Article révisé par les pairs
Résumé : As an emerging trend, Green Propulsion has been exponentially growing over the last decades in the space sector. This paper assesses different technologies in a trade-off study weighting their applicability to a specific class of upper stage systems currently developed by many companies and often referred to as kick-stages or orbital stages. In a generic two-stage-to-orbit scenario, many launchers require a system able to go the ‘extra mile’ to deliver one or multiple payloads on orbit(s). That is where the kick stage comes into playing a crucial role. The trade-off study reported here is based on a well-known decision-making tool, the Analytical Hierarchy Process, and is divided into two parts: low-thrust class engines such as monopropellants, including pre-mixed blends, usually employed for attitude and reaction control; and high-thrust engines such as hypergolic bi-propellants combinations used for apogee manoeuvres. Hybrid thrusters are also considered in the analysis with a dedicated parallel trade-off.