The Mars Polar Orbiter/Penetrator 1981 mission, intended to investigate the manner in which Mars has evolved, and which surveys its geochemistry, performs climatological investigations, and attempts to determine the planet's gravitational field, was described. The spacecraft, modified from the Viking Orbiter design, carries a new remote-sensing payload and six penetrators. The penetrators are released from a 2.46-h, 1000-km sun synchronous circular orbit and interrogated daily throughout the 2-year orbital mission. X-band telemetry is used to increase data return
Data from six Mariner Mars experiments are presented. Television reconnaissance of Mars and its sate...
Technology requirements and spacecraft design studies for atmosphere braking to orbit about Mars and...
The NASA\u27s next missions to Mars are to land two unmanned spacecraft on the surface in 1976 to pe...
Spacecraft system and subsystem designs were developed at the conceptual level to perform either of ...
The feasibility and efficiency of using an existing Earth orbiter to perform planetary missions was ...
Work on penetrators for planetary exploration is summarized. In particular, potential missions, incl...
Mission objectives are developed for the next logical step in the investigation of the local physica...
The Mars Microprobe Mission will be the second of the New Millennium Program's technology developmen...
Tabular synopses of twelve missions are presented along with the Mariner Jupiter/Saturn 1977 mission...
Present knowledge of the global properties and surface characteraretics of Mars and the composition ...
The Mars Microprobe Mission will be the second of the New Millennium Program's technology developmen...
The Mars Observer mission will extend the exploration and characterization of Mars by providing new ...
Various phases of planetary operations related to the Viking mission to Mars are described. Topics d...
Graphical data necessary for the preliminary design of ballistic missions to Mars are provided. Cont...
The technical feasibility of achieving automatic rendezvous and docking in Mars orbit as a part of a...
Data from six Mariner Mars experiments are presented. Television reconnaissance of Mars and its sate...
Technology requirements and spacecraft design studies for atmosphere braking to orbit about Mars and...
The NASA\u27s next missions to Mars are to land two unmanned spacecraft on the surface in 1976 to pe...
Spacecraft system and subsystem designs were developed at the conceptual level to perform either of ...
The feasibility and efficiency of using an existing Earth orbiter to perform planetary missions was ...
Work on penetrators for planetary exploration is summarized. In particular, potential missions, incl...
Mission objectives are developed for the next logical step in the investigation of the local physica...
The Mars Microprobe Mission will be the second of the New Millennium Program's technology developmen...
Tabular synopses of twelve missions are presented along with the Mariner Jupiter/Saturn 1977 mission...
Present knowledge of the global properties and surface characteraretics of Mars and the composition ...
The Mars Microprobe Mission will be the second of the New Millennium Program's technology developmen...
The Mars Observer mission will extend the exploration and characterization of Mars by providing new ...
Various phases of planetary operations related to the Viking mission to Mars are described. Topics d...
Graphical data necessary for the preliminary design of ballistic missions to Mars are provided. Cont...
The technical feasibility of achieving automatic rendezvous and docking in Mars orbit as a part of a...
Data from six Mariner Mars experiments are presented. Television reconnaissance of Mars and its sate...
Technology requirements and spacecraft design studies for atmosphere braking to orbit about Mars and...
The NASA\u27s next missions to Mars are to land two unmanned spacecraft on the surface in 1976 to pe...