Four possible arrangements of the materials experiment carrier (MEC) and power system (PS) thermal c...
Advanced electric propulsion system concepts with flywheels for electric vehicles are evaluated and ...
Advanced studies are reviewed. Atmospheric sciences, magnetospheric physics, solar physics, gravitat...
Various aspects of a sensitivity analysis, in particular, the impact of variations in metal sheet re...
Feasibility study summary of remote manipulator for satellite repair and maintenance in orbi
The effects on life cycle costs of a number of technology areas are examined for a LEO, 500 kW solar...
The design and flight performance of the Mariner Mars 1971 power subsystem are presented. Mariner 9 ...
Progress from October 1, 1977, through December 31, 1977, is reported in the design of the 50 MT/yea...
Restructuring research objectives from a technical readiness demonstration program to an investigati...
Improvements in a rocketborne electric field meter designed to measure the atmosphere's electric fie...
The results of an initial effort to model the control loops of a 30-cm diameter electron bombardment...
The development of large space structure (LSS) technology is discussed, with emphasis on space fabri...
Low thrust chemical (hydrogen-oxygen) propulsion systems configured specifically for low acceleratio...
A melt level control system was implemented to provide stepless silicon feed rates from zero to rate...
Lightning Attach Point tests were conducted for the space shuttle launch configuration (Orbiter, Ext...
Four possible arrangements of the materials experiment carrier (MEC) and power system (PS) thermal c...
Advanced electric propulsion system concepts with flywheels for electric vehicles are evaluated and ...
Advanced studies are reviewed. Atmospheric sciences, magnetospheric physics, solar physics, gravitat...
Various aspects of a sensitivity analysis, in particular, the impact of variations in metal sheet re...
Feasibility study summary of remote manipulator for satellite repair and maintenance in orbi
The effects on life cycle costs of a number of technology areas are examined for a LEO, 500 kW solar...
The design and flight performance of the Mariner Mars 1971 power subsystem are presented. Mariner 9 ...
Progress from October 1, 1977, through December 31, 1977, is reported in the design of the 50 MT/yea...
Restructuring research objectives from a technical readiness demonstration program to an investigati...
Improvements in a rocketborne electric field meter designed to measure the atmosphere's electric fie...
The results of an initial effort to model the control loops of a 30-cm diameter electron bombardment...
The development of large space structure (LSS) technology is discussed, with emphasis on space fabri...
Low thrust chemical (hydrogen-oxygen) propulsion systems configured specifically for low acceleratio...
A melt level control system was implemented to provide stepless silicon feed rates from zero to rate...
Lightning Attach Point tests were conducted for the space shuttle launch configuration (Orbiter, Ext...
Four possible arrangements of the materials experiment carrier (MEC) and power system (PS) thermal c...
Advanced electric propulsion system concepts with flywheels for electric vehicles are evaluated and ...
Advanced studies are reviewed. Atmospheric sciences, magnetospheric physics, solar physics, gravitat...