Since 1963, solid propellant apogee motors have been placing satellites into geosynchronous orbits. Major technological breakthroughs are not required to satisfy future mission requirements; however, there is a need to improve reliability to enhance cost effectiveness. Several management test options are discussed. A summary of results and conclusions derived from review of missions, where failure of a solid motor was inferred, and correlation of system factors with failures are reported. Highlights of a solid motor diagnostic instrumentation study are presented. Finally, recommendations are provided for areas of future apogee motor upgrade, which will increase project cost effectiveness by reducing the potential for future flight failures
The solid rocket motor failure database; current programs; and shortfalls of solid rocket propulsion...
To increase the success rate of U.S. built Rocket Motors (SRM), the approach taken is: (1) set commo...
Interface problems with various spacecraft which employed solid propellant rocket motors for the fin...
The analysis followed five selected motors through initial design, development, test, qualification,...
Design, testing, and development of solid propellant rocket engine for orbital transfer of Applicati...
A review of typical surveillance and monitoring practices followed during the flight phases of repre...
Qualifications tests on applications technology satellite apogee rocket motor assemblie
A program to identify surplus solid rocket propellant engines which would be available for a program...
Design and test performance of apogee motor nozzle on applications technology satellit
Design, fabrication, and environmental testing of applications technology satellite apogee engine ch...
Design, development, and static firing tests of apogee kick motor for Radio Astronomy Explorer Satel...
A recent article in Aerospace America claims that 'the average success ratio of the current U.S. sta...
The failure of two communication satellites during firing sequence were examined. The correlation/co...
Approximately 85,000 liquid rocket engine failure reports, obtained from 30 years of developing and ...
Rocket vehicle for synoptic meteorological soundings - evaluation of four proposed system
The solid rocket motor failure database; current programs; and shortfalls of solid rocket propulsion...
To increase the success rate of U.S. built Rocket Motors (SRM), the approach taken is: (1) set commo...
Interface problems with various spacecraft which employed solid propellant rocket motors for the fin...
The analysis followed five selected motors through initial design, development, test, qualification,...
Design, testing, and development of solid propellant rocket engine for orbital transfer of Applicati...
A review of typical surveillance and monitoring practices followed during the flight phases of repre...
Qualifications tests on applications technology satellite apogee rocket motor assemblie
A program to identify surplus solid rocket propellant engines which would be available for a program...
Design and test performance of apogee motor nozzle on applications technology satellit
Design, fabrication, and environmental testing of applications technology satellite apogee engine ch...
Design, development, and static firing tests of apogee kick motor for Radio Astronomy Explorer Satel...
A recent article in Aerospace America claims that 'the average success ratio of the current U.S. sta...
The failure of two communication satellites during firing sequence were examined. The correlation/co...
Approximately 85,000 liquid rocket engine failure reports, obtained from 30 years of developing and ...
Rocket vehicle for synoptic meteorological soundings - evaluation of four proposed system
The solid rocket motor failure database; current programs; and shortfalls of solid rocket propulsion...
To increase the success rate of U.S. built Rocket Motors (SRM), the approach taken is: (1) set commo...
Interface problems with various spacecraft which employed solid propellant rocket motors for the fin...