Research on Reliability Criteria of Upper Stage Solid Rocket Motors. 2. Deformation, Damage, Fracture and Combustion
Research on Reliability Criteria of Upper Stage Solid Rocket Motors. 2. Deformation, Damage, Fracture and Combustion
This second report presents macro- and micro-failure processes of solid propellants and propellant deformation, damage and fracture themselves and their relation to combustion by testing with a developed combustion rate measuring device and a special fatigue testing machine for solid propellant.
Dokumentinformationen
Research on Reliability Criteria of Upper Stage Solid Rocket Motors. 2. Deformation, Damage, Fracture and Combustion
1996
57 pages
Report
Keine Angabe
Englisch
Rocket Engines & Motors , Rocket Propellants , Combustion & Ignition , Space Launch Vehicles & Support Equipment , Fatigue(Materials) , Damage , Solid propellant combustion , Solid propellant rocket engines , Upper stage rocket engines , Apogee boost motors , Japanese spacecraft , Fractures(Materials) , Cracking(Fracturing) , Deformation , Thermal fatigue , Fatigue tests , Erosive burning , Burning rate , Solid rocket propellants , Failure mode analysis , Foreign technology