The design of a Mars Mission Vehicle that would have to be launched by two very heavy lift launch vehicles is described along with plans for a mission to Mars. The vehicle has three nuclear engine for rocket vehicle application (NERVA) boosters with a fourth in the center that acts as a dual mode system. The fourth generates electrical power while in route, but it also helps lift the vehicle out of earth orbit. A Mars Ascent Vehicle (MAV), a Mars transfer vehicle stage, and a Mars Excursion Vehicle (MEV) are located on the front end of this vehicle. Other aspects of this research including aerobraking, heat shielding, nuclear thermal rocket engines, a mars mission summary, closed Brayton cycle with and without regeneration, liquid hydrogen ...
Multiyear civilian manned missions to explore the surface of Mars are thought by NASA to be possible...
In the 1960's, Nuclear Thermal Rocket (NTR) engines were developed and ground tested capable of yiel...
A human mission to Mars, if it is to be cost effective, should take maximum advantage of previous ef...
Earth-to-Mars distances vary from 60 to 400 million kilometers over a 14-year cycle. This complicate...
The University of Minnesota Advanced Space Design Program has developed a sample Mars exploration sc...
Highly propellant-efficient electric propulsion is being combined with advanced solar power technolo...
Four projects carried out in 1990-9l at the University of California, Los Angeles, under NASA/USRA s...
The goal of this project was to perform a preliminary design of a long term, reusable transportation...
This paper presents a preliminary design for a crewed transportation system to Mars, looking at both...
A number of manned Mars mission types, propulsion systems, and operational techniques are compared. ...
NASA has completed a preliminary mission and systems study of nuclear electric propulsion (NEP) syst...
The mission benefits of using both high thrust nuclear thermal propulsion (NTP) and low acceleration...
This paper discusses vehicle configuration options using nuclear thermal rocket (NTR) propulsion app...
Mars transfer vehicles (MTV\u27s) using nuclear thermal propulsion (NTP) to reduce transit time intr...
A combined Nuclear Thermal Rocket (NTR) flight test and Mars Sample Return mission (MSR) is explored...
Multiyear civilian manned missions to explore the surface of Mars are thought by NASA to be possible...
In the 1960's, Nuclear Thermal Rocket (NTR) engines were developed and ground tested capable of yiel...
A human mission to Mars, if it is to be cost effective, should take maximum advantage of previous ef...
Earth-to-Mars distances vary from 60 to 400 million kilometers over a 14-year cycle. This complicate...
The University of Minnesota Advanced Space Design Program has developed a sample Mars exploration sc...
Highly propellant-efficient electric propulsion is being combined with advanced solar power technolo...
Four projects carried out in 1990-9l at the University of California, Los Angeles, under NASA/USRA s...
The goal of this project was to perform a preliminary design of a long term, reusable transportation...
This paper presents a preliminary design for a crewed transportation system to Mars, looking at both...
A number of manned Mars mission types, propulsion systems, and operational techniques are compared. ...
NASA has completed a preliminary mission and systems study of nuclear electric propulsion (NEP) syst...
The mission benefits of using both high thrust nuclear thermal propulsion (NTP) and low acceleration...
This paper discusses vehicle configuration options using nuclear thermal rocket (NTR) propulsion app...
Mars transfer vehicles (MTV\u27s) using nuclear thermal propulsion (NTP) to reduce transit time intr...
A combined Nuclear Thermal Rocket (NTR) flight test and Mars Sample Return mission (MSR) is explored...
Multiyear civilian manned missions to explore the surface of Mars are thought by NASA to be possible...
In the 1960's, Nuclear Thermal Rocket (NTR) engines were developed and ground tested capable of yiel...
A human mission to Mars, if it is to be cost effective, should take maximum advantage of previous ef...