Simulated Air Launch Environment. Volume 1
Simulated Air Launch Environment. Volume 1
- Neue Suche nach: O. R. Pritts
- Neue Suche nach: O. R. Pritts
A program was conducted in which the response and failure characteristics of solid propellant rocket motors when subjected to transient thermal conditions representing air launch operational environments were recorded and analyzed. Future Air Force mission profiles were used. The Maverick motor, AGM-65A, was used as a test bed on the program. (Author)
Dokumentinformationen
Simulated Air Launch Environment. Volume 1
1974
258 pages
Report
Keine Angabe
Englisch
Rocket Engines & Motors , Solid propellant rocket engines , Environments , Simulation , Air launched , Flight , External stores , Storage , Rocket propellant grains , Mission profiles , Aerodynamic heating , Aerodynamic loading , Temperature , Profiles , Transients , Failure(Mechanics) , Cyclic tests , Strain gages , Stresses , Safety , Calibration , Tensile properties , Viscoelasticity , Computer programs , Machine coding , Solid rocket propellants , Structural response , Cracks , Air to surface missiles , Thvinc(Thermal viscoelastic computer code) , Thermal viscoelastic computer code , Maverick missiles , TP-L 8006 propellant
Ähnliche Titel
Hybrid Discontinuous Galerkin and Finite Volume Method for Launch Environment Acoustics Prediction
| Online Contents | 2015
High-Resolution Launch Environment Simulations
| NTRS | 2018
High-Resolution Launch Environment Simulations
| NTIS | 2018