  In preceding papers, Project Lyra has covered many possible trajectory
options available to a spacecraft bound for 1I/Oumuamua, including Solar Oberth
manoeuvres, Passive Jupiter encounters, Jupiter Oberths, Double Jupiter
Gravitational Assists, etc. Because feasibility was the key driver for this
analysis, the important question of which launcher to exploit was largely
skirted in favour of adopting the most powerful options as being sufficient,
though these launchers are clearly not necessary, there being alternative less
capable candidates which could be utilised instead. In this paper the various
launch options available to Project Lyra are addressed to allow a general
overview of their capabilities. It is found that the SpaceX Super-Heavy
Starship would be a game-changer for Project Lyra, especially in the context of
refuelling in LEO, and furthermore a SpaceX Falcon Heavy Expendable could also
be utilised. Other launchers are considered, including Ariane 6 and the future
Chinese Long March 9. The importance of the V infinity Leveraging Manoeuvre
(VILM) in permitting less capable launchers to nevertheless deliver a payload
to Oumuamua is elaborated
