The design, analysis, fabrication and testing of a Kevlar-49/HBRF-55A filament wound chamber is reported. The chamber was fabricated and successfully tested to 80% of the design burst pressure. Results of the data reduction and analysis from the hydrotest indicate that the chamber design and fabrication techniques used for the chamber were adequate and the chamber should perform adequately in a static test.
Filament wound rocket motor chambers
1976-09-01
Report
No indication
English
In-House Research on Filament Wound Rocket Motor Cases
British Library Conference Proceedings | 1996
|Product acceptance testing for filament wound composite rocket motor components
Tema Archive | 1985
|Development of boron epoxy rocket motor chambers.
NTRS | 1972
|Development of Filament Wound M-34 Rocket Motor Casing for M-V Satellite Launcher
British Library Conference Proceedings | 1994
|