The goal of this project was to perform a preliminary design of a long term, reusable transportation system between earth and Mars which would be capable of providing both artificial gravity and shelter from solar flare radiation. The heart of this system was assumed to be a Cycler spacecraft propelled by an ion propulsion system. The crew transfer vehicle was designed to be propelled by a nuclear-thermal propulsion system. Several Mars transportation system architectures and their associated space vehicles were designed
This work develops original conceptual designs for compact nuclear fission reactor engines to power ...
This paper presents a preliminary design for a crewed transportation system to Mars, looking at both...
Highly propellant-efficient electric propulsion is being combined with advanced solar power technolo...
This thesis investigates the design of interplanetary missions for the continual habitation of Mars ...
One proposed solution to slow transport times, constrained consumables, and exorbitant propellant bu...
Nuclear Thermal Propulsion (NTP) has long been considered as a viable in-space transportation altern...
The design of a Mars Mission Vehicle that would have to be launched by two very heavy lift launch ve...
Promising options for interplanetary travel between the Earth and Mars are considered. An evolving m...
This paper discusses vehicle configuration options using nuclear thermal rocket (NTR) propulsion app...
The University of Minnesota Advanced Space Design Program has developed a sample Mars exploration sc...
A variety of mission scenarios are compared in this thesis to assess the strengths and weaknesses of...
Four projects carried out in 1990-9l at the University of California, Los Angeles, under NASA/USRA s...
This paper analyzes the feasibility of insertion of a 1000-metric ton asteroid into an Earth-Mars cy...
Earth-to-Mars distances vary from 60 to 400 million kilometers over a 14-year cycle. This complicate...
This work develops original conceptual designs for compact nuclear fission reactor engines to power ...
This work develops original conceptual designs for compact nuclear fission reactor engines to power ...
This paper presents a preliminary design for a crewed transportation system to Mars, looking at both...
Highly propellant-efficient electric propulsion is being combined with advanced solar power technolo...
This thesis investigates the design of interplanetary missions for the continual habitation of Mars ...
One proposed solution to slow transport times, constrained consumables, and exorbitant propellant bu...
Nuclear Thermal Propulsion (NTP) has long been considered as a viable in-space transportation altern...
The design of a Mars Mission Vehicle that would have to be launched by two very heavy lift launch ve...
Promising options for interplanetary travel between the Earth and Mars are considered. An evolving m...
This paper discusses vehicle configuration options using nuclear thermal rocket (NTR) propulsion app...
The University of Minnesota Advanced Space Design Program has developed a sample Mars exploration sc...
A variety of mission scenarios are compared in this thesis to assess the strengths and weaknesses of...
Four projects carried out in 1990-9l at the University of California, Los Angeles, under NASA/USRA s...
This paper analyzes the feasibility of insertion of a 1000-metric ton asteroid into an Earth-Mars cy...
Earth-to-Mars distances vary from 60 to 400 million kilometers over a 14-year cycle. This complicate...
This work develops original conceptual designs for compact nuclear fission reactor engines to power ...
This work develops original conceptual designs for compact nuclear fission reactor engines to power ...
This paper presents a preliminary design for a crewed transportation system to Mars, looking at both...
Highly propellant-efficient electric propulsion is being combined with advanced solar power technolo...