Add to ORKGCriteria for the design and development of turbines for rocket engines to meet specific performance, and installation requirements are summarized. The total design problem, and design elements are identified, and the current technology pertaining to these elements is described. Recommended practices for achieving a successful design are included
All the types of actuators and associated operators used in booster, upper stage, and spacecraft pro...
The ways are described by which propellant processing is affected by choices made in designing rocke...
Monograph was published which summarizes and systematically orders large body of successful techniqu...
The turbopump system, from preliminary design through rocket engine testing is examined. Selection o...
Design criteria and recommended practices are discussed for the following configurations selected fr...
Significant guidelines are presented for the successful design of aerospace tanks and tank component...
A monograph is organized and presents, for effective use in design, the significant experience and k...
A monograph on valves for use with liquid rocket propellant engines is presented. The configurations...
The nozzle is a major component of a rocket engine, having a significant influence on the overall en...
The development of and operational programs for effective use in design are presented for liquid roc...
State of the art and design criteria for components used in liquid propellant rocket propulsion syst...
Design and fabrication of gear drives for rocket engine turbopumps are described in the sequence enc...
Liquid propellant rocket engine conference proceedings and parameters for design of rocket engines a...
The design of gas generators intended to provide hot gases for turbine drive is discussed. Emphasis ...
The axial pump is considered in terms of the total turbopump assembly. Stage hydrodynamic design, pu...
All the types of actuators and associated operators used in booster, upper stage, and spacecraft pro...
The ways are described by which propellant processing is affected by choices made in designing rocke...
Monograph was published which summarizes and systematically orders large body of successful techniqu...
The turbopump system, from preliminary design through rocket engine testing is examined. Selection o...
Design criteria and recommended practices are discussed for the following configurations selected fr...
Significant guidelines are presented for the successful design of aerospace tanks and tank component...
A monograph is organized and presents, for effective use in design, the significant experience and k...
A monograph on valves for use with liquid rocket propellant engines is presented. The configurations...
The nozzle is a major component of a rocket engine, having a significant influence on the overall en...
The development of and operational programs for effective use in design are presented for liquid roc...
State of the art and design criteria for components used in liquid propellant rocket propulsion syst...
Design and fabrication of gear drives for rocket engine turbopumps are described in the sequence enc...
Liquid propellant rocket engine conference proceedings and parameters for design of rocket engines a...
The design of gas generators intended to provide hot gases for turbine drive is discussed. Emphasis ...
The axial pump is considered in terms of the total turbopump assembly. Stage hydrodynamic design, pu...
All the types of actuators and associated operators used in booster, upper stage, and spacecraft pro...
The ways are described by which propellant processing is affected by choices made in designing rocke...
Monograph was published which summarizes and systematically orders large body of successful techniqu...