  Deflection missions to near-Earth asteroids will encounter non-negligible
uncertainties in the physical and orbital parameters of the target object. In
order to reliably assess future impact threat mitigation operations such
uncertainties have to be quantified and incorporated into the mission design.
The implementation of deflection demonstration missions offers the great
opportunity to test our current understanding of deflection relevant
uncertainties and their consequences, e.g., regarding kinetic impacts on
asteroid surfaces. In this contribution, we discuss the role of uncertainties
in the NEOTwIST asteroid deflection demonstration concept, a low-cost kinetic
impactor design elaborated in the framework of the NEOShield project. The aim
of NEOTwIST is to change the spin state of a known and well characterized
near-Earth object, in this case the asteroid (25143) Itokawa. Fast events such
as the production of the impact crater and ejecta are studied via cube-sat
chasers and a flyby vehicle. Long term changes, for instance, in the asteroid's
spin and orbit, can be assessed using ground based observations. We find that
such a mission can indeed provide valuable constraints on mitigation relevant
parameters. Furthermore, the here proposed kinetic impact scenarios can be
implemented within the next two decades without threatening Earth's safety.
