HYPERSONIC BOOST-GLIDE SYSTEMS AND HYPERSONIC CRUISE MISSILES - SIPRI
HYPERSONIC BOOST-GLIDE SYSTEMS AND HYPERSONIC CRUISE MISSILES
Challenges for the Missile Technology Control Regime
kolja brockmann and dmitry stefanovich
STOCKHOLM INTERNATIONAL PEACE RESEARCH INSTITUTE
SIPRI is an independent international institute dedicated to research into conflict, armaments, arms control and disarmament. Established in 1966, SIPRI provides data, analysis and recommendations, based on open sources, to policymakers, researchers, media and the interested public.
The Governing Board is not responsible for the views expressed in the publications of the Institute.
GOVERNING BOARD
Ambassador Jan Eliasson, Chair (Sweden) Dr Mohamed Ibn Chambas (Ghana) Ambassador Chan Heng Chee (Singapore) Jean-Marie Gu?henno (France) Dr Radha Kumar (India) Dr Patricia Lewis (Ireland/United Kingdom) Dr Jessica Tuchman Mathews (United States) Dr Feodor Voitolovsky (Russia)
DIRECTOR
Dan Smith (United Kingdom)
HYPERSONIC BOOST-GLIDE SYSTEMS AND HYPERSONIC CRUISE MISSILES
Challenges for the Missile Technology Control Regime kolja brockmann and dmitry stefanovich
April 2022
Contents
Acknowledgements
iv
Summary
v
Abbreviations
vii
1. Introduction
1
Box 1.1. The Missile Technology Control Regime
2
2. Hypersonic boost-glide systems and hypersonic cruise missiles
4
Hypersonic speed, manoeuvrability and hypersonic flight trajectories
4
Hypersonic boost-glide systems
6
Hypersonic cruise missiles
7
Drivers and status of hypersonic missile development and proliferation
7
Figure 2.1. True speed by altitude at Mach 5
5
Figure 2.2. Notional trajectories of ballistic missiles, hypersonic boost-glide
6
systems and aeroballistic missiles
Figure 2.3. A cutaway diagram of subsystems packaging of an X-51A scramjet
7
engine demonstrator
Table 2.1. Selected current hypersonic missile systems and development
9
programmes
3. Conventional?nuclear entanglement and MTCR controls on
12
dual-capable delivery systems
Conventional?nuclear entanglement and the case of HGVs and HCMs
12
MTCR controls on nuclear and dual-capable delivery systems
13
4. Applying MTCR export controls to hypersonic boost-glide systems
15
and hypersonic cruise missiles
Definitional ambiguities concerning HGVs and HCMs
15
Current coverage of hypersonic missile technology by the MTCR annex
17
Export controls in the context of civilian space programmes, reusable rockets 20
and crewed spacecraft
Table 4.1. Coverage of selected items required for hypersonic missile systems 16
by the MTCR Equipment, Software and Technology Annex
5. Recommendations
22
About the authors
25
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