Combined missions to Mars and Phobos/Deimos were considered in relation to large scientific returns at a low total cost. A matrix of all feasible major combined mission concepts was compiled. The most promising approach was selected from which a nominal mission profile was developed. A systems analysis was performed to trade off performance, configuration, and cost characteristics of candidate mission concepts. Configuration and subsystem optimization analysis were then conducted from which a baseline and an alternate program were selected. Program schedules and cost estimates were prepared for the recommended and alternate program
As human exploration endeavors begin to set sights beyond low Earth orbit to the surface of the Moon...
International audienceThe science operations of the spacecraft and remote sensing instruments for th...
International audienceThe science operations of the spacecraft and remote sensing instruments for th...
The technical feasibility of accomplishing a variety of cost-effective missions to the satellites of...
The feasibility of a satellite rendezvous, landing, and roving mission to the Martian satellites Pho...
The scientific objectives were considered for a Phobos/Deimos mission. The payloads for a minimum us...
The physical characteristics of Phobos and Deimos, satellites of Mars, are discussed. Phobos and Dei...
NASA has conducted a series of mission studies over the past 25 years examining the eventual explora...
The human exploration of Mars represents one of civilizations next major challenges and is an enterp...
The presented trajectory design and analysis was performed for the Phobos and Deimos & Mars Environm...
This study developed, analyzed, and compared mission architectures for human exploration of Mars' Mo...
The results of a more detailed study of three missions to the surface of Mars: (1) an advanced lande...
The science operations of the spacecraft and remote sensing instruments for the Martian Moon eXplora...
AbstractWe review the previous exploration of Phobos and Deimos by spacecraft. The first close-up im...
Parametric data, systems analyses, and space capsule design concepts - direct versus orbital entry f...
As human exploration endeavors begin to set sights beyond low Earth orbit to the surface of the Moon...
International audienceThe science operations of the spacecraft and remote sensing instruments for th...
International audienceThe science operations of the spacecraft and remote sensing instruments for th...
The technical feasibility of accomplishing a variety of cost-effective missions to the satellites of...
The feasibility of a satellite rendezvous, landing, and roving mission to the Martian satellites Pho...
The scientific objectives were considered for a Phobos/Deimos mission. The payloads for a minimum us...
The physical characteristics of Phobos and Deimos, satellites of Mars, are discussed. Phobos and Dei...
NASA has conducted a series of mission studies over the past 25 years examining the eventual explora...
The human exploration of Mars represents one of civilizations next major challenges and is an enterp...
The presented trajectory design and analysis was performed for the Phobos and Deimos & Mars Environm...
This study developed, analyzed, and compared mission architectures for human exploration of Mars' Mo...
The results of a more detailed study of three missions to the surface of Mars: (1) an advanced lande...
The science operations of the spacecraft and remote sensing instruments for the Martian Moon eXplora...
AbstractWe review the previous exploration of Phobos and Deimos by spacecraft. The first close-up im...
Parametric data, systems analyses, and space capsule design concepts - direct versus orbital entry f...
As human exploration endeavors begin to set sights beyond low Earth orbit to the surface of the Moon...
International audienceThe science operations of the spacecraft and remote sensing instruments for th...
International audienceThe science operations of the spacecraft and remote sensing instruments for th...