The accomplishments of the Utah State University (USU) Mars Lander/Rover (MLR) design class during the Winter Quarter are delineated and explained. Environment and trajectory, ground systems, balloon system, and payload system are described. Results from this effort will provide a valid and useful basis for further studies of Mars exploratory vehicles
The requirements, issues, and design options are reviewed for manned Mars landers. Issues such as hi...
Data derived from Mariners 6, 7, and 9, Russian Mars probes, and photographic and radar observations...
In conjunction with NASA Marshall Space Flight Center and several major aerospace corporations the U...
A design is proposed for a Mars Lander/Rover (MLR) for use in gathering needed environmental and sur...
Investigating problems related to landing and controlling mobile planetary vehicle on Mars according...
Spacecraft system and subsystem designs at the conceptual level to perform either of two Mars Orbite...
A viable power system technology for a surface transportation vehicle to explore the planet Mars is ...
Design, development and characteristics of surface vehicle for exploration of planet Mar
The Solar System Exploration Committee (SSEC) of the NASA Advisory Council recommends that a Mars Sa...
Alternative mission/system approaches to automated Mars surface sample return based on utilization o...
The University of Minnesota Advanced Space Design Program has developed a sample Mars exploration sc...
This is a summary of the Group Design Project of the MSc course in Astronautics and Space Engineerin...
Modification to direct versus orbital entry for Mars mission as result of Mars environmental mode
Spacecraft system and subsystem designs were developed at the conceptual level to perform either of ...
Astronauts on a mission to Mars will require several vehicles working together to get to Mars orbit,...
The requirements, issues, and design options are reviewed for manned Mars landers. Issues such as hi...
Data derived from Mariners 6, 7, and 9, Russian Mars probes, and photographic and radar observations...
In conjunction with NASA Marshall Space Flight Center and several major aerospace corporations the U...
A design is proposed for a Mars Lander/Rover (MLR) for use in gathering needed environmental and sur...
Investigating problems related to landing and controlling mobile planetary vehicle on Mars according...
Spacecraft system and subsystem designs at the conceptual level to perform either of two Mars Orbite...
A viable power system technology for a surface transportation vehicle to explore the planet Mars is ...
Design, development and characteristics of surface vehicle for exploration of planet Mar
The Solar System Exploration Committee (SSEC) of the NASA Advisory Council recommends that a Mars Sa...
Alternative mission/system approaches to automated Mars surface sample return based on utilization o...
The University of Minnesota Advanced Space Design Program has developed a sample Mars exploration sc...
This is a summary of the Group Design Project of the MSc course in Astronautics and Space Engineerin...
Modification to direct versus orbital entry for Mars mission as result of Mars environmental mode
Spacecraft system and subsystem designs were developed at the conceptual level to perform either of ...
Astronauts on a mission to Mars will require several vehicles working together to get to Mars orbit,...
The requirements, issues, and design options are reviewed for manned Mars landers. Issues such as hi...
Data derived from Mariners 6, 7, and 9, Russian Mars probes, and photographic and radar observations...
In conjunction with NASA Marshall Space Flight Center and several major aerospace corporations the U...