Development of design and programmatic data for space shuttle reaction control systems and integrated reaction control system/orbit maneuvering system
Algorithms are presented for rotational and translational control of the space shuttle orbiter in th...
A computer program for the design and operation of the space shuttle environmental and thermal contr...
Criteria and concepts for onboard checkout and monitoring system for space shuttle propulsion system...
Development of requirements for auxilary propulsion system used with baseline orbiter and booster of...
A comparison of the concepts of auxiliary propulsion systems proposed for the space shuttle vehicle ...
Components and systems technology for developing space shuttle auxiliary propulsion syste
Conceptual design development of space shuttle integrated avionics system emphasizing necessary elec...
Designs and data for selecting aerodynamic surface control and thrust vector control servoactuato
A study for the selection of a low cost shuttle system for design and development was conducted. The...
Space shuttle low pressure, hydrogen oxygen auxiliary propulsion subsystem requirements, tradeoffs, ...
The auxiliary power unit (APU) for the space shuttle is required to provide hydraulic and electrical...
Analytical studies on the theoretical aspects of thrust vector control of large space vehicles were ...
The engineering design for the Shuttle Missions Simulator is presented in sections, with each sectio...
Two alternate oxygen-hydrogen auxiliary propulsion system concepts for use with the space shuttle ve...
The results of studies and software development activities are summarized. Technical reports and mem...
Algorithms are presented for rotational and translational control of the space shuttle orbiter in th...
A computer program for the design and operation of the space shuttle environmental and thermal contr...
Criteria and concepts for onboard checkout and monitoring system for space shuttle propulsion system...
Development of requirements for auxilary propulsion system used with baseline orbiter and booster of...
A comparison of the concepts of auxiliary propulsion systems proposed for the space shuttle vehicle ...
Components and systems technology for developing space shuttle auxiliary propulsion syste
Conceptual design development of space shuttle integrated avionics system emphasizing necessary elec...
Designs and data for selecting aerodynamic surface control and thrust vector control servoactuato
A study for the selection of a low cost shuttle system for design and development was conducted. The...
Space shuttle low pressure, hydrogen oxygen auxiliary propulsion subsystem requirements, tradeoffs, ...
The auxiliary power unit (APU) for the space shuttle is required to provide hydraulic and electrical...
Analytical studies on the theoretical aspects of thrust vector control of large space vehicles were ...
The engineering design for the Shuttle Missions Simulator is presented in sections, with each sectio...
Two alternate oxygen-hydrogen auxiliary propulsion system concepts for use with the space shuttle ve...
The results of studies and software development activities are summarized. Technical reports and mem...
Algorithms are presented for rotational and translational control of the space shuttle orbiter in th...
A computer program for the design and operation of the space shuttle environmental and thermal contr...
Criteria and concepts for onboard checkout and monitoring system for space shuttle propulsion system...