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The first definitely interstellar object 1I/'Oumuamua (previously A/2017 U1)observed in our solar system provides the opportunity to directly studymaterial from other star systems. Can such objects be intercepted? Thechallenge of reaching the object within a reasonable timeframe is formidabledue to its high heliocentric hyperbolic excess velocity of about 26 km/s; muchfaster than any vehicle yet launched. This paper presents a high-level analysisof potential near-term options for a mission to 1I/'Oumuamua and potentialsimilar objects. Launching a spacecraft to 1I/'Oumuamua in a reasonabletimeframe of 5-10 years requires a hyperbolic solar system excess velocitybetween 33 to 76 km/s for mission durations between 30 to 5 years. Differentmission durations and their velocity requirements are explored with respect tothe launch date, assuming direct impulsive transfer to the intercepttrajectory. For missions using a powered Jupiter flyby combined with a solarOberth maneuver using solid rocket boosters and Parker Solar Probe heat shieldtechnology, a Falcon Heavy-class launcher would be able to launch a spacecraftof dozens of kilograms towards 1I/'Oumuamua, if launched in 2021. An additionalSaturn flyby would allow for the launch of a New Horizons-class spacecraft.Further technology options are outlined, ranging from electric propulsion, andmore advanced options such as laser electric propulsion, and solar and lasersails. To maximize science return decelerating the spacecraft at 'Oumuamua ishighly desirable, due to the minimal science return from a hyper-velocityencounter. Electric and magnetic sails could be used for this purpose. It isconcluded that although reaching the object is challenging, there seem to befeasible options based on current and near-term technology.

Project Lyra: Sending a Spacecraft to 1I/'Oumuamua (former A/2017 U1), the Interstellar Asteroid