https://www.diva-portal.org/smash/record.jsf?pid=diva2%3A1900953&dswid=-8192

*Author*
Wilk, Lisa

*25 September 2024*

*Abstract*
The global surface temperature has been steadily increasing over the last
50 years, reaching an all-time high in 2023. One proposed strategy to
mitigate global warming is geoengineering, specifically by placing a
sunshade in the vicinity of Lagrange Point One L1, in the Sun-Earth system.
This sunshade system would block part of the sunlight that reaches Earth,
thereby lowering the surface temperature. A viable transportation method
for the sunshade system to L1 is solar sailing, or solar propulsion, which
uses light to propel the spacecraft forward. In this thesis, a proposed
solar sailing precursor spacecraft is developed to demonstrate the
feasibility of this approach and validate the used technology. The design
focuses on the solar sail, the booms and the attitude control system. The
selected systems are scalable and currently available, eliminating the need
for new technology development. The precursor spacecraft will be a 12U
CubeSat equipped with a 144 m² solar sail. The sail membrane will be made
out of Clear Polymer 1 (CP1), and coated on both sides with vaporized
aluminium to achieve high reflectivity. The sail will be supported by four
8.5 m long Collapsible Tubular Mast (CTM) booms made from Carbon Fiber
Reinforced Polymer (CFRP). Momentum management will be performed using an
Active Mass Translator (AMT), and Reflectivity Control Devices (RCD). The
precursor spacecraft will be launched into geostationary orbit and spend
approximately 1500 days solar sailing to the vicinity of L1. The estimated
cost to realize this mission is around 5.5 M US$.

*Source: DiVA*

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