The capability of an Ultra Distributed Energy Store System (UDESS) powered electromagnetic launcher (EM) is experimentally assessed. The UDESS system was developed specifically to address the velocity speed limit seen in plasma armature EM launchers. Metal armature launch packages were also developed and tested to assess the usefulness of the UDESS concept for low velocity applications.
Hypervelocity Launcher for Aerothermodynamic Experiments
1995-07-01
Report
No indication
English
Some aerothermodynamic considerations of hypervelocity vehicles
TIBKAT | 1959
|NTIS | 1976
|Aerothermodynamic Reentry Flight Experiments Expert
British Library Conference Proceedings | 2007
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