  At the far reaches of the outer Solar System, the ice giants remain the last
class of planets yet to be studied using orbiters. The 2023-2032 Planetary
Science Decadal Survey has underscored the importance of the ice giants in
understanding the origin, formation, and evolution of our Solar System. The
enormous heliocentric distance of Uranus presents considerable mission design
challenges, the most important being able to reach Uranus within a reasonable
time. The present study presents two examples of aerocapture enabled short
flight time, fast trajectories for Uranus orbiter missions, and highlights the
enormous benefits provided by aerocapture. The first is an EEJU trajectory with
a launch opportunity in July 2031 with a flight time of 8 years. The second is
an EJU trajectory with a launch opportunity in June 2034 with a flight time of
only 5 years. Using the Falcon Heavy Expendable, the available launch
capability is 4950 kg and 1400 kg respectively for the two trajectories. Both
trajectories have a high arrival speed of 20 km/s, which provides sufficient
corridor width for aerocapture. Compared to propulsive insertion architectures
which take 13 to 15 years, the fast trajectories offer significant reduction in
the flight time.
