Trajectories to Nab a NEA (Near-Earth Asteroid)

Damon Landau, John Dankanich, Nathan Strange, Julie Bellerose, Pedro Llanos, Marco Tantardini, Pedro J Llanos de la Concha

Research output: Contribution to conferencePresentation

Abstract

In 2010 and 2011 NASA and Keck Institute for Space Studies sponsored investigations into the feasibility of identifying, capturing, and returning an entire (albeit small) NEA to the vicinity of Earth, and concluded that a 40-kW solar electric propulsion system launched on an Atlas 551 provided sufficient propulsion to control an asteroid's trajectory. Once secured by the spacecraft, a NEA with a naturally close encounter with Earth is nudged over a few years to target a lunar gravity assist, capturing the object into Earth orbit. With further use of solar perturbations, up to 3,600,000 kg of NEA could be placed in high-lunar orbit.
Original languageAmerican English
StatePublished - Feb 2013
EventAAS/AIAA Spaceflight Mechanics Conference - Kauai, HI
Duration: Feb 1 2013 → …

Conference

ConferenceAAS/AIAA Spaceflight Mechanics Conference
Period2/1/13 → …

Keywords

  • near-Earth asteroids
  • solar electric propulsion system
  • asteroid trajectories

Disciplines

  • Space Vehicles
  • Astrophysics and Astronomy

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