MULTIPLE PISTON TWO-STAGE LIGHT GAS LAUNCHER,
Abstract
A new method for operating light gas launchers is proposed which provides a significant increase in velocity capability. This method, adaptable to existing launchers, makes use of a second piston in the pumptube. The additional piston provides a second compression of the gas in the pumptube with a corresponding additional push on the projectile resulting in increased velocity. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- May 01, 1964
- Accession Number
- AD0604844
Entities
People
- Robert H. Waser
- Robert Piacesi
Organizations
- Naval Ordnance Laboratory