Scientific mission to a solar polar orbit using solar sail propulsion

Research output: Contribution to conferencePaper

Abstract

Solar sail propelled missions to a polar orbit of the Sun offer unique science opportunities. Previous proposals have recommended the use of a 2-phase transfer to reach a solar polar orbit, however a 3-phase transfer has since been shown to offer a significant reduction in the transfer time at the expense of higher thermal stresses. The 3-phase transfer involves spiralling in close to the Sun, performing a rapid inclination increase, and spiralling back out to the final target orbit. A general perturbation solution for such a transfer has been defined which offers significant advantages over the numerically optimised solutions currently available. The insights provided by this analytical solution are used here to rapidly generate a holistic understanding of the mission architecture options available and hence how the mission and system design could be traded. A number of potential science missions are identified which could benefit uniquely from the use of such an orbit. These require that a solar latitude of 60° be achieved within 5 years before proceeding to a true polar orbit. A comparison between the use of the 2- and 3-phase transfer options identify that in real terms, the 3-phase transfer will reach a polar orbit approximately 1 year ahead of the 2-phase transfer. In addition, the increased efficiency of the transfer would allow for an increase in the allowable
payload mass; with up to an extra 33kg payload potential predicted. Further work should allow for the mission and system design to be traded; for example to investigate the implications of increased thermal system mass (due to a reduction in the minimum solar approach distance) against reduced transfer time or sail size.
LanguageEnglish
PagesIAC-14-E2.1.7
Number of pages7
Publication statusPublished - 3 Oct 2014
Event65th International Astronautical Congress (IAC 2014) - Metro Toronto Convention Centre, Toronto, Canada
Duration: 29 Sep 20143 Oct 2014

Conference

Conference65th International Astronautical Congress (IAC 2014)
CountryCanada
CityToronto
Period29/09/143/10/14

Fingerprint

Propulsion
Orbits
Sun
Systems analysis
Thermal stress

Keywords

  • solar sailing
  • solar polar orbit
  • 3-phase transfer
  • analytical solutions
  • mission design

Cite this

McGrath, C., & Macdonald, M. (2014). Scientific mission to a solar polar orbit using solar sail propulsion. IAC-14-E2.1.7. Paper presented at 65th International Astronautical Congress (IAC 2014), Toronto, Canada.
McGrath, Ciara ; Macdonald, Malcolm. / Scientific mission to a solar polar orbit using solar sail propulsion. Paper presented at 65th International Astronautical Congress (IAC 2014), Toronto, Canada.7 p.
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McGrath, C & Macdonald, M 2014, 'Scientific mission to a solar polar orbit using solar sail propulsion' Paper presented at 65th International Astronautical Congress (IAC 2014), Toronto, Canada, 29/09/14 - 3/10/14, pp. IAC-14-E2.1.7.

Scientific mission to a solar polar orbit using solar sail propulsion. / McGrath, Ciara; Macdonald, Malcolm.

2014. IAC-14-E2.1.7 Paper presented at 65th International Astronautical Congress (IAC 2014), Toronto, Canada.

Research output: Contribution to conferencePaper

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McGrath C, Macdonald M. Scientific mission to a solar polar orbit using solar sail propulsion. 2014. Paper presented at 65th International Astronautical Congress (IAC 2014), Toronto, Canada.