The invention comprises a space ship, which commutes between earth orbit and lunar orbit, and is powered by a rocket engine, using superheated steam, or other non-cryogenic propellant, where the propellant is heated in a conventional uranium nuclear reactor.
Thermal-nucleak powered rocket using non-cryogenic propellant
2017-05-11
Patent
Elektronische Ressource
Englisch
Cryogenic Propellant Rocket Engine Problems
NTIS | 1993
|Modular Dissected Cryogenic Solid-Rocket Propellant Grains
Online Contents | 2002
|Modular Dissected Cryogenic Solid-Rocket Propellant Grains
British Library Conference Proceedings | 1998
|Status of Cryogenic Solid Rocket Propellant Development
British Library Conference Proceedings | 2003
|Milestones in cryogenic liquid propellant rocket engines
AIAA | 1967
|