Mission to Mars using integrated propulsion concepts: considerations, opportunities, and strategies.
The aim of this paper is to evaluate the feasibility of a mission to Mars using the Integrated Propulsion Systems (IPS) which means to couple Nuclear-MPD-ISPU propulsion systems. In particular both mission analysis and propulsion aspects are analyzed together with technological aspects. Identifying possible mission scenarios will lead to the study of possible strategies for Mars Exploration and also of methods for reducing cost. As regard to IPS, the coupling between Nuclear Propulsion (Rubbia's engine) and Superconductive MPD propulsion is considered for the Earth-Mars trajectories: major emphasis is given to the advantages of such a system. The In Situ Resource Utilization (ISRU) concerns on-Mars operations; In Situ Propellant Utilization (ISPU) is foreseen particularly for LOX-CH4 engines for Mars Ascent Vehicles and this possibility is analyzed from a technological point of view. Tether Systems are also considered during interplanetary trajectories and as space elevators on Mars orbit. Finally strategic considerations associated to this mission are considered also.
Accettura
Antonio G
AG
Space Propulsion Design Department, Fiat Avio, Colleferro Rome, Italy. antonio.accettura@fiatavio.it
Bruno
Claudio
C
Casotto
Stefano
S
Marzari
Francesco
F
D001272:Atmosphere / Q000737:chemistry; D002245:Carbon Dioxide / Q000737:chemistry; D004738:Engineering; D005069:Evaluation Studies as Topic; D005118:Extraterrestrial Environment; D005160:Facility Design and Construction; D018470:Gravity, Altered; D018535:Mars; D013026:Space Flight / Q000295:instrumentation*; D018531:Spacecraft / Q000295:instrumentation*; D014893:Weightlessness
D002245:Carbon Dioxide