A survey of mission opportunities to Trans-Neptunian Objects

Ryan McGranaghan, Brent Sagan, Gemma Dove, Aaron Tullos, J. E. Lyne, Joshua P. Emery

Research output: Chapter in Book/Report/Conference proceedingConference contribution

4 Scopus citations

Abstract

Preliminary designs for high thrust, flyby missions to five large trans-Neptunian Objects are discussed, with an emphasis on Quaoar, but also including Sedna, Makemake, Haumea, and Eris. The primary focus of this study was the design of the interplanetary trajectory for Earth departure dates between 2014 and 2050. The best trajectories identified use only a Jupiter gravity assist, require a total mission delta-V as low as 7.15 km/s and have arrival V values at the target comparable to those of the New Horizons mission to Pluto. Transit times range from 13.57 years for missions to Quaoar to 24.48 years to reach Sedna and Eris. Jupiter periapse radius is a critical factor for these missions, with satisfactory trajectories requiring values ranging from 3.5 to 25 planetary radii.

Original languageEnglish (US)
Title of host publicationASTRODYNAMICS 2011 - Advances in the Astronautical Sciences
Subtitle of host publicationProceedings of the AAS/AIAA Astrodynamics Specialist Conference
Pages3333-3348
Number of pages16
StatePublished - 2012
Externally publishedYes
Event2011 AAS/AIAA Astrodynamics Specialist Conference, ASTRODYNAMICS 2011 - Girdwood, AK, United States
Duration: Jul 31 2011Aug 4 2011

Publication series

NameAdvances in the Astronautical Sciences
Volume142
ISSN (Print)0065-3438

Conference

Conference2011 AAS/AIAA Astrodynamics Specialist Conference, ASTRODYNAMICS 2011
Country/TerritoryUnited States
CityGirdwood, AK
Period7/31/118/4/11

Keywords

  • Interplanetary
  • Mission design
  • Trans-Neptunian Objects

ASJC Scopus subject areas

  • Aerospace Engineering
  • Space and Planetary Science

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