Asteroid Redirect Mission

[1] If funded, the mission would have launched in December 2021,[2] with the additional objectives to test a number of new capabilities needed for future human expeditions to deep space, including advanced ion thrusters.

[5] Key technologies being developed for ARM have continued, especially the ion thruster propulsion system that would have been flown on the robotic mission.

[6][11][8][14][15][16] Not only would the solar electric propulsion (SEP) technologies and designs be applied to future missions, but the ARRM spacecraft would be left in a stable orbit for reuse.

[20] Lunar Distant Retrograde Orbit (DRO), encompassing Earth-Moon L1 and L2, is essentially a node for Earth system escape and capture.

[2][24][25] Additional mission aims included demonstrating planetary defense techniques able to protect the Earth in the future – such as using robotic spacecraft to deflect potentially hazardous asteroids.

[27] The mission would also test the performance of advanced solar electric propulsion (ion engines)[13] and broad-band laser communication in space.

[13][47] The advanced ion engine uses 10% of the propellant required by equivalent chemical rockets, it can process three times the power of previous designs, and increase efficiency by 50%.

[48] It would use the Hall-effect, which provides low acceleration but can fire continuously for many years to thrust a large mass to high speed.

By early 2017 NASA had yet to select a target for ARM, but for planning and simulation purposes, the near-Earth asteroid (341843) 2008 EV5 was used as an example for the spacecraft to pick up a single 4 m (13 ft) boulder from it.

[53] The carbonaceous boulder that would have been captured by the mission (maximum 6 meter diameter, 20 tons)[45] is too small to harm the Earth because it would burn up in the atmosphere.

[28] Option B, which was selected in March 2015, would have the vehicle land on a large asteroid and deploy robotic arms to lift up a boulder up to 4 m (13 ft) in diameter from the surface, transport it and place it into lunar orbit.

[24][29] This option was identified as more relevant to future rendezvous, autonomous docking, lander, sampler, planetary defense, mining, and spacecraft servicing technologies.

[62] In January 2016 contracts were awarded by NASA's Jet Propulsion Laboratory (JPL) for design studies for a solar electric propulsion-based spacecraft.

Grippers on the end of the robotic arms are used to grasp and secure a boulder from a large asteroid. Once the boulder is secured, the legs would push off and provide an initial ascent without the use of thrusters.
Astronaut on EVA to take asteroid samples, Orion in the background
Asteroid grippers on the end of the robotic arms are used to grasp and secure a 6 m boulder from a large asteroid. An integrated drill would be used to provide final anchoring of the boulder to the capture mechanism.
Rendering of the Asteroid Redirect Vehicle departing the asteroid after capturing a boulder from its surface
The 'Option A' was to deploy a container large enough to capture a free-flying asteroid up to 8 m (26 ft) in diameter.