Dealing with Uncertainties in Asteroid Deflection Demonstration Missions: NEOTwIST
Siegfried Eggl, Daniel Hestroffer, Juan L. Cano, Javier Martin Avila,, Line Drube, Alan W. Harris, Albert Falke, Ulrich Johann, Kilian Engel,, Stephen R. Schwartz, Patrick Michel

TL;DR
This paper discusses how uncertainties in asteroid properties affect deflection missions, using the NEOTwIST concept to test mitigation strategies and improve impact risk assessment within a feasible timeframe.
Contribution
It introduces the NEOTwIST asteroid deflection concept, demonstrating its potential to evaluate uncertainties and their effects on asteroid deflection outcomes.
Findings
NEOTwIST can constrain mitigation parameters effectively.
The proposed impact scenarios are feasible within two decades.
Uncertainty quantification improves impact risk assessment.
Abstract
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…
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