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UNIVERSITE DE GENEVE

INSTITUT UNIVERSITAIRE DE HAUTES ETUDES INTERNATIONALES

THE TRANSFER OF DUAL-USE OUTER SPACE

TECHNOLOGIES: CONFRONTATION OR

CO-OPERATION?

Thèse

présentée à l’Université de Genève pour l’obtention du grade de Docteur en

relations internationales

par

Péricles GASPARINI ALVES

(Brésil)

Thèse No. 612

GENEVE 2000

(2)

Epigraph

The first of December had arrived! the fatal day! for, if the projectile were not discharged that

very night at 10h. 46m.40s. p.m., more than eighteen years must roll by before the moon

would again present herself under the same conditions of zenith and perigee.

The weather was magnificent. ...

The whole plain was covered with huts, cottages, and tents. Every nation under the sun was represented there; and every language might be heard spoken at the same time. It was a perfect Babel re-enacted. ...

The moment had arrived for saying ‘Goodbye!’ The scene was a touching one. ... ‘Thirty-five!—thirty-six!—thirty-seven!—thirty-eight!—thirty-nine!—forty! Fire!!!’

Instantly Murchison pressed with his finger the key of the electric battery, restored the current of the fluid, and discharged the spark into the breach of the Columbiad.

An appalling, unearthly report followed instantly, such as can be compared to nothing whatever known, not even to the roar of thunder, or the blast of volcanic explosion! No words can convey the slightest idea of the terrific sound! An immense spout of fire shot up from the bowels of the earth as from a crater. The earth heaved up, and ...

View of the Moon in orbit around the Earth, Galileo Spacecraft, 16 December 1992

image002

Courtesy of NASA

‘The projectile discharged by the Columbiad at Stones Hill has been detected ...12th December, at 8.47 pm., the moon having entered her last quarter. This projectile has not arrived at its destination, it has passed by the side; but sufficiently near to be retained by the lunar attraction. ...

‘However, two hypotheses come here into our consideration.

‘1. Either the attraction of the moon will end by drawing them into itself, and the travellers will attain their destination; or, —

‘2. The projectile, following an immutable law, will continue to gravitate round the moon till the end of time.

‘At some future time, our observations will be able to determine this point, but till then the experiment of the Gun Club can have no other result than to have provided our solar system with a new star. Extracted from the Chapters

“Fire!” & “A New Star”

From the Earth to the Moon

Jules Verne 1865

(3)

Acknowledgments

The decision to write a Thesis dissertation may not be too difficult to make, especially since

obtaining a Doctoral’s Degree at the end of a Thesis process is an encouraging stimulus.

However, ideas are always easier to conceive and announce than to implement: writing a

PhD. Thesis is no exception. Nonetheless, despite the many difficulties one may encounter in

writing a dissertation, the level of satisfaction that may be enjoyed when arriving at the finish

line is often greater than any obstacle encountered on the way. This has been my own

experience.

The road I took to write this manuscript was not always an easy one to ride on. I have

encountered many obstacles which made this endeavour evermore difficult than it could have

been otherwise. Some of these obstacles were predictable, since they were clearly in

confrontation with my démarche. In retrospect, they have not been strong enough to stop me

from moving mountains in a crusade of words and deeds. Other obstacles, however, were

considerably more difficult to surmount for reasons which are not worth mentioning here.

Fortunately, my efforts and determination were stronger than their opposition and the

prospective reader shall judge if it was worthwhile the effort to finish this work.

I would like to mention those who facilitated the completion of this work and my first thanks

goes to those who played a fundamental role in supporting my original ideas and efforts.

Namely, Ambassador Jayantha Dhanapala, then Director of the United Nations Institute for

Disarmament Research (UNIDIR) and at present UN Under-Secretary-General for

Disarmament Affairs, who always supported my work and ceaselessly advised me to continue

pursuing my studies. His successor, Mr Sverre Lodgaard, always hinted that I should pay

more attention to potential contributions that confidence-and security-building measures could

provide to the technology transfer debate; and Patricia Lewis, current UNIDIR Director,

supported my efforts to complete this manuscript. Additionally, special thanks are also

addressed to Professor Serge Sur, former Deputy Director of UNIDIR, for the long hours of

conversation on space and related matters during my tenure at the Institute. His comments and

support were very much appreciated.

My sincere and warm thanks must go to Mr Curt Gasteyger, Emeritus Professor and Director

of the Programme for Strategic Studies and International Security at the Graduate Institute of

International Studies (IUHEI). Besides being one of my teachers at IUHEI and Director of my

(4)

Thesis, Professor Gasteyger was also Director of two other works of mine at the Institute: a

Memoire de Diplôme in 1988 and Memoire de diplome d’etude superior (DES) in 1993. It

was therefore a pleasure and indeed an honour that he accepted to be the Director of my PhD.

Every since the early stages of this Thesis, Professor Gasteyger provided me with important

strategic advice as regards both the general line of thought of this work and issues of

substance. I must note here that he did not always agree with my description or appreciation

of events and ideas, but his doubts only encouraged me to better clarify my views. This

feature of our student/professor relationship was quite challenging and extremely important to

stimulate my thoughts. Additionally, I should also like to attest my gratitude for Professor

Gasteyger’s institutional and moral support throughout my many years of studies at IUHEI,

without which I would probably not have been able to carry-out this work.

I also thank all of those who assisted me in visiting various space and space-related factories

and installations throughout the world, interview scientists and technicians on-site. This

proved to be extremely useful since for me, as a student of international relations, I was

neither trained nor exposed to detailed technical aspects of outer space technologies.

The support of Véronique Marie Clément Alves, my wife, was also essential for me to face

the challenge of writing a PhD Thesis and I thank her many hours of patience and active

support for me to carry on this important but tedious work.

Miss Riche Pannetti of Geneva deserves special mention in this acknowledgments. Miss

Pannetti has assisted me making the necessary language corrections and indeed polishing the

English to be appreciated in its own merit. She has not measured efforts in helping me and

often exceeded regular working hours to finish one more sentence, paragraph, page, chapter...

Unfortunately, for reasons of time, she did not have the opportunity to finish all the

corrections. I also thank her for being a true friend at good and difficult moments.

Last, but not least, while apologizing for those whom I may have unintentionally omitted, I

should like to state that the responsibility of the statements in this Thesis are my own and

neither of those whom I have mentioned nor of the Institution I work for.

(5)

List of Acronyms and Symbols

ABL Airborne

Laser

ABM Anti-Ballistic

Missile

ACDA

Arms Control and Disarmament Agency (USA)

ACRS

Arms Control and Regional Security

ADCP

Air Defence Communication Platform

AEGIS

Ship-mounted weapons system

AG Australian

Group

AGRE

Active Geophysical Rocket Experiment

AHWG

Ad Hoc Working Group

ALCM

Air-Launched Cruise Missile

ALERT

Attack & Launch Early Reporting to Theatre

AMI

Active Microwave Instrument

ANSC

Alliance New Strategic Concept

ANSP

Australian National Space Programme

AN/TPS Ground-based

radar

AOC

Air Operations Centre

AR Altimeter

Radar

ARABSAT Arab Corporation for Space Communication

ARGOS

Data Collecting System

ARR

Andøya Rocket Range (Norway)

ARTEMIS

Advanced Relay TEchnology MISsion (ESA)

ASAR

Advanced Synthetic Aperture Radar

ASAT Anti-Satellite

weapons

ASB

Australian Space Board

ASBM

Air-to-Surface Ballistic Missile

ASI

Italian Space Agency

ASLV

Augmented Satellite Launch Vehicle (India)

ASO

Australian Space Office

ATSR

Along-Track Scanning Radiometer

ATSR-M

Along-Track Scanning Radiometer & Microwave Sounder

AUSSAT Australian

Satellite

(6)

Bae British

Aerospace

BEAR

Beam Experiment Aboard Rocket (SDI)

BM Ballistic

Missile

BM/C

3

Battle Management/Command, Control, Communications

BMD

Ballistic Missile Defense

BMDO

Ballistic Missile Defense Organization

BMFT

Federal Ministry for Research and Technology (Germany)

BMI

Ballistic Missile Interception

BNSC

British National Space Centre

BPI Boost-Phase

Interceptor

BRAZILSAT Brazilian Satellite

BSA

Brazilian Space Agency

BSTS

Boost Surveillance and Tracking Satellite

BUR Bottom-Up

Review

BW Biological

Weapons

BWC

Biological and Toxin Weapons Convention

C

2

Command and Control

C

3

I

Communications, Command, Control and Intelligence

CALT

China Academy of Launch Vehicle Technology

CASDN

National Defence Scientific Steering Committee (France)

CAST

Chinese Academy of Space Technology

CASTR

Chinese Academy of Space Technology Research

CBERS

China-Brazil Earth Resource Satellite

CBMs Confidence-Building

Measures

Cbo

Collision Bodies (ASAT weapons)

CCD

Charge Coupled Devise

CCI

Constellation Communications, Inc.

CD

Conference on Disarmament

CFE

Conventional Armed Forces in Europe

ChR

Chemical Rockets (ASAT weapons)

CIA

Central Intelligence Agency (USA)

CII

International Export Certificate (Brazil)

CIS

Commonwealth of Independent States

(7)

CLTC

China Satellite Launch and TT&C General

CM Cruise

Missile

CMC

Central Military Commission (Japan)

CNAD

Conference of National Armaments Directors

CNES

National Centre of Space Studies (France)

CNIE

National Commission of Space Research (Argentina)

CNR

National Research Council (Italy)

CNRS

National Centre of Scientific Research (France)

COBAE

Brazilian Commission for Space Activities

COCOM

Coordinating Committee for Multilateral Export Control

CONAE

National Commission of Space Activities (Argentina)

COPUOS

Committee on the Peaceful Uses of Outer Space

COSTND

Commission of Science and Technology for National Defence

CPE

Circle Probable Error

CPI

Permanent Inter-ministerial Commission (Brazil)

CRC

Command Report Centre

CSA

Canadian Space Agency

CSBMs

Confidence- and Security-Building Measures

CSC

Central Special Committee (Japan)

CSCB

Clouds of Small Collision Bodies (ASAT weapons)

CSG

French Guyana Space Centre

CSS Chinese

Surface-to-Surface

CTA

Aerospace Technical Centre (Brazil)

CTBT

Comprehensive Test-Ban Treaty

CTS

Communications Technology Satellite (Canada)

CVE

Verification of Delivery Certificate (Brazil)

CW Chemical

Weapons

CWC

Chemical Weapons Convention

CZ Chang

Zheng

DAMs

Direct Ascending Missiles (ASAT weapons)

DARA

German Space Agency

DARPA

Defence Advanced Research Projects Agency (USA)

DEDU

Development and Educational Communication Unit (India)

(8)

DMA

Ministerial Armaments Delegation (France)

DoC

Department of Commerce (USA)

DoD

Department of Defense (USA)

DOS

Department of Space (India)

DoS

Department of State (USA)

DPI

Dual Pilot Implementation (US/USSR)

DPKOS

Department for Peace-keeping Operations

DPRK

Democratic People’s Repubic of Korea

DRDL

Defence Research and Development Laboratory (India)

DRDO

Defence Research and Development Organization (India)

DRS

Data Relay Satellite (ESA)

DSP

Defense Support Programme

DST

Defence and Space Talks (US/Russia)

DT Dual

Trust

EAD

Extended Air Defence

EAGLE

Extended Airborne Global Launch Evaluator

EAR

Export Administration Regulation (USA)

ECCO

Equatorial Constellation Communications

ECOSAT

European Control by Satellite

ECS

European Communication Satellite (ESA)

ECSRC

Executive Committee of the Space Research Council (Pakistan)

ELDO

European Launcher Development Organization

ELINT Electronic

Intelligence

EMFA

Joint-Armed Forces Ministry (Brazil)

EmSC

Emerging Space-Competent State

ENCD

Eighteen-Nation Committee on Disarmament

EOSAT

Earth Observation Satellite Company

ERINT

Extended Range Intercept Technology

ERNO

ERNO Raumfahrttechnik GmbH (Germany)

ERS

Earth Resource Satellite

ERTS

Earth Resources Technology Satellite (USA)

ESA

European Space Agency

ESCS

Emerging Space-Competent State

(9)

ESMON

Earth-to-Space Monitoring Network

ESRO

European Space Research Organization

ETM

Enhanced Thematic Mapper (LANDSAT)

EtSC

Established Space-Competent State

EU European

Union

EURATOM European Atomic Energy Community

EWS

Early Warning System

FOBS

Fractional Orbital Bombardment System

FOC

Faint Object Camera (Germany)

FSA

Free-Standing Agreement (US/USSR)

FTR

Flight Test Range

FY Fiscal

Year

GBI Ground-Based

Interceptor

GBR Ground-Based

Radar

GEM

Guidance Enhancement Missile

GEO Geostationary

Orbit

GEODSS

Electron-Optical Deep Space Surveillance System

GLBM

Ground-Launched Ballistic Missile

GLCM

Ground-Launched Cruise Missile

GOCNAE

Organizing Group of the National Commission for Space Activities

(Brazil)

GP Geneva

Protocol

GPALSs

Global Protection Against Limited Strikes (USA)

GPS

Global Positioning Satellite

GPSCWG

Global Protection System Concept Working Group (US/Russian GPALs)

GSLV

Geostationary Satellite Launch Vehicle

GSTo

Geosynchronous Transfer Orbit

HAWK

Homing All The Way Killer

HEU

Highly Enriched Uranium

HOPE

H-II Orbiting Plane (Japan)

HORUS

Hypersonic Orbital Research and Utilization System

HRV

High Resolution Visible (SPOT)

HTK Hit-To-Kill

(10)

IAEA

International Atomic Energy Agency

IAG

Industrial Advisory Group

IAI

Israel Aircraft Industries

IAVAC

International Agency for the Verification of Arms Control Agreements

IBSS

Infrared Background Signature Survey (SDI)

ICBM

Inter-continental Ballistic Missile

ICJ

International Court of Justice

IDC

International Data Centre

IEC

International Export Certificate

IGMDP

Integrated Guided Missile Development Programme (India)

IIAE

Instituto de Investigaciones Aeronáuticas y Espaciales (Argentina)

IIC

International Import Certificate

IMS

International Monitoring System

INC

International Notification Centre

INCSR

Indian National Committee for Space Research

INF

Intermediate-Range Nuclear Forces (Treaty)

INLC

International Launch-Notification Centre

INPE

National Institute for Space Research (Brazil)

INSAT

Indian National Satellite

IRA

Israeli Space Agency

IRBM

Intermediate-Range Ballistic Missile

IRIS

Indian Remote Sensing Satellite

IRIS

Italian Research Interim Stage

IR-MSS

Infra-Red Multispectral Scanners

IRS

Indian Remote-Sensing Satellite

ISAS

Institute of Space and Astronautical Science (Japan)

ISAS

International Satellite for Ionospheric Studies (Canada)

ISMA

International Satellite Monitoring Agency (French proposal)

ISRO

Indian Space Research Organization

ISSA

International Space Science Academy

ISTS

Institute for Space and Terrestrial Science (Canada)

ITA

Technological Institute of Aeronautics (Brazil)

ITU

International Telecommunication Union

(11)

JEM

Japanese Experiment Module

JMA

Japan Meteorological Agency

JSLC

Jiuguan Satellite Launch Centre (China)

JTAGS

Joint Tactical Ground Station

KEK

Kinetic Energy Kill

KSC

Kagoshima Space Centre (Japan)

LANDSAT Land use satellite (NASA)

Laser

Light amplification by simulated emission of radiation

LEAP

Light Exo-Atmospheric Projectile

LEO

Low Earth Orbit

LIGHTSATs Light Satellites

LISS

Liner Imaging Self-Scanner

LittleLEO

Little Launcher of Low Earth Orbit (UK)

LLV

Lockheed Launch Vehicle

LM Long

March

LPSC

Liquid Propulsion Space Centre (India)

LPSC

Liquid Propulsion Systems Centre (India)

MAAI

Ministry of Aeronautics and Astronautics Industry

MAc

Mass Accelerators (ASAT weapons)

MAD

Mutual Assured Destruction

MAI

Ministry of Aerospace Industry (China)

MARECS

Maritime European Communications Satellite (ESA)

MBB

Deutsche Aerospace (Germany)

MCB

Manoeuvrable Collision Bodies (ASAT weapons)

MDAHG Missile

Defence

Ad Hoc Group

Mdr

Mass Drivers (ASAT weapons)

MEADS

Medium Extended Air Defence System

MECB

Brazilian Complete Space Mission

MERCOSUR Southern Common Market

MIC

Ministry of Industry and Commerce (Israel)

MIRV

Multiple Independently-targeted Re-entry Vehicle

MIT

Massachusetts Institute of Technology

MITI

Ministry of International Trade and Industry (Japan)

(12)

MOA

Memorandum of Agreement

MoD

Ministry of Defence (Israel)

MOE

Ministry of Education (Japan)

MOPT

Ministry of Post and Telecommunications (Japan)

MOS

Marine Observation Satellite (Japan)

MOST

Ministry of Post and Telecommunications (Japan)

MOT

Ministry of Transport (Japan)

MOU

Memorandum of Understanding

MPLMs

Mini Pressurized Logistics Modules (Italy)

MRV

Mutual Re-entry Vehicle

MS Multispectral

MSDS

Marconi Space and Defence Systems (UK)

MSS

Marconi Space Systems (UK)

MSS

Mobile Servicing System (Canada)

MSS Multispectral

Scanners

MTCR

Missile Technology Control Regime

MTOPS

Million Theoretical Operations Per Second

MURST

Ministry for the Universities and Science and Technology (Italy)

NAC

North Atlantic Council

NACC

North Atlantic Cooperation Council

NADC

NATO Air Defence Committee

NAL

National Aerospace Laboratory (Japan)

NASA

National Aeronautics and Space Agency (USA)

NASDA

National Space Development Agency (Japan)

NASP

National Aero-Space Plane (USA)

NATO

North Atlantic Treaty Organization

NDRE

Norwegian Defense Research Establishment

NGSV

Argentinian New Generation Space Vehicle

NIPR

National Institute for Polar Research (Japan)

NMD

National Missile Defense (USA)

NMTs

National Technical Means of Verification

NNRMS

National Natural Resources Management System (India)

NOAA

National Oceanic and Atmospheric Administration (USA)

(13)

NORAD

North American Aerospace Defense Command (USA)

NORSAR

Norwegian Seismic Array

NPA

Non-Proliferation Agency (US Senate bill)

NPS

Nuclear Power Source

NPT Non-Proliferation

Treaty

NPWG

Non-Proliferation Working Group (US/Russian GPALs)

NRC

Nuclear Regulatory Commission (USA)

NRSA

National Remote Sensing Agency (India)

NRSC

National Remote Sensing Centre (China)

NSC

Norwegian Space Centre

NSG

Nuclear Suppliers Group

NSP

National Space Plan (Italy)

NST

Nuclear and Space Talks (US/Russia)

NTC

Noshiro Testing Centre (Japan)

NTMs

National Technical Means

NTNF

Royal Norwegian Council for Scientific and Industrial Research

NTWD

Navy Theatre-Wide Defence

NUPI

Norwegian Institute of International Affairs

NWFZ

Nuclear Weapon-Free Zone

OECD

Organization for Economic Co-operation and Development

OPANAL

Agency for the Prohibition of Nuclear Weapons in Latin America and the

Caribbean

OREX

Orbital Re-entry Experiment

OS Outer

Space

OSCE

Organization for Security and Cooperation in Europe

OST

Outer Space Treaty

OTH-B Over-The-Horizon-Backscatters

PAC

PATRIOT Advanced Capability

PAN Panchromatic

PARCS

Perimeter Acquisition Radar Attack Characterization System

PAROS

Ad Hoc Committee on the Prevention of an Arms Race in Outer Space

Committee

PAXSAT

Canadian Peace Satellite

(14)

PFS Pre-Feasibility

Study

PLO

Palestinian Liberation Organization

PLS

Personnel Launch System

PNDA

E

Brazilian National Policy o

n the Development of Space Activities

POC

Point of Contact

PRL

Physical Research Laboratory (India)

PSLV

Polar Satellite Launch Vehicle (India)

PTBT

Partial Test-Ban Treaty

QRP

Quick Reaction Programme

R&D

Research & Development

RADA

RSAT

Radar Satellite (Canada)

RAMOS

Russian American Observation Satellites

RECOSI

Regional Cooperation for Satellite Imagery

RoK

Republic of Korea

ROTE

X

Robotics Technolog

y Experiment (Germany)

RPM

Retro Propulsion Module (Germany)

RS-1/2

/3

Rohini Satellite-1, 2 or 3 (India)

RSMA

Regional Satellite Monitoring Agency

SAC

Space Application Centre (India)

SAC

Space Activities Commission (Japan)

SAC-B

Argentinean Scientific Applications Sa

tellite-B

SAD

Space Activity Division (Sweden)

SALT

Strategic Arms Limitation Treaty

SAM Surface-to-Air

Missile

SAR

Synthetic Aperture Radar

SBC

Sanriku Balloon Centre (Japan)

SBIRS

Space-Based Infrared System

SBM Security-Building

Measures

SBT Sea-Bed

Treaty

SCD

Data Collecting Satellite (Brazil)

SDI

Strategic Defense Initiative (USA)

SDIO

Strategic Defence Initiative Organiz

ation

SDP

Space Development Programme (Japan)

(15)

SERE

B

Society for the Study and the Realiza

tion of Ballistic Vehicles

SFU

Space Flyer Unit (Japan)

SHAP

E

Supreme Headquarters of

Allied Powers in Europe

SHAR

Sriharikota Space Centre (India)

SIPA

Satellite Image Processing Agency (France)

SIPRI

Stockholm International Peace Research Institute

SL Space

Launcher

SLBM

Submarine-Launched Ballistic Missile

SLV

Satellite Launch Vehicle

Smi

Space Mines (ASAT weapons)

SMT

S

Space and Missile Tracking Sys

tem

SNAE

National System of Space Activities (Brazil)

SNSB

Swedish National Space Board

SOI

Statement of Intent

SPAS

Shuttle Pallet Satelli

te (Germany)

SPOT

Earth Observation Satellite (France)

SR Sounding

Rocket

SRAM

Short-Range Attack Missile

SRC

Space Research Council (Pakistan)

SROS

S

Stretched Rohini Satellite Series (In

dia)

SSC

Space Surveillance Centre (USA)

SSC

Swedish Space Corporation

SSOD

United Nations Special Sessi

ons on Disarmament

SSR

Remote Sensing of the Earth (Brazil)

SSV

Single Stage Version

STA

Science and Technology Agency (Japan)

STAR

S

Strategic Tactical Airborne Range System

START

Strategic Arms Reduction Talks Treaty

STFNP

Special Task Force on Non-Proliferation (US Senate bill)

STRV

Space Test Research Vehicle

STS

Space Transportation System

SUPA

RCO

Space and Upper Atmosphere

Research Commission (Pakistan)

SYRACUSE Système de Radio-Communication Utilisant un Satellite (France)

(16)

TACDAR

Tactical Data & Related Applications

TACS

Theatre Air Control System

TBMD

Theater Ballistic Missile Defense

TCWG

Technology Co-operation Wo

rking Group (US/Russian GPALs)

TD Theatre

Defence

TEL

Light Space Transport (Brazil)

THAAD

Theater High Altitude Area Defence

TM Thematic

Mapper

TMD

Theater Missile Defense

TNCD

Ten-Nation Committee on Disarmament

TOAM

Tactical Air Operations M

odule

TSS

Tromsø Satellite Station (Norway)

TT&C

Tracking, Telemetry, and Control

TT&T

Telemetry, Telecommand & Trackin

g

UAV

Unmanned Air Vehicle

UDSC

Usuda Deep Space Centre (Japan)

UNDC

United Nations Disarma

ment Commission

UNDDA

United Nations Department for Dis

armament Affairs

UNIDIR

United Nations Institute for Disarmament R

esearch

UNITRAC

E

International Trajectography Centre (France)

UNOOA

United Nations Office for Outer Space Affairs

UNPO

United Nations Peace Operation

UNSCOM

United Nations Special Commission

UOES

User Operational Evaluation System

USSR

Union of Soviet Socialist Republics

Uvs Unmanned

Vehicles

VAP

Vehicle Evaluation Pay-load

VLS

Satellite Launching Vehicle

VNIR

Visible and Near Infra-Red

VSAT

Very Small Aperture Termin

als

VSSC

Vikram Sarabhai Space Centre (India)

WA Wassenaar

Arrangement

WEU

Western European Union

(17)

WFI Wide-Field

Imager

WMD

Weapons of Mass Destruction

WPO

Warsaw Pact Organization

WSO

World Space Organization

XSLC

Xichang Satellite Launch Centre (China)

() Unverified

data

[] Doubtful

estimation

..

Data unavailable or inapplicable

(18)

1. Outer Space Technology Transfer: The Present

Dilemma

The right of any State to develop outer space technologies, be they launching capabilities, orbiting satellites, planetary probes, or ground-based equipment, is, in principle, unquestionable. In practice, however, problems arise when technology development approaches the very fine line between civil and military application, largely because most the technologies can be used for dual military and civil purposes. This dichotomy has raised a series of political, military, and other concerns which affect the transfer of outer space technologies in different ways, and particularly between established and emerging space-competent States. Accordingly, for many years several States have sought ways and means to curb the transfer of specific dual-use outer space technologies, particularly launcher technology, while still allowing some transfer of these technologies for civil use.

However, controlling outer space technologies has never been an easy task. It has become increasing complex, not least because of the fundamental changes in international relations which have and continue to occur in the 1990s. Indeed, the nature and potential use of outer space and related technologies are such that, collectively or individually, States are often faced with the dilemma of having to choose between what could be an illegal transfer and permissive; between what could be a genuine civil use application at a certain point in time—but could be used for military purposes in another—and applications which are overtly or implicitly military in character. For example, the development of space weapons for offensive uses can be seen as a threat to international security and peace, despite the fact that they may, in actual fact, be components of defensive or deterrent strategies. Similarly, while the development of space launcher capability is not perceived as such a threat, access to this technology—because it could contribute to the acquisition of ballistic missiles—is often considered as detrimental to regional and/or global stability.

A further factor is the changing collective perception of what constitutes military space. For example, the development of military-grade satellite technologies is often perceived as the acquisition of military technologies because, inter alia, military-grade satellite technologies have been traditionally used by some States to support their military doctrines. At present, international market access to military-grade satellite data is becoming more common and new civil and security-related applications emerging. Joint manufacturing ventures are also on the increase since they are now considered politically attainable, militarily desirable, and economically viable. Moreover, military outer space activities—whether space-based or not—are also used within the framework of United Nations Peace Operations (UNPOs), or as part of the security strategies of regional military alliances.

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Thus, the question of which specific aspects of outer space technology transfer could constitute a threat to international security acquires greater relevance. To answer this and related questions, it is necessary to consider complex fundamental issues, evaluate the political, military, technological, and economic ramifications of this matter, and assess the purposes and situations for which the transfer of outer space technologies are intended.

Nevertheless, the development of outer space technologies continues in a quagmire of conflicting interests and technology transfer control rationales. First, there are political-military considerations where a State’s decision to develop military outer space or related applications can be assessed not only as a function of perceived levels of threat to its security, but also as a need to respond to or leap ahead of potential technological innovations. Second, are the fundamental conceptual differences in appreciation among States of the right to possess different weapons and weapons systems for defensive or offensive purposes. Has a State which possesses military space technologies the right to restrain another from obtaining such capabilities? This is not a question limited to the dual-use issue. It has been at the heart of the haves/have nots debate in all the non-proliferation talks (nuclear, chemical, and biological issues and, to some extent, certain conventional weapons as well) for decades. Third, there are the economic implications, whose impact is perhaps the least well-known and debated of all. These economic implications include reluctance on the part of some States and/or organizations to promote increased competition in outer space manufacture. Concomitantly, the very competitive space industry exercises a measure of control on technology transfers via its industrial secrecy policies and market advantage strategies.

In the midst of these and other interests the transfer of dual-use outer space technologies is caught between selective control regimes on the one hand and the absence of a universal agreement—of mutual interest—on the other. Dual-use technology transfers do not take place in a vacuum. Presently, they are affected by the aftermath of the end of the Cold War and the break-up of the Soviet Union, and the search for a new world order. Additionally, since major nuclear and chemical disarmament efforts are underway, non-proliferation will receive increased attention in future security debates— notably with respect to the strengthening of the Biological and Toxin Weapons Convention, new nuclear- and delivery systems-related (e.g., missiles and other rockets) agreements. The new era has required a reassessment of national priorities related to international security which affects the way global and regional geopolitical policies are conceived. Such a reassessment has led to a greater interest in civil-related issues, an approach which is more amenable to cope with development and environmental problems.

While this new political direction may eventually stimulate a constructive turn in international relations, there is still an unanswered question: how can international security and peace in both the short and the long term be ensured? Central to this concern is the transfer of dual-use outer space technologies in general, and of delivery-vehicles in particular. For the time being, discussions on dual-use outer space technologies lack creativity; political will to promote diplomatic initiatives is also

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lacking. This situation does not necessarily further international security, nor does it foster co-operation in the civil use of dual-use outer space applications.

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2. Thesis Rationale and Hypothesis

It is in the specific context of the impact on international security caused by the transfer of dual-use outer space technologies that the rationale of the present thesis is argued. Currently, the relationship between the suppliers and the recipients of these technologies is based on selective control regimes which, in many instances, give rise to conflicting political situations. In the main, control regimes have been established to curb the development of ballistic missiles, military reconnaissance satellites, and other weapons and weapon systems. The argument could also be made, however, that economic considerations have also stimulated these control regimes. Polemics aside, the problems caused by these regimes are such that there is an urgent need to rethink their mode of implementation, added to which is the fact that control regimes have also hindered, both directly and indirectly, the development of certain civil-oriented space programmes.

The hypothesis of this document is that the interests of both suppliers and recipients in the transfer

of dual-use outer space technologies can best be served not through selective control regimes but through joint co-operative measures, because it is the most efficient way to control civil-use of outer space technologies, while at the same time ensuring their transfers. In order to prove this hypothesis,

this document will therefore:

1. appraise the specific, progressive steps required to achieve co-operation between suppliers

and recipients of space technologies;

2. assess the measures that would offer more transparency in technology transfer and thus

lead to greater predictability of the end-use; and

3. examine measures which could build-up confidence and security among States in so far as

outer space technologies are concerned.

In developing this rationale, this thesis does not undertake a detailed analysis of all outer space and related technology transfers, since it would be a tedious exercise which falls outside the scope of this paper’s main objective. Rather, the discussion is limited to an appraisal of the relationship between technology-supplier States—i.e., those which reached competence in outer space activities between the 1950s and the 1970s—and potential recipient States—which are currently developing their first generation of indigenous space launchers, satellites, and/or ground stations. The debate in this document starts in the dawn of the space age and ends in the year 2000.

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3. Methodology and Proposed Solutions

It is clear that the objectives set forth above are not easy to reach. After all, the dual-use debate is not new and its complexities are also quite well known. It is therefore necessary to first clarify what outer space technologies actually are and what their dual use may entail. Understanding the technical intricacies is essential: for instance, are space launchers ballistic missiles? Unfortunately, the importance of the answer to this question is not always appreciated, for in it lies some of the fundamental reasons for controlling access to rocket technologies. Equally necessary is a survey as to which countries are most likely to export or import outer space technologies. Such an exercise would also be valuable in identifying countries which have assigned their outer space technologies to the military sector, since they are often the strongest proponents of control regimes related to technology transfer.

In view of the need to evaluate and clarify the political and strategic implications of access to outer space technologies on international security, this thesis highlights the consequences that the dual use of outer space technologies can have on (a) the spread of weapons technologies and (b) the military use of space assets. More specifically, it appraises and clarifies some of the ramifications which are often discussed in the context of the non-proliferation debate. It also pays particular attention to launching vehicles capable of carrying nuclear or other payloads of mass destruction and the space component of such issues as Earth-orbit satellites versus space probes. Reconnaissance satellites are especially pertinent since their role in the next century has yet to be fully assessed and appreciated.

At the same time, the focus of this thesis is an examination of several existing and future technology transfer control regimes, although the detail is narrowed to more space-related relevant instruments and arrangements. First, it is important to learn more about technology transfer issues and the role of national legislation. For example, central to the control regime debate is the discussion on the evolution, or lack, of national legislation covering dual-use outer space technologies, as well as a discussion on their orientation and scope. Which countries have developed or are developing legislative measures in this area? Are legislation on control regimes legally sound and implementable in practice, and to what extent? Second, at a time of fundamental change in the nature and order of international relations, the wisdom of ad hoc control regimes must not escape scrutiny. Although experts are very much aware of these problems, the future of control regimes remains uncertain, so what are their potential implications for international security? Hence, a reassessment of the problems surrounding existing control regimes must be made – both in terms of their foreseeable improvement and/or a possible new universal multilateral agreement, and within the context of an uncontrolled regime.

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This further argues the need for new international mechanisms to safeguard the transfer of dual-use outer space technologies, while not fuelling proliferation opportunities for weapon systems. This argument is not just ideological thinking. It could constitute the basis of a policy that could be implemented if certain specific initiatives are taken. To build confidence between suppliers and recipients of outer space technologies, adhesion to bilateral agreements on space technologies and activities, arms limitation agreements on weapons of mass destruction, and other measures would offer increased transparency in the development of outer space activities as well as higher levels of predictability. Of course, the roles of both suppliers and recipient States in unilateral, reciprocal measures would have to be carefully evaluated. Concession issues would need to be given the highest priority in order to improve predictability and the creation of crisis management mechanisms.

Multilaterally, there should also be agreement to establish a dialogue mechanism between suppliers and recipients, to enable mutual political objectives to be complemented by compliance and enforcement procedures. Central to the debate would be a discussion of fundamental, practical questions. For example: is it appropriate to undertake multilateral negotiations? If so, in what form and at what type of forum should they take place? Whether a World Space Organization (WSO) could solve outer space technology transfer problems also finds legitimacy in this context.

However, scrutinizing ways of creating new relationships between suppliers and recipients in the transfer of dual-use outer-space technologies can easily be a zero-sum-game endeavour. The challenge is to instigate impartial and innovative thinking. Moves favouring co-operation simply for the sake of ensuring the transfer of dual-use technologies are not the answer here! Moreover, while international organizations have their role, they are not a panacea, as the comprehensive test ban treaty discussions have shown. The costly, complex exercise that led to the Chemical Weapons Convention (CWC) should not be taken as a precedent.

In conclusion, the question of whether there should be a better restructuring of outer space technology transfer would now appear to be irrelevant without a better understanding of the present relationship among States on the vital outer space sector of the security debate. The quest for improved relationships in respect of technology transfer and dual use must first start with an assessment of the political, military, technical, and economic implications of outer space technologies. Any such assessment must therefore consider the relevance that access to these technologies has for different geopolitical situations. Only by co-operation can the supplier/recipient relationship be established in a sound, durable manner. However, any such co-operation must be reinforced by agreements to ensure transparency and predictability on issues which directly affect the security and development of individual States or groups of States.

The right of any State to develop outer space technologies is, in principle, unquestionable. In practice, problems arise when technology development approaches the very fine line between civil and military application, largely because most the technologies can be used for dual military and civil purposes. This dichotomy has raised a series of political, military, and other concerns which affect the transfer of

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outer space technologies, and particularly between established and emerging space-competent States. Accordingly, several States have sought means to curb the transfer of specific dual-use outer space technologies, particularly launcher technology, while allowing some transfer of these technologies for civil use. This document argues that the interests of both suppliers and recipients States can best be served not through selective control regimes but through joint co-operative measures, because it is the most efficient way to control civil-use of outer space technologies, while at the same time ensuring their transfers.

Part I

Dual-Use Outer Space Technologies:

The

Terminology

The meaning and scope of certain terms, many of which are used interchangeably to describe specific objects and behaviours in the transfer of dual-use technologies can confuse the experienced reader just as much as the novice. Mutual understanding of these terms is therefore crucial in understanding the issues related to this paper. The purpose of Part I is therefore to define the terminology to be used below. Among the many terms with multiple meanings are technology transfer, dual use, outer space (as distinct from air space), ballistic missile, delivery vehicle, space launcher and sounding rocket.

There is also a need to explore the latest developments in capabilities and the identification of different categories of competence. The question of who does what in outer space will accordingly be addressed at some length. A description of what are called Established Space-Competent (EtSC) States

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is also appropriate, not only because of these countries’ capability to manufacture space equipment, but also because of their capacity to supply outer space technology to the international market.1

However, it is not enough to describe the EtSC States alone. Hence, the Emerging

Space-Competent (EmSC) States, known as technology-recipient States, are also identified. The

relationships, routes, and progress of EmSC States in their quest for outer space capability do not necessarily resemble those of EtSC States, although the past, present, and prospective growth of their national space programmes are unquestionably interwoven. In many instances such progress is an essential factor in the technology transfer debate. This is particularly true of the actual and potential military capabilities of EmSC States.

1/

In this paper, capability means the ability of a State, organization, or institution to put

together the administrative (organizational), industrial, and financial R&D techniques to

organize and finalize given systems or components, such as the design, manufacture, and the

ability to deploy and operate these systems and components.

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Chapter 1: Definition of Terms

The transfer of dual-use outer space technology is such a vast subject that an entire thesis could be devoted to its terminology alone. However, for obvious reasons, the present paper will focus on the meaning of technology transfer and dual use, describe how these terms are applied in the context of outer space, and examine how dual use can be effectively identified among different applications.

A. Technology Transfer

The term “technology transfer” may be used in a variety of circumstances because there is little agreement among experts on its actual meaning. While some experts contend that a clear-cut meaning can be identified, at least one other school of thought argues that the term “technology transfer” is meaningless. There may be some justification for the latter argument since technology transfer could be used, in a general sense, to imply the movement of technology from a supplier to a recipient. This may seem to be an oversimplification, but it is actually quite a complex statement. First, those involved in transfer can be individuals, companies, States, or any other type of enterprise. This complicates the issue in that “technology transfer” defines neither the supplier nor the recipient, thus creating an “identity” problem when the issue of legal responsibility has to be addressed.

A further complication is the fact that the word “technology” is itself vague. Is it an abstract concept or can it be identified as a tangible asset? The answer is not necessarily readily evident. A “grey area” between the two concepts would provide a greater degree of flexibility in definition according to the circumstances at stake. For instance, a transfer could involve complete or selective movement of know-how regarding a given system, manufacturing equipment, finished product, or service (see Diagram I.1.A). As the Diagram illustrates, technology transfer can also affect a prospective recipient’s increased capability to become autonomous and, therefore, also become, in its turn, a supplier in the future. However, it is also important to note that mere movement of goods or services may not necessarily enable the recipient to access the technology. For instance, a recipient may engage in technology transfer but unable to absorb it because of insufficient scientific, human, financial, or other fundamental technological resources. Thus, “technology transfer” would not apply in such a case—although it could be argued that an attempt to transfer technology may have been made. Even if there is no difficulty in accepting this assumption, there will still be a problem in regard to ability to identify and distinguish the movement of technology and assets from non-transfer-related events.

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image003

To reach a clear definition of technology transfer, three other issues must be addressed: (1) the conditions in which it can occur; (2) the ability the supplier/recipient to provide/absorb transferred assets so as to permit their coherent use; and (3) the fundamental objectives behind the decision the supplier/recipient to transfer/acquire the technology. In the first and second instances, it is difficult to estimate the transfer conditions because the flow of technology between a supplier and a recipient may not be easily identifiable. For example, in a joint-venture, the R&D of a given system may depend not only on a supplier’s input but also—and to varying degrees—on that of a potential recipient. In such an example, the concept of sharing technology R&D may also be added to the definition as part and parcel of the technology transfer process.

Additionally, input should not be characterized only in such terms of abstract participation as the provision of knowledge, but also in terms of human, financial, and other investment resources – which adds to the difficulty of identifying technology transfers. In the third instance, the decision to acquire technology—as distinct to undertaking indigenous R&D—is often closely linked to a need to decrease programme costs and development time, while at the same time widening the scope of potential applications.2

Therefore, it seems that, to be pertinent, a working definition of “technology transfer” for the purpose of this paper has to take three factors into consideration – namely:

(a) the existence of asset movement, including knowledge and services,

between two or more protagonists;

(b) the possibility that a recipient may employ the transferred assets either to

produce finished products or to provide services without the assistance of the

original supplier; and

(c) the ability of a recipient to have access to a given technology in a manner

that would save time, financial investment, and other resources.

2/

For some decision-makers, the issue of cost and time seems to be a major motivation to

engage in technology transfer agreements and avoid indigenous R&D developments. For

example, the main argument in the case of outer space applications is that physical, chemical,

and other natural laws, as well as the many different ways of addressing problems deriving

therefrom, are well known. One of the main objectives is the lack of adequate financing and

time (in terms of years or decades) for the development of a space programme: therefore,

technology transfer is seen as an alternative solution.

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In conclusion, for the purpose of the present discussion, the term “technology transfer” is

neither meaningless nor vague. On the contrary, it carries a strategic vision and responds to

specific criteria.

B. Outer Space and Dual-Use Technologies

In the light of the above definition, the transfer of outer space technologies would naturally

refer to the movement of outer space assets, applications, and services between suppliers and

recipients. However, outer space is an environment and it is not particularly obvious, a priori,

how the outer space environment fundamentally relates to technology transfer. There is no

precise, universally agreed, legal, technical, or political definition of the boundaries separating

outer space from air space or from deep space, nor is there any agreement in diplomatic

and/or scientific quarters of the term “outer space” itself.

3 One of the major obstacles in defining

the boundary between air space and outer space is the difficulty in obtaining agreement on the quantifiable physical parameters dividing the two environments. Moreover, this boundary is not necessarily stable and may, at some point in time, be affected by atmospheric changes and/or physical phenomena. However, for the purpose of the present discussion, a working definition of outer space could be as follows:4

[o]uter space is all of the space surrounding the Earth where objects

can move in at least one full orbit around the Earth without artificial

3/

For lengthy discussion of different possible definitions of outer space, see, inter alia,

“The Question of the Definition and/or the Delimitation of Outer Space,” Official Records of

the General Assembly, A/AC.105/C 2/7, 7 May 1970; “The Question of the Definition and/or

the Delimitation of Outer Space,” Official Records of the General Assembly, A/AC.105/C 2/7,

21 January 1977; “Matters relating to the Definition and/or Delimitation of Outer Space and

Outer Space Activities, Bearing in Mind Inter Alia, Questions Related to the Geostationary

Orbit,” Official Records of the General Assembly, A/AC 105/C.2/L.139, 4 April 1983;

Bhupendra Jasani (ed.), “Introduction,” I, Problems of Definitions, Where Does Outer Space

Begin?, in Peaceful and Non-Peaceful Uses of Space: Problems of Definition for the

Prevention of an Arms Race, UNIDIR, New York: Taylor & Francis, 1991, p. 19; Caesar

Voûte, “Boundaries in Space,” in Peaceful and Non-Peaceful Uses of Space: Problems of

Definition for the Prevention of an Arms Race, op. cit.

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propulsion systems according to the laws of celestial mechanics,

without being prevented from doing so by the frictional resistance of

the Earth’s atmosphere. It extends from an altitude above the earth of

approximately 100 km upwards.

Under this working definition, any technologies which contribute directly to applications in such an environment could be considered as outer space technologies: e.g., rocket boosters, satellites and their components, and Earth-based control and tracking systems. Equally, other technologies contributing to these and other outer space applications in a less direct manner could be considered as “related” outer space technologies — for instance, the technologies of systems and sub-systems which could be used instead of the traditional means of manufacturing and operating space devices. In consequence, the following questions may then be raised: (1) what are dual-use outer space technologies, and (2) how can they be distinguished from single-use technologies? Are operational interactions and technical similarities the only criteria to differentiate dual- from single-use technologies? Or are there other more conceptual and less technical reasons?

The term dual is used in its generic sense to denote the mathematical number “two”. When used in relation to an operative verb such as use, “dual” means more than one employment, nature, or characteristic of a given object or method, or any other word it qualifies. More specifically, in the context of outer space technologies, dual use can be defined as being a usage which has both civil and military employment, whether proven or potential. In a more general sense, dual use also embraces weapon technologies and their systems and sub-systems, in any of their different basing modes: ground-based—fixed or mobile, ship-mounted, air-mounted, and space-based. However, while there are a great variety of weapon-specific systems that could be associated with outer space, it is the non-weapon technology that could be employed for military purposes which is the most difficult to define. For example, in rocketry, the line differentiating booster technologies from ballistic missiles is rather fine. It is a core issue in international security debates. Indeed, it is often thought that the possession of the former is a passport to obtaining the latter. However, rocketry technology is only one component of the dual-use debate. It is therefore important to understand the dual-use nature of both artificial satellites5 and rocket/satellite Earth-based tracking technologies. Here too, the line between

civil and military technologies is difficult to draw. One may therefore question how these technologies can be identified and also, equally importantly, how they have been employed in terms of dual use. The discussion which follows is an attempt to illuminate these issues.

5/

The term artificial satellites (satellites hereafter) refers to active or non-active man-made

objects in outer space. It therefore includes man-made space debris, but excludes other objects

in outer space such as meteorites.

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C. Space Booster or Ballistic Missile Technologies?

Different launch vehicles may provide distinct, diverse applications and three major categories of carrier rockets using outer space technologies can be identified: (a) sounding rockets, (b) space launchers, and (c) ballistic missiles. While the first two rockets are essential to the space boosters (or space launching vehicles) used for the exploration of outer space, the BM is propelled into outer space with the intent to use that environment only as a pathway to its final destination back into the Earth’s atmosphere—with, however, the exception of an attack on satellites such as Anti-Satellite (ASAT) weapons.

Sounding rockets are usually employed for scientific studies and provide the capability to conduct

endo-atmospheric and, more importantly, exo-atmospheric experiments6—the latter providing limited

access (a few minutes) to microgravity.7 These rockets usually have a range less than 1000 km and

most have a single solid fuelled-propelled body (see examples in Photos I.1.1 and I.1.2). In most cases, their trajectories are designed in such a way that, via its parachute, the payload returns to the vicinity of the launch pad, thus allowing the payload-bay and its scientific equipment to be recuperated and perhaps reused for other missions.

Photo I.1.1: Example of a Solid-Fuel Graphite Fibre Rocket Motor

image004

Courtesy the US DoD

Photo I.1.2: Example of a Solid-Fuel Motor Test Fire

image005

Courtesy the US DoD

As may be seen from Photo I.1.3, sounding rockets are intended to carry experimental scientific experiment equipment in their payload-bay or to conduct experiments themselves. Different signals from experiments provide Earth stations with data derived from devices in the payload-bay, such as

6/

Endo-atmospheric launchers are vehicles designed to boost a payload up to the limits of

the atmosphere

generally considered as altitudes below 100 km. In contrast,

exo-atmospheric launchers are vehicles capable of boosting a payload above the altitude of 100

km.

7/

Microgravity is the quasi-total absence of weight produced when a spacecraft orbits

around the Earth. This phenomenon is created by an equilibrium between the spacecraft’s

gravitational and centrifugal forces.

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visual and parametric observation of experiments conducted during the endo-atmospheric and/or exo-atmospheric phases of the flight. This allows scientists in Earth-based stations to have real-time access to the experiments and the possibility of transmitting experiment-related telecommand signals8 to the

vehicle’s experimental scientific equipment.

Photo I.1.3: Example of Sounding Rocket Payload Bay

image006

Courtesy of MBB/ERNO Orbital Systems & Launcher Division

Space launchers are, however, technologically more complex and financially more demanding than sounding rockets. Their technical characteristics and mission functions are also different, because space launchers are exo-atmospheric rockets which can be used to reach low Earth orbits (approximately 150-500 km), high altitudes such as geostationary9 orbit, and even deep space (over

40,000 km). Thus, there are different types of space launchers for different Earth and transfer orbits. Consequently, launchers designed to reach geostationary and high transfer orbits are more complex to construct than those for low orbits because—assuming the rockets carry equal payloads— considerably higher thrust power is required. Space lunchers can have different body structures and propulsion fuels: some have a single body while others have three to four stages as well as strap-on boosters.10 Usually, strap-on boosters are propelled by solid fuel, while the main body of the space launcher uses a combination of solid- and liquid-propelled motors.11 As shown in Photo I.1.4,

8

Telecommand signals are commands transmitted to the satellite from the ground through a

radiofrequency link.

9

A geostationary orbit, also known as a geosynchronous orbit, is an orbit located nearly

36,000 km above the Equator, where a satellite travels at the same speed relative to a point

situated on the Equator. Thus, satellites in this orbit appear stationary above a specific point

on the Equator.

10

Strap-on boosters are small rockets attached to the body of a larger main rocket to increase

thrust in the initial (boost) phase of launch.

11

Both solid and liquid propellants function as the result of a chemical reaction. See a

discussion by Stephen E. Doyle, Civil Space Systems: Implications for International Security,

UNIDIR, Dartmouth: Aldershot, 1994, pp. 43-45. Doyle also refers to experimental sounding

rockets in the 1920s that were propelled with liquid fuel engines. Other propellants presently

under consideration and development include nuclear and electrical reaction elements.

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fuel motors are structurally more complex and more cumbersome to operate than solid devices. Only a few States are able to manufacture cryogenic propellant, a special high-performance liquid fuel for liquid boosters.12

Photo I.1.4: Example of Liquid-Fuel Motor (Japanese H-2 LE-7 engine)

image007

Courtesy of NASDA

Mission space launchers—which are sometimes called expandable launchers—

are rockets which place satellites and manned vehicles into Earth orbits or launch

probes into deep space. They have a greater payload capability than sounding

rockets, although their satellites do not always contain scientific study instruments.

The difference in mission purpose also reflects a difference in the form and size of

the rocket’s payload-bay structure (see Photos I.1.5 and I.1.6). In addition, the type

of trajectory of space launchers also differ from those of sounding rockets, with the

additional particularity that space launchers are not usually intended to return to the

Earth: they either burn-up when they re-enter the Earth’s atmosphere or remain in

outer space as space debris. There are, however, vehicles that carry astronauts into

outer space and are designed to have their manned capsulae re-enter the Earth’s

atmosphere and then be parachuted into the sea or onto the ground as well as the

capability to perform regular aircraft-like landings.

Photo I.1.5: Example of Space Launcher Payload-bay-I (Preparation before

closing the fairing)

image008

Courtesy of Arianespace

Photo I.1.6: Example of Space Launcher Payload-bay-II (Satellite composite mating

on to the launcher)

image009

Figure

Table I.2.2: Selected Sounding Rocket/Space Launcher  Technology Development by EtSC States: Level-I Countries
Table I.2.4: Selected Sounding Rocket/Space Launcher Technology Development by EtSC  States: Level-II Countries
Table I.2.5: Select Sounding Rocket/Space Launcher  Technology Development by EmSC States
Table I.2.7: EmSC States – Satellite and Related Manufacturing Capabilities ¶
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