This report describes the results of an experimental program conducted by Physics International to develop a high-performance light-gas to launch projectiles. With this launcher the flight dynamics of re-entry vehicles could be studied to obtain erosion and ablation data in a cost-effective laboratory environment. (Author)
Hypervelocity Launcher Design
1976
164 pages
Report
Keine Angabe
Englisch
Hypervelocity Launcher for Aerothermodynamic Experiments
NTRS | 1995
|Development of a Linear Implosion-driven Hypervelocity Launcher
Tema Archiv | 2013
|