Paper information

Paper code

IAC-19,C3,5-C4.7,x50876

Room

143A

Title

Analysis and System Design of Nuclear Thermal Rocket Employing Propellant produced In-Situ for Planetary Exploration

abstract

View PDF

Session

5-C4.7. Joint Session on Advanced and Nuclear Power and Propulsion Systems

symposium

C3. IAF SPACE POWER SYMPOSIUM

congress

IAC-19

Type of presentation

none

Main author

Mr. Davide Barbero, Politecnico di Torino, Italy

Co-authors

Mr. Alessandro Lovagnini, Politecnico di Torino, Italy;