PERFORMANCE OF A SMALL TWO-STAGE, LIGHT-GAS GUN USED FOR IMPACT TESTING
Abstract
The performance of a small, two-stage, lightgas model launcher used for high velocity impact testing is estimated for the practical range of operating variables. Hydrogen and helium are compared as propellants. The effects of powder charge, piston weight, and pump tube gas charge pressure are shown. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Jan 01, 1962
- Accession Number
- AD0270170
Entities
People
- W.b. Stephenson
Organizations
- Arnold Engineering Development Complex