彈道導(dǎo)彈能力所構(gòu)成的潛在反衛(wèi)星威脅
發(fā)布時(shí)間:2022-01-14 17:00
迄今為止,只有美國(guó)和中國(guó)使用改進(jìn)的彈道導(dǎo)彈技術(shù),成功地獲得和展示了動(dòng)能反衛(wèi)星能力。然而,由于許多其他國(guó)家也已經(jīng)獲得了彈道導(dǎo)彈技術(shù),因此他們也有動(dòng)機(jī)發(fā)展動(dòng)能反衛(wèi)星武器。對(duì)使用這種動(dòng)能反衛(wèi)星技術(shù)實(shí)施限制,將有利于所有在外層空間擁有利益的國(guó)家,并確保所有衛(wèi)星在太空中的安全。然而,至今還未有類(lèi)似的限制。本碩士論文將探討不同國(guó)家的動(dòng)能反衛(wèi)星能力所構(gòu)成的潛在威脅。論文的第一部分將顯示彈道導(dǎo)彈可以達(dá)到的最高高度的計(jì)算。然后,將這些高度與衛(wèi)星的高度做比較,以評(píng)估是否該衛(wèi)星被導(dǎo)彈威脅。這第一部分的結(jié)論是,幾乎所有的低地球軌道衛(wèi)星很容易受到本文所分析的國(guó)家的導(dǎo)彈擊中。本文的第二部分將第一部分的計(jì)算結(jié)果應(yīng)用于具體國(guó)家。本文討論的六個(gè)國(guó)家包括中國(guó),印度,伊朗,朝鮮,俄羅斯,和美國(guó)。選擇這些國(guó)家是因?yàn)樗麄円呀?jīng)具備反衛(wèi)星能力(中國(guó)和美國(guó));被懷疑在不久的將來(lái)將取得反衛(wèi)星能力(印度和俄羅斯);或是因?yàn)槟壳耙該碛写罅康膹椀缹?dǎo)彈能力而被視為構(gòu)成極大威脅(伊朗和朝鮮)。總體結(jié)論是,從長(zhǎng)遠(yuǎn)來(lái)看,制訂反衛(wèi)星武器的法規(guī)框架是有利于每個(gè)國(guó)家的。這個(gè)結(jié)論與具有相似性。本文的結(jié)論是,應(yīng)該支持現(xiàn)有的關(guān)于限制反衛(wèi)星武器的部署和使用的建議...
【文章來(lái)源】:清華大學(xué)北京市 211工程院校 985工程院校 教育部直屬院校
【文章頁(yè)數(shù)】:86 頁(yè)
【學(xué)位級(jí)別】:碩士
【文章目錄】:
摘要
Abstract
CHAPTER 1 INTRODUCTION
CHAPTER 2 BACKGROUND INFORMATION
2.1 Ballistic Missiles
2.1.1 History
2.1.2 Types
2.1.2.1 Tactical Ballistic Missile
2.1.2.2 SRBM
2.1.2.3 MRBM
2.1.2.4 IRBM
2.1.2.5 ICBM
2.1.2.6 SLBM
2.2 ASATs
2.2.1 History
2.2.2 ASAT Tests
2.2.2.1 U.S.’ Test in 1985
2.2.2.2 Chinese Test in 2007
2.2.2.3 U.S.’ Test in 2008
2.3 BMs, ASATs and the Relevance of my Thesis
CHAPTER 3 LITERATURE REVIEW
CHAPTER 4 CALCULATIONS
4.1 Introduction
4.2 Maximum Altitude of the BMs
4.3 Perigees of the Satellites
4.4 Results
4.4.1 China
4.4.2 India
4.4.3 Iran
4.4.4 North Korea
4.4.5 Russia
4.4.6 The U.S
CHAPTER 5 ANALYSIS
5.1 China
5.1.1 History
5.1.2 Effects of the Results
5.1.3 Conclusion
5.2 India
5.2.1 History and Motives
5.2.2 Effects of the Results
5.2.3 Conclusion
5.3 Iran
5.3.1 History and Motives
5.3.2 Effects of the Results
5.3.3 Conclusion
5.4 North Korea
5.4.1 History and Motives
5.4.2 Effects of the Results
5.4.3 Conclusion
5.5 Russia
5.5.1 History and Motives
5.5.2 Effects of the Results
5.5.3 Conclusion
5.6 The U.S
5.6.1 History and Motives
5.6.2 Effects of the Results
5.6.3 Conclusion
CHAPTER 6 CONCLUSIONS AND RECOMMENDATIONS
CHAPTER 7 REFERENCES
Acknowledgements
APPENDIX A: BALLISTIC MISSILE KINEMATICS
APPENDIX B: SATELLITES AND THEIR PERIGEES
China
India
Iran
North Korea
Russia
The U.S
個(gè)人簡(jiǎn)歷/Resume
本文編號(hào):3588880
【文章來(lái)源】:清華大學(xué)北京市 211工程院校 985工程院校 教育部直屬院校
【文章頁(yè)數(shù)】:86 頁(yè)
【學(xué)位級(jí)別】:碩士
【文章目錄】:
摘要
Abstract
CHAPTER 1 INTRODUCTION
CHAPTER 2 BACKGROUND INFORMATION
2.1 Ballistic Missiles
2.1.1 History
2.1.2 Types
2.1.2.1 Tactical Ballistic Missile
2.1.2.2 SRBM
2.1.2.3 MRBM
2.1.2.4 IRBM
2.1.2.5 ICBM
2.1.2.6 SLBM
2.2 ASATs
2.2.1 History
2.2.2 ASAT Tests
2.2.2.1 U.S.’ Test in 1985
2.2.2.2 Chinese Test in 2007
2.2.2.3 U.S.’ Test in 2008
2.3 BMs, ASATs and the Relevance of my Thesis
CHAPTER 3 LITERATURE REVIEW
CHAPTER 4 CALCULATIONS
4.1 Introduction
4.2 Maximum Altitude of the BMs
4.3 Perigees of the Satellites
4.4 Results
4.4.1 China
4.4.2 India
4.4.3 Iran
4.4.4 North Korea
4.4.5 Russia
4.4.6 The U.S
CHAPTER 5 ANALYSIS
5.1 China
5.1.1 History
5.1.2 Effects of the Results
5.1.3 Conclusion
5.2 India
5.2.1 History and Motives
5.2.2 Effects of the Results
5.2.3 Conclusion
5.3 Iran
5.3.1 History and Motives
5.3.2 Effects of the Results
5.3.3 Conclusion
5.4 North Korea
5.4.1 History and Motives
5.4.2 Effects of the Results
5.4.3 Conclusion
5.5 Russia
5.5.1 History and Motives
5.5.2 Effects of the Results
5.5.3 Conclusion
5.6 The U.S
5.6.1 History and Motives
5.6.2 Effects of the Results
5.6.3 Conclusion
CHAPTER 6 CONCLUSIONS AND RECOMMENDATIONS
CHAPTER 7 REFERENCES
Acknowledgements
APPENDIX A: BALLISTIC MISSILE KINEMATICS
APPENDIX B: SATELLITES AND THEIR PERIGEES
China
India
Iran
North Korea
Russia
The U.S
個(gè)人簡(jiǎn)歷/Resume
本文編號(hào):3588880
本文鏈接:http://sikaile.net/kejilunwen/jingguansheji/3588880.html
最近更新
教材專(zhuān)著