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7 - Space Security

Published online by Cambridge University Press:  06 April 2023

Michael Byers
Affiliation:
University of British Columbia, Vancouver
Aaron Boley
Affiliation:
University of British Columbia, Vancouver

Summary

Humanity’s ascent into space began in 1929 when the German Army tested its first rocket, the A-1. But while militaries have always accounted for a large portion of human space activity, their use of the space environment has been constrained by a mutual self-interest in preserving access to it for communications, navigation, reconnaissance, weather forecasting, arms control verification and early warning. In 1962, the ‘Starfish Prime’ nuclear test demonstrated that nuclear explosions in space pose a major and indiscriminate threat to satellites. This prompted the United States and the Soviet Union to negotiate the 1963 Limited Test Ban Treaty, which prohibits nuclear tests in space. This chapter addresses such tensions between the expansion of military capabilities in space and the need to keep space free of direct conflict. The chapter highlights the growing need for a treaty to ban the testing of ‘kinetic’ anti-satellite weapons, i.e. weapons that rely on violent impacts to destroy a satellite and thus create space debris. Although Russia tested such a weapon in November 2021, the very next month the United Nations General Assembly created an ‘Open Ended Working Group on Reducing Space Threats through Norms, Rules and Principles of Responsible Behaviours’. The chapter concludes with an examination of the potentially destabilising effects of an imminent extension of military activities to cis-lunar space, the region between Earth and the Moon, including special Moon–Earth orbits.

Information

Figure 0

Figure 7.1 Gabbard plot showing the apogee–perigee distribution of tracked fragments resulting from India’s ASAT weapon test (destruction of Microsat-R). The approximate altitude of the ISS is shown with a star. The apogee and perigee of Microsat-R just prior to the impact are shown by the downward and upward triangle. Despite the impact occurring at about 280 kilometres, tracked debris extended above LEO (i.e. above 2,000 kilometres in altitude). Note that if an object (such as an operational satellite) is between the red and blue points on this plot, then the debris crosses that object’s orbital altitude.

Figure 1

Figure 7.2 Fraction of USA 193 and Microsat-R debris de-orbited by the number of months after the events. The USA 193 strike took place at an altitude of about 240 kilometres, leading to a relatively rapid loss of the debris, with about 90 per cent of the trackable debris pieces having de-orbited after about two months. In contrast, the Microsat-R strike occurred at about 280 kilometres, leading to much longer-lived debris, with 90 per cent of the debris de-orbiting only after 13 months.

Data: USSPACECOM.
Figure 2

Figure 7.3 Orbital trajectories for 340 pieces of debris from the Russian ASAT weapon test. The debris fragments cover a large range of low Earth orbits, crossing critical infrastructure, including the ISS, the Tiangong Space station and Russian satellites. Moreover, due to the high altitude of the test, all of the debris fragments will pass through the orbital space of the ISS and the Tiangong Space station as they decay.

Figure 3

Figure 7.4 The blue, thick line shows the increase in tracked debris across different altitudes due to the Russian ASAT weapon test. The increase is determined by comparing the USSPACECOM satellite catalogues as of 17 November 2021 (just after the event but before event debris was catalogued) and as of 27 January 2022. The grey, thin line shows the satellite number density as a function of altitude, with Starlink clearly visible. Ten-kilometre bins are used for determining the debris and satellite densities, weighted by the time the object spends within a given altitude bin.

(This figure was made in collaboration with Outer Space Institute junior fellow Sarah Thiele).
Figure 4

Figure 7.5 Ballistic trajectories for three different profiles, showing a depressed, an efficient and a high-altitude trajectory. The blue curve represents the surface of the Earth, while the dot-dashed curve is at an altitude of 100 kilometres and the dotted line is at 300 kilometres.

Figure 5

Figure 7.6 Simplified example of the flight times corresponding to the depressed, efficient and high-altitude trajectories in Figure 7.5. The times are based on Keplerian arcs, so they do not account for the time needed to accelerate the ICBMs to burnout (at around 100 kilometres). Nonetheless, this introduces a timing difference of only one to a few minutes, so the overall scale of the flight times is preserved.

Figure 6

Figure 7.7 Depiction of the FTG-15 interception test. Credit: Laura Grego and David Wright, ‘Incremental Progress but No Realistic Capability: Analysis of the Ground-Based Midcourse Missile Defense Test FTG-15’ (2018) Union of Concerned Scientists Report, online: www.ucsusa.org/resources/analysis-gmd-missile-defense-test-ftg-15.

Reproduced with permission.
Figure 7

Figure 7.8

Figure 8

Figure 7.8

Figure 9

Figure 7.9 A depiction of the Lagrange points for a simple dynamical model involving two massive bodies (M1 > M2), such as the Earth and the Moon. The curves and colours represent constraints on the motion of a third essentially (i.e. by comparison) ‘massless’ body, such as a spacecraft. The image itself is in the ‘rotating frame’; that is, M1 and M2 appear to be stationary even though they are orbiting each other about their centre of mass. X marks the spot for the L1, L2 and L3 Lagrange points. L4 and L5 are shown as the darker ‘islands’ on the plot. An object at exactly those points will appear to be stationary in this rotating frame. In practice, the objects are placed on orbits that oscillate about the L points. This example sets M2 to be one-third the mass of M1 to accentuate the structure (the actual Moon-to-Earth mass ratio is about one to 81).

Figure 10

Figure 7.10 Artist’s illustration of plans for a new DARPA program to develop designs and materials for building large structures in orbit and on the moon.

Image courtesy of Darpa.mil according to the DARPA User Agreement (www.darpa.mil/policy/usage-policy).

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  • Space Security
  • Michael Byers, University of British Columbia, Vancouver, Aaron Boley, University of British Columbia, Vancouver
  • Book: Who Owns Outer Space?
  • Online publication: 06 April 2023
  • Chapter DOI: https://doi.org/10.1017/9781108597135.008
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  • Space Security
  • Michael Byers, University of British Columbia, Vancouver, Aaron Boley, University of British Columbia, Vancouver
  • Book: Who Owns Outer Space?
  • Online publication: 06 April 2023
  • Chapter DOI: https://doi.org/10.1017/9781108597135.008
Available formats
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Save book to Google Drive

To save content items to your account, please confirm that you agree to abide by our usage policies. If this is the first time you use this feature, you will be asked to authorise Cambridge Core to connect with your account. Find out more about saving content to Google Drive.

  • Space Security
  • Michael Byers, University of British Columbia, Vancouver, Aaron Boley, University of British Columbia, Vancouver
  • Book: Who Owns Outer Space?
  • Online publication: 06 April 2023
  • Chapter DOI: https://doi.org/10.1017/9781108597135.008
Available formats
×