In this study, attributes are described for solid and liquid propulsion systems based on historical data. This study is not intended to compare liquid and solid propulsion system attributes, rather to present options for their use in various mission scenarios. US launch vehicle data from 1970 to 2008 was analyzed to assess solid and liquid propulsion development cost and schedule characteristics, performance features, and safety and mission success attributes. The study assessed historical trends for liquid and solid systems, and investigated implications of those trends. It was found that the two propulsion technologies have unique, common and complementary attributes that can be leveraged to meet mission requirements
A study was performed to identify the current and historical trends in the capability of solid rocke...
Plans are formulated for chemical propulsion technology programs to meet the needs of advanced space...
Earth to orbit launch vehicles are propelled by rocket engines and motors, both liquid and solid. Th...
As NASA, the Department of Defense and the aerospace industry in general strive to develop capabilit...
The solid rocket motor failure database; current programs; and shortfalls of solid rocket propulsion...
A research effort has been undertaken to investigate critical aspects of launch vehicle performance ...
State of the art and design criteria for components used in liquid propellant rocket propulsion syst...
A process model was developed to assess the suitability of new/modified technologies and subsystems ...
Storability and performance tests on high energy liquid propellants for space mission
The Liquid Rocket Booster study was initiated by NASA to define an alternative to the Solid Rocket B...
The technical requirements for the solid propellant rocket engine to be used with the space shuttle ...
The liquid rocket propulsion technology needs to support anticipated future space vehicles were exam...
Mass properties data for the 156 inch diameter, parallel burn, solid propellant rocket engine for th...
The factors affecting the choice of the 156 inch diameter, parallel burn, solid propellant rocket en...
Liquid propellant rocket engine conference proceedings and parameters for design of rocket engines a...
A study was performed to identify the current and historical trends in the capability of solid rocke...
Plans are formulated for chemical propulsion technology programs to meet the needs of advanced space...
Earth to orbit launch vehicles are propelled by rocket engines and motors, both liquid and solid. Th...
As NASA, the Department of Defense and the aerospace industry in general strive to develop capabilit...
The solid rocket motor failure database; current programs; and shortfalls of solid rocket propulsion...
A research effort has been undertaken to investigate critical aspects of launch vehicle performance ...
State of the art and design criteria for components used in liquid propellant rocket propulsion syst...
A process model was developed to assess the suitability of new/modified technologies and subsystems ...
Storability and performance tests on high energy liquid propellants for space mission
The Liquid Rocket Booster study was initiated by NASA to define an alternative to the Solid Rocket B...
The technical requirements for the solid propellant rocket engine to be used with the space shuttle ...
The liquid rocket propulsion technology needs to support anticipated future space vehicles were exam...
Mass properties data for the 156 inch diameter, parallel burn, solid propellant rocket engine for th...
The factors affecting the choice of the 156 inch diameter, parallel burn, solid propellant rocket en...
Liquid propellant rocket engine conference proceedings and parameters for design of rocket engines a...
A study was performed to identify the current and historical trends in the capability of solid rocke...
Plans are formulated for chemical propulsion technology programs to meet the needs of advanced space...
Earth to orbit launch vehicles are propelled by rocket engines and motors, both liquid and solid. Th...