High-Tech Conditions 9 (4) The Era of Hu Jintao (2004–2012): Informatized Local Wars 10 2.
    [Show full text]