Add to ORKGPreliminary identification and evaluation of promising LO2/Hydrocarbon rocket engine cycles were used to produce a consistent and reliable data base for vehicle optimization and design studies. cycles G and C were chosen for design analysis. Preliminary design analysis of the heat transfer subsystem was performed to establish major technology requirements
High pressure liquid rocket engine design, performance, weight, envelope, and operational characteri...
Liquid oxygen (LOX)/hydrocarbon propulsion concepts for a "second generation' orbiter auxiliary prop...
A research and technology program for advanced high pressure, oxygen-hydrogen rocket propulsion tech...
Preliminary identification and evaluation of promising liquid oxygen/ hydrocarbon (LO2/HC) rocket en...
This study identifies and evaluates promising LO2/HC rocket engine cycles, produces a consistent and...
The advantages and disadvantages, system performance and operating limits, engine parametric data, a...
The program consists of parametric analysis and design to provide a consistent engine system data ba...
Engine data and information are presented to perform system studies on cargo orbit-transfer vehicles...
An advanced LOX/LH2 engine study for the use of NASA and vehicle prime contractors in developing con...
A preliminary characterization of Orbital Maneuvering System (OMS) and Reaction Control System (RCS)...
During the past three decades, an enormous amount of resources were expended in the design and devel...
Preliminary engineering definition information is presented for a liquid pressure-fed reusable boost...
Two hydrogen oxygen rocket engine system concepts were analyzed parametrically over a thrust range f...
Detailed computer models of the engine were developed to predict both the steady state and transient...
Technology for long life, high performing, gaseous hydrogen-gaseous oxygen rocket engines suitable f...
High pressure liquid rocket engine design, performance, weight, envelope, and operational characteri...
Liquid oxygen (LOX)/hydrocarbon propulsion concepts for a "second generation' orbiter auxiliary prop...
A research and technology program for advanced high pressure, oxygen-hydrogen rocket propulsion tech...
Preliminary identification and evaluation of promising liquid oxygen/ hydrocarbon (LO2/HC) rocket en...
This study identifies and evaluates promising LO2/HC rocket engine cycles, produces a consistent and...
The advantages and disadvantages, system performance and operating limits, engine parametric data, a...
The program consists of parametric analysis and design to provide a consistent engine system data ba...
Engine data and information are presented to perform system studies on cargo orbit-transfer vehicles...
An advanced LOX/LH2 engine study for the use of NASA and vehicle prime contractors in developing con...
A preliminary characterization of Orbital Maneuvering System (OMS) and Reaction Control System (RCS)...
During the past three decades, an enormous amount of resources were expended in the design and devel...
Preliminary engineering definition information is presented for a liquid pressure-fed reusable boost...
Two hydrogen oxygen rocket engine system concepts were analyzed parametrically over a thrust range f...
Detailed computer models of the engine were developed to predict both the steady state and transient...
Technology for long life, high performing, gaseous hydrogen-gaseous oxygen rocket engines suitable f...
High pressure liquid rocket engine design, performance, weight, envelope, and operational characteri...
Liquid oxygen (LOX)/hydrocarbon propulsion concepts for a "second generation' orbiter auxiliary prop...
A research and technology program for advanced high pressure, oxygen-hydrogen rocket propulsion tech...