Target selection for a hypervelocity asteroid intercept vehicle flight validation mission

• We describe and show results from a highly capable trajectory optimization program.
• Our program incorporates gravity assists and uses a genetic algorithm.
• Our program produces very low ΔVΔV solutions even for complicated mission scenarios.

Asteroids and comets have collided with the Earth in the past and will do so again in the future. Throughout Earth׳s history these collisions have played a significant role in shaping Earth׳s biological and geological histories. The planetary defense community has been examining a variety of options for mitigating the impact threat of asteroids and comets that approach or cross Earth׳s orbit, known as near-Earth objects (NEOs). This paper discusses the preliminary study results of selecting small (100-m class) NEO targets and mission analysis and design trade-offs for validating the effectiveness of a Hypervelocity Asteroid Intercept Vehicle (HAIV) concept, currently being investigated for a NIAC (NASA Advanced Innovative Concepts) Phase 2 study. In particular this paper will focus on the mission analysis and design for single spacecraft direct impact trajectories, as well as several mission types that enable a secondary rendezvous spacecraft to observe the HAIV impact and evaluate it׳s effectiveness.