Pressurized rovers can add many attractive capabilities to a human lunar exploration campaign, most notably by extending the reach of astronauts far beyond the immediate vicinities of lunar landers and fixed assets such as habitats. Effective campaigns will depend on an efficient allocation of environmental control and life support system (ECLSS) equipment amongst mobile rovers and fixed habitats such that widespread and sustainable exploration can be achieved. This paper will describe some of the key drivers that influence the design of an ECLSS for a pressurized lunar rover and a conceptual design that has been formulated to address those drivers. Opportunities to realize programmatic and operational efficiencies through commonality of ro...
Traditional concepts of lunar bases describe scenarios where components of the bases are landed on t...
Rover trade study: As summarized recently, mission simulations at Black Point Lava Flow (Arizona) th...
The Spring 1990 Introduction to Design class was asked to conceptually design second generation luna...
Engineers at Johnson Space Center (JSC) are developing an Environmental Control and Life Support Sys...
NASA is engaged in early architectural analyses and trade studies aimed at identifying requirements,...
With the Preliminary Design Review (PDR) for the Orion Crew Exploration Vehicle planned to be comple...
Engineers at Johnson Space Center (JSC) are developing an Environmental Control and Life Support Sys...
AbstractThis paper presents the conceptual design and analysis of a system intended to increase the ...
The Moon is the next destination for future human space exploration beyond LEO and a key element of ...
As the U.S. space program plans for a return to the Lunar surface and ultimately for a mission to Ma...
This paper presents results of a life support architecture study based on a 2009 NASA lunar surface ...
Lunar robotic functions include: 1. Transport of crew and payloads on the surface of the moon; 2. Of...
Engineers designing life support systems for NASA s next Lunar Landers face unique challenges. As wi...
The purpose of this paper is to identify and briefly discuss some of the ground rules and mission sc...
This paper defines the types of technology that would be used in a lunar base for environmental cont...
Traditional concepts of lunar bases describe scenarios where components of the bases are landed on t...
Rover trade study: As summarized recently, mission simulations at Black Point Lava Flow (Arizona) th...
The Spring 1990 Introduction to Design class was asked to conceptually design second generation luna...
Engineers at Johnson Space Center (JSC) are developing an Environmental Control and Life Support Sys...
NASA is engaged in early architectural analyses and trade studies aimed at identifying requirements,...
With the Preliminary Design Review (PDR) for the Orion Crew Exploration Vehicle planned to be comple...
Engineers at Johnson Space Center (JSC) are developing an Environmental Control and Life Support Sys...
AbstractThis paper presents the conceptual design and analysis of a system intended to increase the ...
The Moon is the next destination for future human space exploration beyond LEO and a key element of ...
As the U.S. space program plans for a return to the Lunar surface and ultimately for a mission to Ma...
This paper presents results of a life support architecture study based on a 2009 NASA lunar surface ...
Lunar robotic functions include: 1. Transport of crew and payloads on the surface of the moon; 2. Of...
Engineers designing life support systems for NASA s next Lunar Landers face unique challenges. As wi...
The purpose of this paper is to identify and briefly discuss some of the ground rules and mission sc...
This paper defines the types of technology that would be used in a lunar base for environmental cont...
Traditional concepts of lunar bases describe scenarios where components of the bases are landed on t...
Rover trade study: As summarized recently, mission simulations at Black Point Lava Flow (Arizona) th...
The Spring 1990 Introduction to Design class was asked to conceptually design second generation luna...