Add to ORKGThe ultimate objective of this project is to land men on the surface of the moon and return the men safely to earth. The objective of this document is to define the design approaches and operational techniques for transporting a three-man crew to the moon and returning them to earth
Mars landing and reconnaissance mission - environmental control and life support system - subsystem ...
Mission planning and systems design of lunar surface photographic reconnaissance capsul
The University Space Research Association (USRA) requested the University of Minnesota Spacecraft De...
The current technical effort is part of the third phase of a broad-scoped and systematic study of sp...
Remote sensing missions were synthesized which could contribute significantly to the understanding o...
NASA's two Office of Space Flight (Code M) Space Transfer Vehicle (STV) contractors supported develo...
The space shuttle will provide an opportunity to extend and enhance the crew's inherent capabilities...
Major growth options for tended and manned space stations in LEO and GEO are examined including incr...
A study was conducted to define reasonable and representative large deployable reflector (LDR) syste...
Information is given in simple terms of the Apollo 15 lunar exploration and scientific equipment, to...
The Science Mission Requirements Document (MSRD) is the authoritative source for the science mission...
Systems design validation of Surveyor lunar roving vehicle - navigation, control and display, televi...
Spacecraft development, mission design planning, flight crew operations, and flight operations are c...
NASA is engaged in early architectural analyses and trade studies aimed at identifying requirements,...
Radar sensor system for acquisition of lunar surface data - Lunar contour mapping syste
Mars landing and reconnaissance mission - environmental control and life support system - subsystem ...
Mission planning and systems design of lunar surface photographic reconnaissance capsul
The University Space Research Association (USRA) requested the University of Minnesota Spacecraft De...
The current technical effort is part of the third phase of a broad-scoped and systematic study of sp...
Remote sensing missions were synthesized which could contribute significantly to the understanding o...
NASA's two Office of Space Flight (Code M) Space Transfer Vehicle (STV) contractors supported develo...
The space shuttle will provide an opportunity to extend and enhance the crew's inherent capabilities...
Major growth options for tended and manned space stations in LEO and GEO are examined including incr...
A study was conducted to define reasonable and representative large deployable reflector (LDR) syste...
Information is given in simple terms of the Apollo 15 lunar exploration and scientific equipment, to...
The Science Mission Requirements Document (MSRD) is the authoritative source for the science mission...
Systems design validation of Surveyor lunar roving vehicle - navigation, control and display, televi...
Spacecraft development, mission design planning, flight crew operations, and flight operations are c...
NASA is engaged in early architectural analyses and trade studies aimed at identifying requirements,...
Radar sensor system for acquisition of lunar surface data - Lunar contour mapping syste
Mars landing and reconnaissance mission - environmental control and life support system - subsystem ...
Mission planning and systems design of lunar surface photographic reconnaissance capsul
The University Space Research Association (USRA) requested the University of Minnesota Spacecraft De...