Space Debris in Geostationary Earth Orbit
Submitting Institution
University of SouthamptonUnit of Assessment
General EngineeringSummary Impact Type
PoliticalResearch Subject Area(s)
Physical Sciences: Astronomical and Space Sciences, Atomic, Molecular, Nuclear, Particle and Plasma Physics
Medical and Health Sciences: Public Health and Health Services
Summary of the impact
The University of Southampton's research into space debris has made a
vital contribution to space
policy by addressing an issue identified by the United Nations (UN) as
having important
implications for all humanity. This research has played a key role in
advising policymakers "on how
best to manage the orbital environment in a sustainable manner for
generations to come" (page
52, UK in Space, British National Space Centre, 2009). Challenging
prevailing theories,
researchers influenced Inter-Agency Space Debris Coordination Committee
(IADC) Space Debris
Mitigation (SDM) guidelines, resulting in the implementation of
sustainable practices by satellite
operators in Geostationary Earth Orbit (GEO) requiring an investment by
them of an estimated £1
billion since 2008.
Underpinning research
Most people in the world reap the benefits of space systems, driving
revenues from commercial
space products and services to £70 billion in 2011 (40% of the global
space economy). The
biggest demand comes from Global Positioning System devices and
direct-to-home (DTH)
television, but space technology also plays a vital role in responding to
natural disasters that affect
hundreds of millions of people each year. Without space infrastructure,
the ability to manage
humanitarian aid and water resources; to deliver health care, telephone
and internet services in
remote areas, amongst other vital services, would disappear; millions of
people would be adversely
affected.
Within this context, the UN described space debris as one of the top-ten
issues of 2008 having
important implications for mankind, alongside climate change and the
global food crisis
(http://www.un.org/en/events/tenstories/08/spacedebris.shtml).
The UN also released guidelines on
space debris mitigation (SDM) in 2008 and established a Working Group in
2010 to address the
Long-term Sustainability of Outer Space Activities (LTSSA). The LTSSA
Working Group's goal is to
look at measures affecting the safe use of outer space for peaceful
purposes and the benefit of all
nations.
Research on space debris has been conducted at the University of
Southampton since 1990 and
throughout the impact assessment period. The work has been supported by
the Defence
Evaluation and Research Agency (DERA, three studentships, 1992-2001),
QinetiQ, UK Space
Agency and an EPSRC post-doctoral research fellowship, held by Lewis
(1999-2002 [3.1],
subsequently Lecturer). Arguing in 1999 that space debris models are
essential in predicting the
characteristics of the debris environment but that research had focused on
Low Earth Orbit (LEO)
[3.2], Swinerd recognised a need to understand the hazards in High
Earth Orbit (HEO), especially
GEO, which is considered too important and unique an environment to risk
degradation. Active
satellites here account for most of the revenue from commercial space
services. Revenues from
DTH broadcasting and satellite broadband internet services from these
spacecraft were £55 billion
in 2011.
Understanding the GEO debris population was the subject of important
preliminary research
performed in collaboration with DERA [3.3]. This led to the
development of the Debris Analysis and
Monitoring Architecture for the Geosynchronous Environment (DAMAGE) by
Lewis and Swinerd, a
simulation model of the GEO debris environment [3.4]. This model
includes a fast propagator,
enabling studies of millions of orbits [3.5]. In collaboration
with QinetiQ (£40,000 estimate in kind)
and the UK Space Agency (value £186,000), Lewis extended DAMAGE to LEO and
Medium Earth
Orbit (MEO) to enable full LEO-to-GEO analyses. There remain only a
handful of models
worldwide with similar capability to DAMAGE, which is unique in the UK and
provides the technical
basis for policy development. Richard Crowther, Chief Engineer for the UK
Space Agency,
explains:
"The research conducted by the University of Southampton... has been
critical in developing
both national and international policy to address the long term
sustainability and security of
space operations. The outcome of the DAMAGE studies and access to the
expertise of key
individuals at the University of Southampton... enable the UK to
influence policy and technical
development and position UK industry and academia to win leading roles
in programme
opportunities emerging from the European Space Agency and the European
Union."
Serving on the IADC, the inter-governmental agency coordinating worldwide
activities related to
space debris, Lewis used Southampton's DAMAGE simulation tool to assist in
the design of
updates to the IADC SDM Guidelines. In particular, collaborative research
using DAMAGE was
conducted by Southampton with QinetiQ and the US Aerospace Corporation [3.6]
to assess the
importance of the initial shape, or eccentricity, of the orbits used as
graveyards by retired GEO
spacecraft. This work was reported to the IADC and credited in its report
on IADC Action Item (AI)
22.1, GEO Disposal Orbit Eccentricity, as a key motivation for updating
the IADC SDM guidelines.
References to the research
(three key references are indicated using *)
[3.1] Swinerd, G.G., Long-term evolution of the HEO space debris
environment, EPSRC,
October 1999-September 2002, £144,000.
[3.2]* Walker, R., Stokes, P.H., Wilkinson, J., and Swinerd, G.G.,
1999, Enhancement and
validation of the IDES orbital debris environment model. Space Debris, 1
(1), 1-19.
[3.3] Martin, C.E., Lewis, H.G., and Walker, R.J., 2001. Studying
the MEO and GEO space
debris environments with the integrated debris evolution suite (IDES)
model. Proceedings
of the Third European Conference on Space Debris, Darmstadt, Germany. The
European
Space Agency (ESA) Special Publication 473, 351-354.
[3.4] Lewis, H.G., Swinerd, G.G., Williams, N. and Gittins, G.,
2001. DAMAGE: a dedicated GEO
debris model framework. Proceedings of the Third European Conference on
Space Debris,
Darmstadt, Germany. The European Space Agency (ESA) Special Publication
473, 373-378.
[3.5]* Williams, D.N., Swinerd, G.G., Lewis, H.G., and Gittins,
G., 2004. A new fast cloud
propagator for use in the GEO regime. Advances in Space Res., 34 (5),
1181-1187.
[3.6]* Lewis, H.G., Swinerd, G.G., Martin, C.E., and Campbell,
W.S., 2004. The stability of
disposal orbits at super-synchronous altitudes. Acta Astronautica, 55
(3-9), 299-310.
Details of the impact
(numbers in [ ] refer to section 5)
To ensure the sustainability of satellite services, IADC SDM guidelines
published in 2002
recommended retired GEO spacecraft should be manoeuvred to graveyard
orbits above the
geostationary ring. The IADC reported to the UN in 2000 that the shape of
these graveyard orbits
did not need to be circular because altitude variations arising from
elliptical orbits would reduce the
collision probability within the graveyard
(http://www.iadc-online.org/Documents/37th_UN_COPUOS_STSC.pdf).
Lewis was able to use his research findings and capabilities of the
DAMAGE simulation tool to
influence the IADC SDM guideline for disposing of GEO spacecraft. In the
2006 final report on
IADC Action Item (AI) 22.1, GEO Disposal Orbit Eccentricity [5.1],
the analysis by Lewis et al. in
[3.6] and work by the Indian Space Research Organisation (ISRO)
were credited as the key drivers
for updating the IADC SDM guidelines. Both sets of researchers recommended
the graveyard orbit
should be nearly circular with a maximum eccentricity of 0.005. This shape
ensures that retired
spacecraft do not return to the geostationary ring and pose a risk to
active spacecraft there.
According to Luciano Anselmo, the former Head of the Italian Space Agency
Delegation to the
IADC [5.2],
"this `interference' situation occurs more frequently than is
typically assumed, and has definite
costs in terms of control centre resources and eventual avoidance
manoeuvres. The critical role
of the initial eccentricity was therefore confirmed, and the results
obtained by Lewis and
colleagues, due to their level of completeness and detail, offered the
needed guidance to
propose a change of the IADC Mitigation Guidelines."
In the context of work for IADC AI 22.1, some IADC delegations expressed
concern that a
guideline containing a maximum eccentricity requirement was overly
constraining for satellite
operators and proposed manipulating the initial orientation of graveyard
orbits, as an alternative.
By increasing the scope of their investigation for the IADC study and
analysing the evolution of
many possible graveyard orbits using DAMAGE, Lewis et al. demonstrated an
initial `sun-pointing'
orientation was insufficient for long-term stability of the graveyard
orbits in every case. Although
contradicting the analyses performed by some other space agencies, Lewis
argued this was due to
a selection bias. Failure to address this issue correctly could have
allowed some retired spacecraft
to interfere or collide with active spacecraft on the geostationary ring
and pollute the region with
fragmentation debris. The final report of IADC AI 22.1 [5.1]
adopted Lewis et al.'s recommendation
that orbit orientations should be assessed on a case-by-case basis.
Thus, a consensus was reached and the IADC SDM guidelines were updated,
reflecting a more
conservative, maximum orbit eccentricity requirement of 0.003. The updated
guidelines were
published in 2007 and have remained unchanged throughout the REF impact
assessment period
[5.3]. According to Holger Krag, the acting chairperson of IADC
Working Group 4, which
establishes and maintains the IADC SDM Guidelines [5.4],
"The systematic analysis by Lewis of the stability of GEO graveyard
orbit altitudes constituted a
major input to the working group's activities. The recent version of the
guidelines and the
Support Document, which recalls the theoretical background to the
guidelines, build upon
findings in [3.6] and make use of material
gathered in that work."
Compliance with the IADC SDM guideline ensures that valuable "real
estate" in the geostationary
ring is freed for future use, interference with active satellites is
minimised, and collisions resulting in
the degradation of the GEO environment are prevented. Holger Krag
explains, "GEO operators
appreciate such guidance and apply them with increasing success rates as
can be concluded from
[ESA's Report on the Classification of Geosynchronous Objects].
Joanne Wheeler, Partner for
Telecoms and Satellite at CMS Cameron McKenna LLP [5.5], agrees:
"Lewis and the team at Southampton have world-leading experience in
this area and the
reputation for this. A key outcome of their work has been to identify
what measures can be
taken by satellite operators to support the sustainable use of the
geostationary region, given
the challenges presented by space debris risks. This is critical for the
future growth of the UK
and international space sector, which rely on revenues from
communications satellites in
geostationary orbit."
The IADC SDM guidelines also directly influenced ISO 24113 Space Debris
Mitigation
Requirements and ISO 26872 Disposal of Satellites Operating at
Geosynchronous Altitude. Dr
Hedley Stokes, Co-convener of the ISO Orbital Debris Coordination Working
Group explains [5.6],
"The University of Southampton's analysis of GEO spacecraft
post-mission disposal orbits has
provided organisations such as IADC and ISO with extremely valuable data
to assist in the
formulation of international space debris mitigation guidelines and
standards."
In addition, Lewis has informed the public debate over the threats from
space debris, through
evidence given to the June 2013 meeting of the House of Commons Science
and Technology
Committee [5.7], and through a September 2011 interview on the BBC
World News Today
programme broadcast on BBC World News (weekly audience estimated to be 74
million:
http://www.bbc.co.uk/news/world-radio-and-tv-12957296)
[5.8].
In terms of compliance with this IADC SDM Guideline, there are
consequences for GEO satellite
operators: the fuel used to manoeuvre a satellite to a graveyard orbit
would otherwise be used to
maintain satellite operations on the geostationary ring and generate
revenues for around three
months (roughly one-quarter of the yearly station-keeping budget). Dean
Hope, Senior Manager of
Flight Dynamics at Inmarsat [5.9] explains:
"Inmarsat and many other commercial operators now recognise the need
to budget sufficient
propellant onboard spacecraft in order to perform orbit raising at end
of life. This is an
investment that is vital to avoid the possibility of running out of fuel
and drifting through the
GEO arc, thereby increasing the risk of collision and polluting such a
valuable resource with
orbital debris. Inmarsat appreciates the work of Lewis and colleagues,
which has enabled the
IADC and ISO to provide much-needed, precise guidance to spacecraft
operators on end of life
orbit raising. Most recently, in April 2013 and after almost 23 years of
operations, Inmarsat 2F1
was successfully re-orbited to an altitude of more than 400 km above GEO
in accordance with
IADC space debris mitigation guidelines and new ISO recommended disposal
standards."
Based on the fuel requirements, re-orbiting to a graveyard orbit in
compliance with the IADC SDM
guideline requires an investment by satellite operators, equivalent to £16
million of earnings per
satellite [5.10]. According to European Space Agency data, 50 of
79 GEO spacecraft reaching the
end of their operational life between 2008 and 2012 were re-orbited in
compliance with the IADC
SDM guideline resulting in an investment of up to £800 million by the
commercial space service
sector. Based on current re-orbiting rates, an additional 8-18 GEO
spacecraft are expected to be
re-orbited by the end of 2013, increasing the investment to an estimated
£1 billion during the REF
assessment period.
Sources to corroborate the impact
[5.1] IADC AI 22.1 Final Report on GEO Disposal Orbit
Eccentricity, April 2006.
[5.2] Southampton work as driver for update to IADC SDM guidelines:
Istituto di Scienza e
Tecnologie dell'Informazione "Alessandro Faedo", National Research
Council, Italy.
[5.3] IADC Space Debris Mitigation Guidelines, IADC-020-1,
Revision 1, September 2007
(http://www.iadc-online.org/Documents/IADC-2002-01,%20IADC%20Space%20Debris%20Guidelines,%20Revision%201.pdf).
[5.4] Southampton contribution to update of IADC SDM guidelines:
European Space Agency
Space Debris Office, Darmstadt, Germany.
[5.5] Partner,Telecoms and Satellite, CMS Cameron McKenna LLP.
[5.6] Impact of Southampton work on International Standards:
Co-convener of the ISO Orbital
Debris Coordination Working Group.
[5.7] http://www.parliament.uk/business/committees/committees-a-z/commons-select/science-and-technology-committee/news/130606-space-ev/
[5.8] http://www.bbc.co.uk/news/science-environment-14763668
[5.9] Impact on operators: Senior Manager, Flight Dynamics,
Inmarsat.
[5.10] Estimate based on 2012 and predicted revenues from HYLAS-1
satellite:
http://www.avantiplc.com/investors/financial-reports