PRESSURE AND TEMPERATURE IN THE EXHAUST OF SIDEWINDER MK 31 MOD O ROCKET MOTOR
Abstract
Temperature and pressure measurements were made in the exhaust stream of 15 statically fired Sidewinder Mk 31 Mod 0 rocket motors. The peak rise in temperature and pressure is presented in the form of contour plots extending to a distance of 90 ft downstream in the case of temperature and of 35 ft downstream for pressure. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Oct 19, 1961
- Accession Number
- AD0265025
Entities
People
- R.g. Bolick
Organizations
- Naval Surface Warfare Center Dahlgren Division