Add to ORKGThe preliminary operating specification, envelopes, and weight are presented for the selected engine system, subsystems and other CEI'
Design consideration for air breathing gas turbine engine as third propulsion system of space shuttl
The auxiliary power unit (APU) for the space shuttle is required to provide hydraulic and electrical...
The operating requirements established by NASA for the SSME were considerably more demanding than th...
Detailed mass properties are presented for a gimbaled, fixed thrust, regeneratively cooled engine ha...
Design and systems considerations are presented on an engine concept selection for further prelimina...
Preliminary engineering definition information is presented for a liquid pressure-fed reusable boost...
Final cost estimates are presented for the selected engine configurations and schedules considered i...
The engine weight, mass properties data, and engine design criteria and specifications are presented...
The requirements imposed on the airbreathing engines by the shuttle mission and some results from en...
An analysis and design effort was conducted as part of the study of solid rocket motor for a space s...
The general and design criteria for the expendable second stage of the reusable space shuttle booste...
The factors affecting the choice of the 156 inch diameter, parallel burn, solid propellant rocket en...
Historical weight estimating relationships were developed for the liquid rocket booster (LRB) using ...
Engine data and information are presented to perform system studies on cargo orbit-transfer vehicles...
Two alternate oxygen-hydrogen auxiliary propulsion system concepts for use with the space shuttle ve...
Design consideration for air breathing gas turbine engine as third propulsion system of space shuttl
The auxiliary power unit (APU) for the space shuttle is required to provide hydraulic and electrical...
The operating requirements established by NASA for the SSME were considerably more demanding than th...
Detailed mass properties are presented for a gimbaled, fixed thrust, regeneratively cooled engine ha...
Design and systems considerations are presented on an engine concept selection for further prelimina...
Preliminary engineering definition information is presented for a liquid pressure-fed reusable boost...
Final cost estimates are presented for the selected engine configurations and schedules considered i...
The engine weight, mass properties data, and engine design criteria and specifications are presented...
The requirements imposed on the airbreathing engines by the shuttle mission and some results from en...
An analysis and design effort was conducted as part of the study of solid rocket motor for a space s...
The general and design criteria for the expendable second stage of the reusable space shuttle booste...
The factors affecting the choice of the 156 inch diameter, parallel burn, solid propellant rocket en...
Historical weight estimating relationships were developed for the liquid rocket booster (LRB) using ...
Engine data and information are presented to perform system studies on cargo orbit-transfer vehicles...
Two alternate oxygen-hydrogen auxiliary propulsion system concepts for use with the space shuttle ve...
Design consideration for air breathing gas turbine engine as third propulsion system of space shuttl
The auxiliary power unit (APU) for the space shuttle is required to provide hydraulic and electrical...
The operating requirements established by NASA for the SSME were considerably more demanding than th...