Add to ORKGSpacecraft system and subsystem designs at the conceptual level to perform either of two Mars Orbiter missions, a Climatology Mission and an Aeronomy Mission were developed. The objectives of these missions are to obtain and return data
Data derived from Mariners 6, 7, and 9, Russian Mars probes, and photographic and radar observations...
The requirements, issues, and design options are reviewed for manned Mars landers. Issues such as hi...
Astronauts on a mission to Mars will require several vehicles working together to get to Mars orbit,...
Spacecraft system and subsystem designs were developed at the conceptual level to perform either of ...
The FLTSATCOM Earth orbiting communications satellite is a prominent candidate to serve as the Mars ...
The accomplishments of the Utah State University (USU) Mars Lander/Rover (MLR) design class during t...
The University of Minnesota Advanced Space Design Program has developed a sample Mars exploration sc...
Mars Aerocapture Systems Study (MASS) is a detailed study of the application of aerocapture to a lar...
The technical feasibility of achieving automatic rendezvous and docking in Mars orbit as a part of a...
Design concepts are described for landing large spacecraft masses on the Mars surface in support of ...
Covered here is the second phase of a broad scoped and systematic study of space transfer concepts f...
The topics are presented in viewgraph form and include the following: Mars Observer; Mars Environmen...
This document contains graphical data necessary for the preliminary design of ballistic missions ret...
Technology requirements and spacecraft design studies for atmosphere braking to orbit about Mars and...
The Aerial Regional-Scale Environmental Survey (ARES) is a Mars exploration mission concept that uti...
Data derived from Mariners 6, 7, and 9, Russian Mars probes, and photographic and radar observations...
The requirements, issues, and design options are reviewed for manned Mars landers. Issues such as hi...
Astronauts on a mission to Mars will require several vehicles working together to get to Mars orbit,...
Spacecraft system and subsystem designs were developed at the conceptual level to perform either of ...
The FLTSATCOM Earth orbiting communications satellite is a prominent candidate to serve as the Mars ...
The accomplishments of the Utah State University (USU) Mars Lander/Rover (MLR) design class during t...
The University of Minnesota Advanced Space Design Program has developed a sample Mars exploration sc...
Mars Aerocapture Systems Study (MASS) is a detailed study of the application of aerocapture to a lar...
The technical feasibility of achieving automatic rendezvous and docking in Mars orbit as a part of a...
Design concepts are described for landing large spacecraft masses on the Mars surface in support of ...
Covered here is the second phase of a broad scoped and systematic study of space transfer concepts f...
The topics are presented in viewgraph form and include the following: Mars Observer; Mars Environmen...
This document contains graphical data necessary for the preliminary design of ballistic missions ret...
Technology requirements and spacecraft design studies for atmosphere braking to orbit about Mars and...
The Aerial Regional-Scale Environmental Survey (ARES) is a Mars exploration mission concept that uti...
Data derived from Mariners 6, 7, and 9, Russian Mars probes, and photographic and radar observations...
The requirements, issues, and design options are reviewed for manned Mars landers. Issues such as hi...
Astronauts on a mission to Mars will require several vehicles working together to get to Mars orbit,...