Mars, Phobos, and Deimos Sample Return Enabled by ARRM Alternative Trade Study Spacecraft
Author(s) -
Jacob A. Englander,
Matthew A. Vavrina,
Bo J. Naasz,
Raymond G. Merrill,
Min Qu
Publication year - 2014
Publication title -
aiaa/aas astrodynamics specialist conference
Language(s) - English
Resource type - Conference proceedings
DOI - 10.2514/6.2014-4354
Subject(s) - mars exploration program , astrobiology , spacecraft , sample (material) , environmental science , aerospace engineering , physics , engineering , thermodynamics
The Asteroid Robotic Redirect Mission (ARRM) has been the topic of many mission design studies since 2011. The reference ARRM spacecraft uses a powerful solar electric propulsion (SEP) system and a bag device to capture a small asteroid from an Earth-like orbit and redirect it to a distant retrograde orbit (DRO) around the moon. The ARRM Option B spacecraft uses the same propulsion system and multi-Degree of Freedom (DoF) manipulators device to retrieve a very large sample (thousands of kilograms) from a 100+ meter diameter farther-away Near Earth Asteroid (NEA). This study will demonstrate that the ARRM Option B spacecraft design can also be used to return samples from Mars and its moons - either by acquiring a large rock from the surface of Phobos or Deimos, and or by rendezvousing with a sample-return spacecraft launched from the surface of Mars.
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