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(Reference retrieved automatically from Web of Science through information on FAPESP grant and its corresponding number as mentioned in the publication by the authors.)

Intervening in Earth's climate system through space-based solar reflectors

Full text
Author(s):
Salazar, F. J. T. [1] ; McInnes, C. R. [1] ; Winter, O. C. [2]
Total Authors: 3
Affiliation:
[1] Univ Glasgow, Sch Engn, Glasgow G12 8QQ, Lanark - Scotland
[2] UNESP Grp Dinam Orbital & Planetol, BR-12516410 Guaratingueta, SP - Brazil
Total Affiliations: 2
Document type: Journal article
Source: Advances in Space Research; v. 58, n. 1, p. 17-29, JUL 1 2016.
Web of Science Citations: 6
Abstract

Several space-based climate engineering methods, including shading the Earth with a particle ring for active cooling, or the use of orbital reflectors to increase the total insolation of Mars for climate warming have been considered to modify planetary climates in a controller manner. In this study, solar reflectors on polar orbits are proposed to intervene in the Earth's climate system, involving near circular polar orbits normal to the ecliptic plane of the Earth. Similarly, a family of displaced polar orbits (non-Keplerian orbits) are also characterized to mitigate future natural climate variability, producing a modest global temperature increase, again to compensate for possible future cooling. These include deposition of aerosols in the stratosphere from large volcanic events. The two-body problem is considered, taking into account the effects of solar radiation pressure and the Earth's J(2) oblateness perturbation. (C) 2016 COSPAR. Published by Elsevier Ltd. All rights reserved. (AU)

FAPESP's process: 15/00559-3 - Intervening on Earth's climate through heliotropic dust rings and dust cloud at the L1 Lagrange point
Grantee:Francisco Javier Tipán Salazar
Support type: Scholarships abroad - Research Internship - Post-doctor
FAPESP's process: 11/08171-3 - Orbital dynamics of minor bodies
Grantee:Othon Cabo Winter
Support type: Research Projects - Thematic Grants
FAPESP's process: 13/03233-6 - Dynamics, control and reconfiguration of satellite formation flight around Lagrangian points
Grantee:Francisco Javier Tipán Salazar
Support type: Scholarships in Brazil - Post-Doctorate